CN104217476A - Electronic key - Google Patents
Electronic key Download PDFInfo
- Publication number
- CN104217476A CN104217476A CN201410230936.3A CN201410230936A CN104217476A CN 104217476 A CN104217476 A CN 104217476A CN 201410230936 A CN201410230936 A CN 201410230936A CN 104217476 A CN104217476 A CN 104217476A
- Authority
- CN
- China
- Prior art keywords
- fuselage
- function
- clamping
- sliding component
- cover cap
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
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Classifications
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- G—PHYSICS
- G07—CHECKING-DEVICES
- G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
- G07C9/00—Individual registration on entry or exit
- G07C9/00174—Electronically operated locks; Circuits therefor; Nonmechanical keys therefor, e.g. passive or active electrical keys or other data carriers without mechanical keys
- G07C9/00944—Details of construction or manufacture
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B19/00—Keys; Accessories therefor
- E05B19/0082—Keys or shanks being removably stored in a larger object, e.g. a remote control or a key fob
Abstract
An electronic key (1; 101) comprises a functional body (6; 106) used for accommodating electrical and electronic components and forming a shell and at least one button member (5; 105) on the functional body (6; 106). With a simple design, the electronic key is provided to ensure a better comfort and at the same time simple and trouble-free operation. This is achieved in that a cover (2; 102) by means of a locking mechanism (14; 114) can be locked on the functional body (6; 106) releasably, and can cover at least the upper side (7; 107) and / or the bottom (8; 108) of the function body (6; 106).
Description
Technical field
The present invention relates to a kind of electron key, it has function fuselage and at least one Key element for laying electric power and electronic component and being configured to housing shape, and this Key element is arranged on it this function machine.
Background technology
The electron key of aforementioned type is for example known by DE 101 21 045 A1, and it relates to the housing for electron key.This housing is made up of upper cover and lower cover at this, and wherein this upper cover has groove, and the Key element with single button inserts in this groove.Electric power and electronic component are arranged on circuit board in this enclosure interior.The member that formation by Key element on can operating circuit plate is engaging element.Nowadays this known electron key is applied in motor vehicle to standardization, and can be used for simpler and easy and more cosily open or close motor vehicle door and/or baggage room.But the shortcoming by the known electron key of prior art is, their operate not close friend and comfort levels are limited.Therefore for example standard is, cell through lid is set, it can pass in upper cover or lower cover, wherein always must apply certain power and need certain sensitivity in order to take off this lid, to this lid is turned down from upper cover or the lower cover of housing in order to change battery.Although be applied in electron key to this lid standardization, this lid can not only hide battery case, and can hide emergency key.But this lid can not meet day by day the comfort level requirement improving, and can not meet user and wish requirement simple to operate.
Summary of the invention
The object of the invention is, create a solution, it is in simply constructed mode and a kind of electron key is provided inexpensively, and it has guaranteed better comfortableness, and can realize the operation of simple and no problem simultaneously.
In the electron key of aforementioned type, this object is achieved in the following manner by the present invention, and lid is releasably locked in function machine and hides at least upside and/or the downside of function fuselage with it and completely by locking mechanism.
Favourable and suitable structural scheme and improvement project of the present invention drawn by dependent claims.
By the invention provides a kind of electron key, it also has high comfortableness by simple and compact make in operation.The effect of this lid is, defencive function fuselage and be arranged on its top also or member of its inside avoid damaging.With compared with the known lid or cell through lid of prior art, described lid has hidden upside and/or the downside of function fuselage completely, and therefore they make to have the form of expression graceful and high-quality by electron key of the present invention.In addition, can also be without problems and just lid can be taken off with it from function machine without effort very by this locking mechanism, be for example arranged on function machine mechanical emergency key or battery case with it in order to employ.But this locking mechanism also allows cosily to change lid, because not only just wish to change lid in the time that lid is impaired.For example, in order to make electron key there is on the whole format surface new and that outward appearance is up-to-date, also wish to change this lid.
In the structural scheme of electron key of the present invention, specify, this lid has at least one and is used for hiding completely the housing of upside or downside, or this lid has the first housing of the upside that hides function fuselage completely and hides the second housing of the downside of function fuselage completely.Therefore this lid can be made up of at least two housings, therefore in these two housings, only has one to unclamp from function machine with it, and another housing hides as beforely and therefore upside or the downside of defencive function fuselage.By this hood-like structure, these at least two housings have wheel rim on its outward flange separately, this wheel rim match with the outline of function fuselage at least piecemeal and like this around, make to only have the region, longitudinal side of function fuselage to touch from the outside, wherein these housings seamlessly and closely surround function fuselage (except region, longitudinal side).
When the formation that Key element is arranged on prior art is on the upside of key of housing shape and/or downside time, if while being especially for example carried in trousers pocket by the known key of prior art, over and over again handle undesirably this Key element.If also change the battery of electron key, if or should employ the emergency key being arranged in casing member or on casing member, fixing especially problem of Key element, because exist in both cases the danger that single button may unclamp from casing member.For this reason, in another structural scheme of electron key, by the present invention regulation, it is upper that this at least one Key element is fixed in two longitudinal sides of function fuselage one, and this longitudinal side couples together upside and downside.Due to Key element setting separately be placed on the longitudinal side of function fuselage, instead of as prior art, arrange and be placed on the upside and/or downside of the function fuselage that is configured to shelly, so avoided the careless manipulation of button.Especially by button being arranged on to these longitudinal sides (also or just a longitudinal side on) of function fuselage, on the upside of function fuselage and/or downside, create the position for laying other element.Can realize the manipulation of this at least one Key element and it is discharged by housing layout of the present invention, therefore before operating buttons element, needn't remove the lid of Key element.But housing abuts on this at least one Key element, function fuselage seamlessly and is closely surrounded on the whole by these cover caps.
The present invention specifies in other structural scheme of electron key, the hook that locking mechanism comprises at least one first distolateral and/or at least one longitudinal side that is arranged on function fuselage connects, and comprise at least one and be arranged on the second sealed connection of shape on distolateral of function fuselage, the mode that at least one cover cap connects to clamp by these is releasably arranged on it function machine.By the present invention, in order to lay cover cap separately, first between function fuselage and corresponding cover cap, set up hook and connect, these cover caps are locked in it function machine by being clamped and connected subsequently.
Simple with regard to structure aspects, be used for forming the possibility being clamped and connected, the present invention specifies in improvement project, the sealed connection of this at least one shape is arranged on the second clamping running-on on distolateral of function fuselage and at least one clamping by least one and connects piece and form, wherein this clamping connects piece and is arranged near of the vertical end of this at least one cover cap, this vertical end be arranged on function fuselage second distolateral on, and this at least one clamping running-on connects power that piece can overcome elastic reset member from latched position activity to off-position with respect to this at least one clamping, in this latched position, this at least one clamping running-on abuts in this at least one clamping and connects on piece and stoped clamping to connect the relative motion between piece and clamping running-on, in this off-position, this at least one clamping running-on discharges this at least one clamping and connects piece.Cover cap is separately locked in it function machine by this way, its method is: connect piece extruding towards clamping and make before it clamp-ons in the direction that patches dorsad running-on at the clamping running-on of function fuselage, cover cap patch running-on first with function fuselage in engagement, cover cap is locked in it function machine.
With regard to simple with regard to structure aspects, to be used for forming hook connection possibility, specify by the present invention, this at least one hook connects the accommodation section that is molded in respectively the snapclose sheet on the longitudinal side of function fuselage and is subordinated to each snapclose sheet by least one and forms, wherein each affiliated accommodation section is molded on the longitudinal side of corresponding cover cap, and wherein the sealed connection of this at least one type is to form like this, in second of function fuselage the distolateral direction, pushes corresponding cover cap and this at least one snapclose sheet be pressed in this accommodation section thus kayser.
In order to unclamp on distolateral and to be clamped and connected at second of function fuselage, the present invention also further specifies in structural scheme, be provided with the steerable sliding component at least one longitudinal side transverse to function fuselage, this at least one clamping running-on is arranged on this sliding component, wherein this at least one clamping running-on and this at least one sliding component be also therefore placed in pockets (this pockets be molded over function fuselage second distolateral on) in and in this pockets, overcome the power of elastic reset member can slippage between latched position and off-position.Under the not operation state of sliding component, this sliding component remains in latched position, therefore clamps running-on and connects piece extruding and make together corresponding cover cap remain on it function machine with clamping and the mode that clamps towards clamping.
In the electron key with two cover caps especially advantageously, the first cover cap is equipped with the first sliding component and the second cover cap to be equipped with the second sliding component, wherein the first and second sliding components comprise respectively clamping running-on and feather key, wherein the clamping running-on of the first sliding component be arranged in the first pockets and with the first sliding component be arranged on feather key outside function fuselage in slip couple state, this pockets extends in the direction of the downside of function fuselage from upside.Wherein the clamping running-on of the second sliding component be arranged in the second pockets and with the second sliding component be arranged on feather key outside function fuselage in slip couple state, this pockets extends in the direction of the upside of function fuselage from downside.These two cover caps can unclamp from function machine by this way independently of each other with it, therefore also only have a unique cover cap to remove, and if do not take another cover cap apart, this another cover cap is also arranged on regularly function machine and can unclamps with it and not.
With regard to the operation (object is dismounting housing) of the ergonomics aspect of electron key, in structural scheme of the present invention, specify, in the second distolateral corner regions that the first sliding component is arranged on, and the second sliding component is arranged on the relative with the first sliding component of function fuselage and in the corner regions of putting, wherein the first and second sliding components are constructed to such an extent that can mutually move.Therefore this electron key can cosily be held in user's the palm of the hand, wherein user is in order to unclamp cover cap this sliding component that for example can move up with the thumb-actuated sliding component of the same hand and in the side of another sliding component, thereby not connecing piece with clamping with sliding component in the clamping running-on of sports coupling state sticks together, therefore cover cap no longer clamps and remains on it function machine, but can unclamp with it and dismantle from function machine.
Being used for by the present invention the alternative possibility (but it is textural equally especially simple) that structure hook connects is, hook connects and is molded over the first groove on distolateral of function fuselage and at least one by least one and patches running-on and form, wherein this at least one patch running-on and be arranged at least one cover cap on distolateral first, and wherein this to be clamped and connected be to form like this, in second of function fuselage the distolateral direction, push at least one cover cap and at least one patches running-on and is pressed in this at least one accommodation section by this thus.
Same with regard to the operation of electron key aspect ergonomics advantageously, be arranged on the second sliding component on distolateral, the power that it has this at least one clamping running-on and overcomes elastic reset member between latched position and off-position in the first distolateral direction slip.
Owing to saving the reason of cost and minimizing part, if sliding component is configured to I-shape, can omit the second sliding component of the second cover cap by structural scheme of the present invention, wherein the indirect piece of this I-shape sliding component especially middle with feather key in Flexible coupling state, and stop running-on is transverse to clamping running-on and be oppositely molded in it its vertical end separately (this vertical end is arranged on the upside or downside of function fuselage), this stop running-on is used for sliding component to be fixed on it function machine.The sliding component that is configured to I-shape is arranged on stop running-on on vertical end and surrounds to a certain extent the second end of function fuselage by it, and therefore sliding component is releasably secured to it function machine by the mode of clip by stop running-on.Then can handle sliding component by feather key, to cancel the sealed connection of shape for dismantling cover cap.
Aspect structure especially advantageously, in other structural scheme of the present invention, specify, each stop running-on of the sliding component of I-shape is configured to hook-shaped and catches from behind and be arranged on stop with it of function machine protuberance, wherein the stop running-on of the sliding component of this I-shape is arranged in the bag container of corresponding cover cap, and wherein the sidewall of bag container is that the clamping of corresponding cover cap connects piece.Therefore in the situation that setting up the sealed connection of shape, this clamping running-on is equivalent to the mode of lock pin, and this lock pin pushes in bag container and therefore fixes cover cap.
Should be understood that above-mentioned and also the feature of elaboration can not only be applied in the combination of mentioning separately below, can also in other combination or individually, apply, and can not leave framework of the present invention.Framework of the present invention only defines by claim.
Brief description of the drawings
Other details, the feature and advantage of content of the present invention draw from the description below in conjunction with accompanying drawing, exemplarily show the preferred embodiments of the present invention in this accompanying drawing.Wherein shown in the drawings:
Fig. 1 perspective there is shown by the first embodiment by electron key of the present invention;
Fig. 2 details there is shown Fig. 1 by electron key of the present invention;
Fig. 3 from above the perspective seen there is shown the function fuselage of the electron key of Fig. 1;
Fig. 4 there is shown the end face of the function fuselage of the electron key of Fig. 1 at the section of perspective;
Fig. 5 has illustrated the electron key of the present invention within the scope of the first sliding component of Fig. 1 in the side cut away view expanding;
Fig. 6 has illustrated the electron key of the present invention within the scope of the second sliding component of Fig. 1 in the side cut away view expanding;
Fig. 7 the side-looking of perspective there is shown Fig. 1 by two of the electron key of the present invention different planes of cutting open;
Fig. 8 there is shown single installation steps in perspective, be used for cover cap be placed in Fig. 1 by with it the function machine of electron key of the present invention;
Fig. 9 perspective there is shown by the second embodiment by electron key of the present invention;
Figure 10 details there is shown Fig. 9 by electron key of the present invention;
Figure 11 details there is shown Fig. 9 by the sliding component of electron key of the present invention;
Figure 12 perspective there is shown Fig. 9 by the housing of electron key of the present invention and function fuselage;
Figure 13 expand side cut away view in illustrated Fig. 9 by electron key of the present invention, it has the cover cap of dismounting; And
Figure 14 there is shown single installation steps in perspective, be used for cover cap be placed in Fig. 9 by with it the function machine of electron key of the present invention.
Embodiment
Fig. 1 perspective there is shown by the first embodiment by electron key 1 of the present invention, and Fig. 2 perspective details there is shown electron key 1.This electron key 1 is used for without the blocking device of key ground activating machine motor-car, and has lid 2, this lid shown in the first embodiment in formed by the first cover cap 3 and the second cover cap 4.In addition as illustrated in fig. 1 and 2, electron key 1 has respectively flexible Key element 5 on its longitudinal side 9.These two Key elements 5 provide different functions, for example, open with the blocking device of breech-block motor-car or open baggage room.With compared with the known key of prior art, these two Key elements 5 are arranged on electron key 1 from the side.
In the detail view of Fig. 2, the first cover cap 3 and the second cover cap 4 disassemble from function fuselage 6, and these two cover caps form hood-like lid 2 together, and this function fuselage is the parts of electron key 1.These two cover caps 3 and 4 are structurally designed to the same, and the vertical view of the first cover cap 3 that therefore Fig. 2 provides is that meaning is identical with the vertical view of the second cover cap 4.The view of the downside of the second cover cap 4 that equally, Fig. 2 provides is that meaning is identical with the view of the downside of the first cover cap 3.Therefore because structure is identical, the vertical view of the second cover cap 4 and the lower view of the first cover cap 3 have been omitted.
Shown in the first embodiment in, the first cover cap 3 has hidden the upside 7 of function fuselage 6 completely, and the second cover cap 4 has hidden the downside 8 of function fuselage 6 completely.Generally, this lid 2 has hidden upside 7 and/or the downside 8 of function fuselage 6 completely, and this lid at least forms by one in cover cap 3 and 4.Because cover cap 3 designs to such an extent that structure is identical with 4, the second cover cap 4 also can be fixed on upside 7, and the first cover cap 3 can be fixed on the downside 9 of function fuselage.Function fuselage 6 is configured to housing shape and is used for laying electric power and electronic component, and these members are for the blocking device without key ground activating machine motor-car.In addition, Key element 5 is arranged on function fuselage 6, and be arranged on the electric power of inside of function fuselage 6 and/or electronic switch in effective connection status, wherein unshowned seal element seals the intermediate cavity between Key element 5 and the inside of function fuselage 6, therefore there is no the inside that moisture can entered function fuselage 6.These two Key elements 5 extend to the second distolateral of function fuselage 6 from first distolateral 10 of function fuselage 6, and are fixed on each longitudinal side 9 of function fuselage 6, and this longitudinal side couples together upside 7 and downside 8.This Key element 5 also can alternatively have multiple buttons, and they can be arranged on the longitudinal side 9 of function fuselage 6.
In the detail view of Fig. 2, also show, two cover caps 3 and 4 are because hood-like structure has wheel rim 34 on its outward flange separately, and this wheel rim matches with the outline of function fuselage 6 at least piecemeal.This wheel rim 34 surrounds the outline of function fuselage 6, makes to only have second distolateral 11 region piecemeal to see from the outside.Because these longitudinal sides are hidden by these two Key elements 5 and first distolateral 10 hidden by each wheel rim of cover cap 3,4 completely, this wheel rim is provided with larger extending part in this region.Cover cap 3,4 essentially no gap and closely surround function fuselage 6 on the whole, except the region of longitudinal side 9 and second distolateral 11, wherein especially the upside of function fuselage 6 and downside 7,8 are closely closely surrounded by cover cap 3,4.
Fig. 5 and 6 there is shown by electron key 1 of the present invention at the section of side respectively, and wherein these views show respectively the enlarged view in the second distolateral region.At this, the sectional view shown in Fig. 5 extends through the first sliding component 12, and the sectional view shown in Fig. 6 extends through the second sliding component 13.Locking mechanism 14 (seeing Fig. 7) takes off on the whole from the view of Fig. 3 to 7, and the lid 2 being made up of the first cover cap 3 and the second cover cap 4 is releasably arranged and is locked in by this locking mechanism by the function fuselage 6 of the electron key of the first embodiment 1.According to the present invention, locking mechanism 14 comprises at least one hook connection 15 and the sealed connection 16 of at least one shape, and the sealed connection of this shape designs by the mode being clamped and connected.
Near the sectional view of Fig. 7 left one side of something shows the longitudinal side 9 of function fuselage 6 and the longitudinal side 19 of cover cap 3,4, at length show that hook connects 15, this hook connecting is connected in the first embodiment and arranges and be formed on the longitudinal side 9 of function fuselage 6.In an illustrated embodiment, four hooks connect 15 and are arranged on each longitudinal side 9 of function fuselage 6, and wherein Fig. 7 connects 15 because selected sectional view only shows two hooks.Hook connection is separately made up of snapclose sheet 17 and accommodation section 18.At this, each snapclose sheet 17 is molded on the longitudinal side 9 of function fuselage 6, and side is outstanding from function fuselage 6.Therefore, four snapclose sheets 17 are molded on each longitudinal side 9 of function fuselage 6, as shown in Figures 2 and 4.A corresponding accommodation section 18 having respectively for snapclose sheet 17 in these two cover caps 3,4, especially as from shown in Fig. 2.At this, each cover cap 3,4 has respectively two accommodation sections on its longitudinal side.The snapclose sheet 17 of function fuselage 6 has the latch surfaces 20 (seeing Fig. 7) tilting towards the first side 10 declines, they are for fixing cover cap 3,4 and correspondingly configured accommodation section 18 actings in conjunction in cover cap 3,4, this accommodation section has respectively latch face 21, and this latch face declines and extends towards first distolateral 10 equally.In the cover cap 3,4 being fixed on function fuselage 6, the mutual wedging of latch face 21 of the kayser face 20 of function fuselage 6 and cover cap 3,4.For fixing cover cap 3,4 separately, corresponding snapclose sheet 17 is inserted in the accommodation section 18 of corresponding cover cap 3,4, as shown in Fig. 8 on the left side view.At this, the first cover cap 3 is placed on the upside 7 of function fuselage 6, as by shown in arrow A.This is equally applicable to the second cover cap 4, and it is placed on the upside 8 of function fuselage 6, as shown in the arrow B by Fig. 8.In the time that cover cap 3,4 is placed on function fuselage 6, the accommodation section 18 of cover cap 3,4 is directed like this, makes snapclose sheet 17 imbed or push in affiliated accommodation section 18.
So, in order to make corresponding kayser face 20 and affiliated latch face 21 can overlap the to each other wedging, must in second distolateral 11 direction, apply corresponding power, this power is applied by user and illustrates by arrow C and the D of Fig. 8.By the power (arrow C in Fig. 8 and D) being applied by user, the clamping of clamping running-on 22 separately under abutting in connects on piece 3, therefore on second distolateral 11, sets up the sealed connection 16 of type, as below also by describing in detail.
This is used for making the first cover cap 3 to be fixed on that the sealed connection 16 of shape on function fuselage 6 has clamping running-on 22 and clamping connects piece 23, this clamping running-on 22 be arranged on function fuselage 6 second distolateral 11 on, and clamping connects piece and is formed in being respectively located on the vertical end 24 on second distolateral 11 of cover cap 3 and (for example sees Fig. 5 and 7).For the first cover cap 3 is locked on function fuselage 6, first the snapclose sheet of function fuselage 6 17 is brought in the affiliated accommodation section 18 of corresponding cover cap 3,4 (seeing Fig. 7 and 8), as already described.Subsequently, the first cover cap 3 moves upward or pushes (direction of seeing the arrow C of Fig. 8) in second distolateral 11 side of function fuselage 6, abut on clamping running-on 22 with method of clamping like this until the clamping of the first cover cap 3 connects piece 23, make clamping connect piece 22 to push the clamping running-on 23 of the first cover cap 3 in first distolateral 10 direction of function fuselage 6 dorsad.This position that clamping running-on 22 and clamping connect piece 23 is equivalent to latched position.
Owing to connecing the clamping effect existing between piece 23 and clamping running-on 22 in clamping, this clamping effect extends to the downside 8 of function fuselage 6 from upside 7 by certain its clamped height, so the first cover cap 3 can not be removed from upside 7 substantially on second of function fuselage 6 distolateral 11.Only have and connect piece 23 and clamping running-on 22 disconnects engagement when clamping, connect piece 22 no longer in second distolateral 11 direction when press nip running-on 23 when clamping, this point just becomes possibility.In other words, because move the clamping horizontal like this longitudinal side 6 that is function fuselage 6 of running-on 22, no longer stop this motion until the clamping running-on 23 of cover cap 3 can move up and clamp running-on 2g in first distolateral 10 side, could cancel the tension of cover cap 3.
No longer abut in clamping and connect on piece 23 in order to make to clamp running-on 22, in the time that the first cover cap 3 is locked on function fuselage 6, the first sliding component 12 must be handled by user, and this first sliding component is arranged in second distolateral 11 folding corner region of function fuselage 6 and is arranged on function fuselage 6 at this place.The first sliding component 12 comprises square 26, feather key 28 and connection and connects piece 27, and clamping running-on 22 is arranged on this square and flexible reposition element 25 is given prominence to from this square from the side, and this connection connects piece square 26 and feather key 28 are coupled together.In the time that sliding component 12 is arranged on function fuselage 6 and before fixing the first cover cap 3, just the assembling parts of the sliding component of many bodies 12 is got up.Be arranged on function fuselage 6 and (also for example see Fig. 2 or Fig. 4) for the first sliding component 12, the first pockets 29, this pockets extends out from upside 7 in the direction of the downside 8 of function fuselage 6.This square 26 inserts in the first pockets 29 by flexible reposition element 25.Guide through the first logical perforation 31 and be fixedly linked with square 26 once connect piece 27, this logical perforation function fuselage 6 second distolateral 11 in moulding.Connect feather key 28 can be set in piece 27 in connection, also or this feather key be fixed on and connect on piece 27.After laying the first sliding component 12, the power that it overcomes flexible reposition element 25 transverse to longitudinal side 9 on second distolateral 11 moves, to the first cover cap 3 is placed on function fuselage 6.Abut in no longer for a long time clamping and connect on piece 23 and in order not stop or hinders the motion (object is to dismantle the first cover cap 3) of cover cap 3 in order to make to clamp running-on 22 now, user must handle the first sliding component 12 and move up it in the side of the second sliding component 13 from the side, therefore the clamping running-on 22 being arranged on the first sliding component 12 moves in off-position subsequently, and clamping running-on 22 discharges clamping and connects piece 23 in this off-position.For this purpose, the first sliding component 12 moves to off-position for the power of dismantling the first cover cap 3 and overcoming elastic reset member 25 by user from latched position.This flexible reposition element 25 shown in the first embodiment in be configured to Compress Spring, and as long as user is not for getting loose the first cover cap 3 to apply resistance from function fuselage 6, this reposition element just remains on latched position by the first sliding component 12.As mentioned above, the first sliding component 12 is placed in the first pockets 29 (sees Fig. 2,4 and 5), this pockets 29 function fuselage 6 second distolateral 11 on moulding.In the first pockets 29, the first sliding component 12 can overcome power slippage between locking member and off-position of elastic reset member 25.Therefore, clamping running-on 22 connects power that piece overcomes elastic reset member 25 from latched position activity to off-position with respect to clamping, in this latched position, this at least one clamping running-on 22 abuts in that clamping connects on piece 23 and push this clamping in first distolateral 10 direction of function fuselage 6 and connects piece, and in this off-position, this at least one clamping running-on 22 discharges these at least one clampings and connects piece 23.The sealed connection 16 of this shape in the effect of latched position is, connect piece 23 and push, thereby the first cover cap 3 is placed on function fuselage 6 in the mode clamping by making to clamp running-on 22 towards clamping.
1 of this electron key is provided with unique cover cap 3, and the cover cap 3 that therefore (the first He) is unique mounts and dismounts as described above.But in an illustrated embodiment,, except the upside 7 being hidden completely by the first cover cap 3, the downside 8 of function fuselage 6 is also hidden completely, has applied the second cover cap 4 for this reason.For the second cover cap 4 being fixed on function fuselage 6 and again from 6 dismountings of function fuselage, regulation, another hook that the locking mechanism 14 of the electron key 1 of the first embodiment comprises on first distolateral 10 connects the sealed connection 16 of another shape on 15 and second distolateral 11, but the sealed connection of this shape is being arranged between the second cover cap 4 and function fuselage 6 on its downside 8 now, as for example the same with shown in 8 from Fig. 7.In order to dismantle the second cover cap 4, be provided with the second sliding component 13, it is arranged in other folding corner region of second distolateral 11.The second sliding component 13 structurally designs equally with the first sliding component 12, as appreciable from Fig. 2.Because cover cap 3,4 is identical with the structure of sliding component 12,13, so can manufacture inexpensively electron key 1.Fig. 2 shows the second sliding component 13, and it has only reversed 180 ° and be erected in form on head compared with the first sliding component 12.Because structure is identical, the second 136 of sliding components are described simply, and elaborating with reference to the first sliding component 13.The square of the second sliding component 13 is inserted in the second pockets 30, compared with the first pockets 29, this pockets 30 extends along the direction of its upside 7 from the downside 8 of function fuselage 6 now, as especially can seen in Fig. 4, Fig. 4 has illustrated the second distolateral 11 region through the first and second pockets 29,30 of function fuselage 6 in section.Certainly be that the connection of the second sliding component 13 connects piece 27 the second logical perforation 32 (seeing Fig. 2) are set, so that square 26 is with from outer setting, the feather key 28 on function fuselage 6 couples together.The sealed connection 16 of shape between the second sliding component 12 and the second cover cap 4 substantially with the first sliding component 11 and the first cover cap 3 between the sealed connection 16 of shape be that structure is identical, wherein give the working method of the same race that is used for fixing and dismantles cover cap 4, therefore can be with reference to the corresponding elaboration of the first cover cap 3.The elastic reset member of the second sliding component 13 is configured to Compress Spring equally, and the second sliding component 13 is remained in latched position, and in this latched position, the second cover cap 4 is fixed on function fuselage 6.Only have and make every effort to overcome when what user applied the power that has taken elastic reset member 25, thereby the second slide switch 13 moves up in the side of the first slide switch 12, the second cover cap 4 could unclamp and take off from function fuselage 6.By the resistibility being applied by user, 26 power that overcome elastic reset member 25 of square that are arranged in the second pockets 30 of the second sliding component 13 move to off-position from latched position.Therefore, the clamping running-on 22 of the second sliding component 13 connects power that piece 23 overcomes elastic reset member 25 from latched position activity to off-position with respect to the clamping of the second cover cap 4, in this latched position, this at least one clamping running-on 22 abuts in that clamping connects on piece 23 and push this clamping in first distolateral 10 direction of function fuselage 6 and connects piece, clamps running-on 22 and discharge clamping and connect piece 23 in this off-position.After the second cover cap 4 unclamps, just can employ the downside 8 of function fuselage 6, wherein in the first embodiment, cell through lid can be arranged on downside 8, and this cell through lid is releasably arranged on function fuselage 6 in order to change battery.
Therefore cover cap 3,4 o'clock is being installed, the manipulation of corresponding sliding component 12,13 makes the affiliated clamping running-on 22 of square 26 connect piece 23 with respect to the clamping of corresponding cover cap 3,4 to move.For this square being guided in the time that square 26 moves between latched position and off-position, be provided with motion guidance groove 33, its moulding and guide to a certain extent sliding component 12 or 13 to carry out side transverse to longitudinal side 6 in the direction of unsteered sliding component 12 or 13 to move in the inner side of the Function-oriented fuselage 6 of corresponding cover cap 3,4 respectively, and can make cover cap 3,4 move up in first distolateral 10 side in the time of dismounting.
Fig. 9 to 14 show by the second embodiment and details by the single member of electron key 101 of the present invention and key 101, this key is used as equally the blocking device of motor vehicle and is used and have lid 102, and this lid is made up of the first cover cap 103 and the second cover cap 104.The electron key 101 of the second embodiment is the same with the first embodiment has flexible Key element 105 equally, and they are arranged on the function fuselage 106 of electron key 101.With regard to the function contemplating of Key element 105 and side, with reference to the elaboration of the first embodiment.These two cover caps 103 with 104 textural be equally also the same, therefore the view full disclosure shown in Figure 10 the technical characterictic of these two cover caps 103 and 104, this view shows the upside of the first cover cap 103 and the downside of the second cover cap 104.The first cover cap 103 has hidden the upside 107 of function fuselage 6 completely, and the second cover cap 104 has hidden the downside 108 of function fuselage 6 completely.Because the structure of these two cover caps 103,104 is identical, the first cover cap 103 also can be fixed on downside 108, and the second cover cap 104 also can be fixed on the upside 107 of function fuselage 106.Key element 105 also extends to the second distolateral 111 of shelly function fuselage 106 from first distolateral 110, and wherein Key element 105 is fixed on each longitudinal side 109 of function fuselage 106.Each Key element 105 of the second embodiment can alternatively be made up of multiple buttons.
Figure 13 perspective section there is shown by the second embodiment by electron key 101 of the present invention.Locking mechanism 114 takes off from the view of electron key 101, and the lid 102 being made up of the first cover cap 103 and the second cover cap 104 is releasably arranged and is locked on function fuselage 106 by this locking mechanism.Locking mechanism 114 comprises hook connection 115 and is clamped and connected 116.This hook connect 115 be arranged on function fuselage 106 first distolateral 110 on, and comprise in an illustrated embodiment two grooves 117 (seeing Figure 12) and form corresponding to these grooves patch running-on 118 (for example seeing Figure 10 or 13), these two grooves be molded over function fuselage 106 first distolateral 110 on, and this grafting running-on be arranged on two cover caps 103 and 104 first distolateral 119 on.In order to lock cover cap 103,104, each grafting running-on 118 of cover cap 130,104 is brought in the groove 117 of function fuselage 106, connects 115 to set up hook.Hook connect 118 on the whole can by least one be molded over function fuselage 106 first distolateral 110 on groove 117 and at least one patch running-on 118 and form, wherein this at least one patch running-on 118 and on first distolateral 119, be arranged at least one cover cap 103,104.
Setting up after hook connects, set up and be clamped and connected 116 subsequently, as by shown in Figure 14.This be clamped and connected be arranged on function fuselage 106 second distolateral 111 on and form like this, it pushes cover cap 103,104 and therefore the grafting running-on 118 of cover cap 103,104 is pressed in corresponding groove 117 in second distolateral 111 direction of function fuselage 106.
With reference to Figure 13, being clamped and connected 116 has clamping running-on 120 and clamping and connects piece 121, this clamping running-on be arranged on function fuselage 106 second distolateral 111 on, and clamping connect piece be formed in respectively cover cap 103 with 104 with first distolateral 119 relative and put distolateral on.
For the first and second cover caps 103,104 are locked on function fuselage 106, the running-on 118 of respectively pegging graft (for example seeing Figure 13) is first brought in the groove 117 of function fuselage 6, as described earlier.Subsequently, each cover cap 103,104 with the first distolateral 119 relative and distolateral swing in second distolateral 111 direction of function fuselage 106 (seeing the arrow E of Figure 14) of putting, until each clamping of each single cover cap 103,104 connects piece 121 like this with method of clamping on the clamping running-on 120 under abutting in, make to clamp running-on 120 and push corresponding cover cap 103,104 in first distolateral 110 direction of function fuselage 106 dorsad.This position that clamping running-on 120 and clamping connect piece 121 is equivalent to latched position.Because clamping connects piece 121 and the clamping running-on 120 clamping effect of existence between cover cap 103 or 104 in other words, cover cap 103,104 can not be removed from upside 107 or from downside 108 on second of function fuselage 106 distolateral 111.Only have and connect piece 121 and clamping running-on 120 disconnects engagement when clamping, no longer stop that when clamping connects piece 120 while clamping running-on 121, this point just becomes possibility.Especially as appreciable from Figure 13, clamping running-on 120 inserts in bag container 122, and this bag container is arranged in each cover cap 103,104, and wherein the sidewall 123 of bag container 122 is that the clamping of corresponding cover cap 103,104 connects piece 121.
No longer abut in clamping and connect on piece 121 in order to make to clamp running-on 120, in the time that the one the second cover caps 103,104 are locked on function fuselage 106, sliding component 124 must be handled by user, this sliding component be arranged on function fuselage 106 second distolateral 111 on.Sliding component 124 there is clamping running-on 120 and construct can slippage in first distolateral 110 the direction at function fuselage 106 between latched position and off-position, in this off-position, clamp running-on 122 and do not abut in clamping and connect on piece 121.This sliding component is substantially configured to I-shape (for example seeing Figure 13) and has indirect piece 125 in xsect, and this indirect piece and feather key 126 carry out Flexible coupling.As appreciable from Figure 11, feather key 126 has flexible and is configured to hook-shaped coupling arm 140, this coupling arm engages with the sliding component 124 of I-shape, and wherein the hooked end of coupling arm 140 is inserted and stoped the decoupling of sliding component 124 by the aperture 141 of sliding component 124.The vertical end 127 and 128 of indirect piece 125 is arranged on the upside and downside 107,108 of function fuselage 106.Stop running-on 129 is transverse to the indirect piece 125 of clamping running-on 120 and be oppositely molded in it on vertical end 127 or 128 separately, and this stop running-on 129 is used for a sliding component 124 and is fixed on function fuselage 106.Each stop running-on 129 of the sliding component 124 of this I-shape is configured to hook-shaped and catches from behind the stop protuberance 130 being arranged on function fuselage 106, wherein the clamping running-on 120 of I-shape sliding component 124 is arranged in the bag container 122 of corresponding cover cap 103,104 by the mode of lock pin, and stops corresponding cover cap 103,104 to move from function fuselage 106 forward.
This feather key 126 is steerable from the outside for the user, its mode is: feather key 126 or sliding component 124 are extruded in first distolateral 110 direction of function fuselage 106, the power that wherein user must overcome elastic reset member 131 moves sliding component 124, because he is that the first and second cover caps 103,104 are also or only for one in these two cover caps 103 or 104 has been unclamped the sealed connection 116 of shape.By push sliding component 124 in first distolateral 110 direction of function fuselage 106, the clamping running-on 120 coming into force by lock pin mode does not abut in clamping and connects on piece 121, and from the bag container 122 of cover cap 103,104, reach thus, therefore cover cap 103,104 can be arranged from function fuselage 106 in order to realize dismounting.
This flexible reposition element 131 inserts in second distolateral 111 aperture of function fuselage 106, and is arranged on the extension site and steering thereof of feather key 126.All handle this feather key 126 at 103,104 o'clock at dismounting cover cap in all cases, because the second embodiment is only provided with unique sliding Key 126, not only can make the first cover cap 103 also can make the second cover cap 104 (being integrally or individually or only one of them) unclamp from function fuselage 106 by it.Different from the first embodiment, this unique feather key 126 is no longer arranged in corner regions in a second embodiment, and is arranged on second distolateral 111 centre of function machine body 106.
Invention described above is not limited to described embodiment certainly.Appreciable, in embodiment illustrated in the accompanying drawings, can implement a large amount of, for professional, hold intelligible deformation program, and can not leave scope of the present invention.For example also can have and exceed the cover cap of two or be that a unique cover cap forms lid 2,102.Also may be considered that, hook connects and 15,115 in the first embodiment, is arranged on first distolateral 10 (instead of in two longitudinal sides 9 at least one on), be arranged in a second embodiment (instead of on first distolateral 110) at least one in two longitudinal sides 109, or for two embodiment, be both arranged on first distolateral 10,110, be also arranged at least one of two longitudinal sides 9,109.Be included in content in instructions and/or that be described in the drawings and different from this specific embodiment but concerning professional hold intelligible content all belong to the present invention.
Claims (13)
1. an electron key (1; 101), it has the function fuselage (6 for laying electric power and electronic component and being configured to housing shape; 106) and at least one Key element (5; 105), this Key element is arranged on this function fuselage (6; It is 106) upper,
It is characterized in that,
Lid (2; 102) by locking mechanism (14; 114) be releasably locked in function fuselage (6; 106) upper, and hide function fuselage (6 completely; 106) at least upside (7; 107) and/or downside (8; 108) on.
2. by electron key (1 claimed in claim 1; 101), it is characterized in that this lid (2; 102) there is at least one and be used for hiding completely upside (7; 107) or downside (8; 108) housing (3,4; 103,104), or this lid (2; 102) have and hide function fuselage (6 completely; 106) upside (7; 107) the first housing (3; 103) and completely hide function fuselage (6; 106) downside (8; 108) the second housing (4; 104).
3. by the electron key (1 described in claim 1 or 2; 101), it is characterized in that this at least one Key element (5; 105) be fixed on function fuselage (6; 107) two longitudinal sides (9; 109) in is upper, and described longitudinal side is by upside (6; 106) and downside (7; 107) couple together.
4. by the electron key (1 described in claim 2 or 3; 101), it is characterized in that locking mechanism (14; 114) comprise at least one and be arranged on function fuselage (6; 106) first distolateral (10; 110) and/or at least one longitudinal side (6; 109) hook on connects (15; 115), and comprise at least one and be arranged on function fuselage (6; 106) second distolateral (11; 111) the sealed connection (16 of shape on; 116), at least one cover cap (3,4; 103,104) mode that connects to clamp by these is releasably arranged on function fuselage (6; 106) on.
5. by electron key (1 claimed in claim 4; 101), it is characterized in that the sealed connection (16 of this at least one shape; 116) be arranged on function fuselage (6 by least one; 106) second distolateral (11; 111) the clamping running-on (22 on; 120) and at least one clamping connect piece (23; 121) form, wherein this clamping connects piece (23; 121) be arranged on this at least one cover cap (3,4; 103,104) near of vertical end (24), this vertical end is arranged on function fuselage (6; 106) second distolateral (11; 111) upper, and this at least one clamping running-on (22; 120) connect piece (23 with respect to this at least one clamping; 121) can overcome elastic reset member (25; 131) power is from latched position activity to off-position, this at least one clamping running-on (22 in this latched position; 120) abut in this at least one clamping and connect piece (23; 121) go up and stoped clamping to connect piece (23; 121) and clamping running-on (22; 120) relative motion between, this at least one clamping running-on (22 in this off-position; 120) discharge this at least one clamping and connect piece (23; 121).
6. by electron key claimed in claim 5 (1), it is characterized in that, this at least one hook connects accommodation section (18) formation that (15) are molded in respectively the snapclose sheet (17) on the longitudinal side (9) of function fuselage (6) and are subordinated to each snapclose sheet (17) by least one, wherein each affiliated accommodation section (18) is molded over corresponding cover cap (3, 4) on longitudinal side (19), and wherein the sealed connection of this at least one type (16) is to form like this, in the direction of second distolateral (11) of function fuselage (6), push corresponding cover cap (3, 4) and thus this at least one snapclose sheet (17) is pressed in this accommodation section (18) kayser.
7. by the electron key (1) described in claim 5 or 6, it is characterized in that, be provided with the steerable sliding component (12 at least one longitudinal side transverse to function fuselage (6) (9), 13), this at least one clamping running-on (22) is arranged on this sliding component, wherein this at least one clamping running-on (22) and this at least one sliding component (12, 13) be also therefore placed in pockets (29, 30) in and at this pockets (29, 30) power that overcomes elastic reset member (25) in can slippage between latched position and off-position, this pockets is molded on second distolateral (11) of function fuselage (6).
8. by electron key claimed in claim 7 (1), it is characterized in that, the first cover cap (3) is equipped with the first sliding component (12) and the second cover cap (4) to be equipped with the second sliding component (13), wherein the first and second sliding components (12,13) comprise respectively clamping running-on (22) and feather key (28), wherein the clamping running-on (22) of the first sliding component (12) be arranged in the first pockets (29) and with the first sliding component (12) be arranged on feather key (28) outside function fuselage (6) in slip couple state, this pockets extends in the direction of the downside (8) of function fuselage (6) from upside (7), wherein the clamping running-on (22) of the first sliding component (12) be arranged in the second pockets (29) and with the second sliding component (13) be arranged on feather key (28) outside function fuselage (6) in slip couple state, this pockets extends in the direction of the upside (7) of function fuselage (6) from downside (8).
9. by electron key claimed in claim 8 (1), it is characterized in that, the first sliding component (12) is arranged in the corner regions of second distolateral (11) of function fuselage (6), and the second sliding component (13) is arranged on the relative with the first sliding component (12) of function fuselage (6) and in the corner regions of putting, wherein the first and second sliding components (12,13) are constructed to such an extent that can mutually move.
10. by electron key claimed in claim 5 (101), it is characterized in that, hook connects (115) and is molded over groove (117) on first distolateral (110) of function fuselage (106) by least one and at least one patches running-on (118) formation, wherein this at least one patch running-on (118) be arranged at least one cover cap (103 on first distolateral (119), 104) on, and wherein these be clamped and connected (116) are to form like this, in the direction of second distolateral (111) of function fuselage (106), push at least one cover cap (103, 104) and thus by this, at least one patches running-on (118) and is pressed in this at least one accommodation section (117).
11. by the electron key (101) described in claim 5 or 10, it is characterized in that, be provided with the sliding component (124) being placed on second distolateral (111), the power that it has this at least one clamping running-on (120) and overcomes elastic reset member (131) between latched position and off-position in the direction of first distolateral (110) slip.
12. by the electron key (101) described in claim 11, it is characterized in that, sliding component (124) is substantially configured to I-shape in xsect, wherein the indirect piece (125) of this I-shape sliding component and feather key (126) are in Flexible coupling state, and stop running-on (129) is transverse to clamping running-on (120) and be oppositely molded in it its vertical end (127 separately, 128), this vertical end is arranged on the upside of function fuselage (106) or downside (127, 128), this stop running-on is used for a sliding component (124) and is fixed on function fuselage (106).
13. by the electron key (101) described in claim 12, it is characterized in that, each stop running-on (129) of the sliding component (124) of I-shape is configured to hook-shaped and catches from behind the stop protuberance (130) being arranged on function fuselage (106), wherein the stop running-on (120) of the sliding component of this I-shape (124) is arranged in the bag container (122) of corresponding cover cap (103,104), and wherein the sidewall (123) of bag container (122) is that the clamping of corresponding cover cap (103,104) connects piece (121).
Applications Claiming Priority (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE102013105535.4 | 2013-05-29 | ||
| DE102013105535 | 2013-05-29 | ||
| DE102013111125 | 2013-10-08 | ||
| DE102013111125.4 | 2013-10-08 | ||
| DE102014100154.0 | 2014-01-08 | ||
| DE102014100154.0A DE102014100154A1 (en) | 2013-05-29 | 2014-01-08 | Electronic key |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104217476A true CN104217476A (en) | 2014-12-17 |
| CN104217476B CN104217476B (en) | 2018-10-09 |
Family
ID=50721630
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410230936.3A Expired - Fee Related CN104217476B (en) | 2013-05-29 | 2014-05-28 | Electron key |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP2808847B1 (en) |
| CN (1) | CN104217476B (en) |
| DE (1) | DE102014100154A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106481148A (en) * | 2016-11-09 | 2017-03-08 | 叶雨玲 | Combined key receives device |
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| DE102007017492A1 (en) * | 2006-04-19 | 2007-10-25 | Marquardt Gmbh | Housing particularly for electronic key of motor vehicle locking system, has two housing parts, and transmitter present in housing for electromagnetic signal, where housing part is made up permeable material for electromagnetic radiation |
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| US6424056B1 (en) * | 2000-11-30 | 2002-07-23 | Telefonaktiebolaget (Lme) | Keyless entry system for a vehicle |
| DE10121045C2 (en) | 2001-04-28 | 2003-03-20 | Huf Huelsbeck & Fuerst Gmbh | Housing for an electronic key |
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| WO2014102005A1 (en) * | 2012-12-29 | 2014-07-03 | Marquardt Gmbh | Housing, in particular for an electronic key |
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2014
- 2014-01-08 DE DE102014100154.0A patent/DE102014100154A1/en not_active Withdrawn
- 2014-05-15 EP EP14168383.9A patent/EP2808847B1/en not_active Not-in-force
- 2014-05-28 CN CN201410230936.3A patent/CN104217476B/en not_active Expired - Fee Related
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| DE19605201B4 (en) * | 1996-02-13 | 2007-04-12 | Marquardt Gmbh | Housing for an electronic key |
| US6594472B1 (en) * | 1999-02-12 | 2003-07-15 | Nokia Mobile Phones Ltd. | Exchangeable radiotelephone covers |
| CN1428737A (en) * | 2001-12-28 | 2003-07-09 | 松下电工株式会社 | Electronic key, electronic lock, electronc key system and key management server |
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| DE102007017492A1 (en) * | 2006-04-19 | 2007-10-25 | Marquardt Gmbh | Housing particularly for electronic key of motor vehicle locking system, has two housing parts, and transmitter present in housing for electromagnetic signal, where housing part is made up permeable material for electromagnetic radiation |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN106481148A (en) * | 2016-11-09 | 2017-03-08 | 叶雨玲 | Combined key receives device |
| CN106481148B (en) * | 2016-11-09 | 2018-11-16 | 泉州格罗特机电设备有限公司 | Combined key storage device |
Also Published As
| Publication number | Publication date |
|---|---|
| EP2808847B1 (en) | 2018-04-11 |
| CN104217476B (en) | 2018-10-09 |
| DE102014100154A1 (en) | 2014-12-04 |
| EP2808847A1 (en) | 2014-12-03 |
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| CF01 | Termination of patent right due to non-payment of annual fee | ||
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Granted publication date: 20181009 |