CN2236119Y - Single-jig measuring machine - Google Patents
Single-jig measuring machine Download PDFInfo
- Publication number
- CN2236119Y CN2236119Y CN 95205936 CN95205936U CN2236119Y CN 2236119 Y CN2236119 Y CN 2236119Y CN 95205936 CN95205936 CN 95205936 CN 95205936 U CN95205936 U CN 95205936U CN 2236119 Y CN2236119 Y CN 2236119Y
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- head
- fuselage
- measuring machine
- gear
- wheel
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- Expired - Fee Related
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Abstract
The single-jig measuring machine of the utility model suits for the measurement of the linear dimension of mechanical parts and belongs to technical field of the mechanical length measurement. Rough and fine gearing mechanisms in the machine head of the utility model use differential wheel systems, a rail system slidingly connected the machine head with the machine body use multistage and rectangular quenching steel rail strips matched with a slide seat pasted with plastic pads in the inner surface, an incidental temperature sensor can be pasted on the measured workpiece, and through an SCM computer apparatus, the measuring result can be compensated for different temperatures according to materials. The utility model has the advantages of large fine tuning gearing ratio and high measuring precision, and the measurement in the production field can acquire or approach to the constant temperature measuring result.
Description
The present invention relates to a kind of single coordinate measuring machine, it is applicable to the dimensional measurement of mechanical component, is specially adapted to measure straight length, the hole shaft diameter, and the mean value and the accuracy of form and position belong to the mechanical length field of measuring technique.
Existing single coordinate measuring machine is mainly by fuselage (1), and base (2) and the head (3) that can move on column fuselage (1) are formed.A kind of head place xsect of single coordinate measuring machine as shown in Figure 1, its fuselage (1) is the square of hollow, be installed with grating scale (9), head is frame shape, moving chi (5) of last dress grating and gauge head (4), head and fuselage add counterweight (8) by wire rope and reach balance by bearing roller (7) relative motion up and down.This measuring machine is simple in structure, manufacture process requirement height, but because configuration aspects, volume is bigger, in addition, and because digital display device is on body, during traverse measurement, the reading inconvenience, and also it is bigger to take the platform area.
Another kind of single measurement of coordinates machine head (3) with respect to the driving mechanism of fuselage (1) motion as shown in Figure 2, by gear (12), worm gear (13), clutch coupling (14), handwheel compositions such as (16), the snap-action and the fine setting of head in the time of can realizing measuring (3).But because structural limitations, ratio of gear is less, and gear shift is also inconvenient, and this machine adopts the dial-up wheel to put initial point, and measurement function is less.
The purpose of this utility model is to design and a kind ofly makes head motion steady, and the fine setting ratio of gear is big, and gear shift is convenient, uses dexterous single coordinate measuring machine;
Improved guide rail mechanism, the structure rigidity is good, and the precision height is wear-resisting, and processing is with low cost easily;
Balance weight mechanism fuses into one counterweight and protective cover, debugs conveniently;
Digital display device is installed on the head, and operation and convenient reading adopt the single-chip microcomputer computer apparatus can carry out multifunctional measuring, realizes that numeral shows and printout, temperature compensation and normal temperature test.
Measurement function of the present utility model realizes above purpose.It is mainly by fuselage (1), base (2), head (3) is formed, grating scale (9) and tooth bar (11) are arranged on the fuselage (1), there is grating to move chi (5) in the head (3), gear (12) and stretch out outside gauge head (4), make thick that gauge head moves up and down, micro-adjusting mechanism is by may command gear (12), the differential gear train of tooth bar (11) relative motion and clutch are formed, train is by modulus, external diameter is identical, and the gear wheel (23) that two different concentrics of the number of teeth are installed side by side, (24) and with its pinion wheel that meshes simultaneously (22) form, clutch can make gear wheel (24) and pinion wheel (22) clutch, when gear (24) and gear (22) when separating, shake handgrip (31), rotate together by the direct driven gear (12) of axle (36), because gear (12) is meshed with tooth bar (11), produce relative motion, thereby make gauge head (4) and head (3) along fuselage (1) fast moving up and down, realize quick coarse adjustment, when gear (24) and pinion wheel (22) engagement, rotate handwheel (32), the pinion wheel (22) that is loaded in the handwheel by axle (25) will produce two motions: the one, and the pinion wheel axle center is around the rotation in gear wheel axle center, the 2nd, the engagement of pinion wheel and gear wheel is rotated, because two gear wheel numbers of teeth differ very little (such as differing) at 1 o'clock, to make two gear wheels produce very little speed discrepancy, connect firmly by trip bolt because of gear wheel (23) and head again, can not rotate, therefore gear wheel (24) will rotate by axle (36) driven gear (12) with minimum rotating speed, realize the fine setting of gauge head, and the handwheel diameter is enough big, the gear wheel number of teeth is abundant, the process and assemble precision obtains quite high trimming precision when higher, in addition, because the number of teeth is many, gearshift is easy, and error is little.
The guide track system that head (3) and fuselage (1) are slidingly connected is made up of the slide carriage mechanism on guide rail mechanism on the fuselage (1) and the head (3).Guide rail mechanism mainly is made of " ∏ " shape guide rail reference for installation (61) that stretches out on the fuselage (1) and the accurate rectangle high rigidity hardened-steel guideway bars (39) of two multistages, the press strips (21) that press-fit thereon.Slide carriage mechanism is mainly by constituting with the slide plate (41) of head one, four " Γ " shape pressing plates (38) that are fixed on the slide plate (41), what the working position of slide plate and pressing plate constituted and two guide rails of fuselage (39) match, two spill slides that certain-length is arranged, the slide inside surface bonding the wear-resisting plastic mattress that self-lubricating property is arranged (40).
Make Weighting system that head (3) steadily moves up and down link to each other with head (3), an end and plumbous counterweight (8) steel band that be connected, that have protective action (51), (54), be supported in guide wheel system (55) on the fuselage (1), be installed on the plumbous counterweight (8) in the fuselage (1) with rectangular enclosure and make steel band (51,54) keep the spring (56) of certain pretension to form by an end.The upper rear of fuselage (1) is provided with the flap (53) of being convenient to install, connect, debug counterweight
Measuring-signal, the command signal of keyboard and the test signal of temperature sensor that processing is transmitted by the moving chi of grating are housed in the head of this measuring machine (3), and the computer apparatus formed of the Single Chip Microcomputer (SCM) system of on display, exporting, it is made up of the printed wire plate (45) that many integration modules (47), (49) and button (50), display screen (60) are housed, socket, cable (37), mount pad and the dial hood etc. that posts facial mask.
The measuring machine temperature-compensated system is formed by being installed on the temperature sensor on the grating scale (9) and being adhered to temperature sensor (63) on the measured workpiece (64), transmission cable, single-chip microcomputer etc., the information that computer is measured sensor compensates calculating by the character of measured material, is demonstrating on the display screen through converting the test data result under the normal room temperature to.
Compared with prior art, outstanding feature of the present utility model and superiority are:
Adopt the differential gear train structure, flexible freely to the fine setting gear shift from manual coarse adjustment, because ratio of gear is big, trimming precision and resolution height have improved the accuracy of test.
Adopt segmentation, rectangle, hardened-steel guideway bar can improve the overall precision of guide rail, short rectangular guideway bar machining reaches high morpheme, dimensional accuracy and surfaceness easily, the precision of whole piece guide rail only needs to be reached by the artificial treatment reference for installation, therefore can reach very high overall precision, the correct grinding hardened-steel guideway cooperates with plastics slide on the head, rigidity, better stable, the life-span is long, and friction factor is little.
Adopt the rectangle fuselage to add " ∏ " shape guide rail reference for installation, improved the guide rail rigidity, and the installation site of counterweight, grating chi, tooth bar is provided, compact conformation, volume are reduced.
Balance weight hanging is on steel band, and there is the spring pretension in guide wheel steel band mechanism, has improved the stationarity of counterweight, and steel band plays protective action to grating, tooth bar and cable.
The single-chip microcomputer computer apparatus can be realized multifunctional testing, can not only realize that numeral shows, and can ask the center of circle, and ask diameter, average, the conversion metric and English has functions such as setting, removing, memory, modification, storage, printing, metric and English measurement.Temperature compensation is this machine functions peculiar, and it can make machine serve in the production scene, obtains the test result under the constant temperature, has overcome the influence of temperature variation to test.
Accompanying drawing 3--5 has expressed a specific embodiment of the present utility model.
Fig. 1. a kind of primary structure synoptic diagram of single coordinate measuring machine,
Fig. 2. a kind of finely and widely adjusting means synoptic diagram of single coordinate measuring machine,
Fig. 3. the stereographic map of single coordinate measuring machine,
Fig. 4. head inner structure figure,
Fig. 5. the balance weight mechanism synoptic diagram.
As Fig. 3--the measuring machine shown in 5, main body by column fuselage (1), base (2), have gauge head (4) and can form with being intended to the head (3) that fuselage (1) front portion moves up and down.
The inner rectangular cavity of fuselage (1), the front portion is two guide rail reference for installation (61) of " ∏ " font, two accurate rectangular guidewaies on it are formed by multistage guide rail bar (39) butt joint, and firmly be installed on the benchmark (61) by screw (42), press strip (21), pin etc., grating scale (9) and tooth bar (11) are contained in neutral gear position between two guide rails respectively, the upper and lower part of fuselage (1) is installed with the bracing frame of steel band guide wheel (55) respectively, and fuselage afterbody has one flap (53) is installed.
Base (2) is made up of base body and cushion block, two row's screw holes are arranged on the vertical mount pad of base body, body (1) can be installed, in the lower cavity of base body electric component is installed, three cushion block and the contact with platform of base body by being installed in the bottom is pasted with the wear-resistant plastic pad on the cushion block.
Head (3) is made up of slide carriage mechanism, gauge head installing mechanism, thick fine adjustment transmission mechanism, computer plug-in card installing mechanism, dial hood etc.Slide carriage mechanism is by slide plate (41), four " Γ " shape pressing plates (38) that symmetry is installed and mounting screw (43) are formed, be pasted with the wear-resistant plastic pad at slide plate (41) and pressing plate (38) with (1) two guide rail contact site of fuselage, the gauge head installing mechanism is by gauge head (4), measuring head base, gripping sleeve, compositions such as lock screw, thick fine adjustment transmission mechanism is by gear (12) tooth bar (11) transmission, differential gear train, clutch, compositions such as handwheel, differential gear train is by gear (22), (23), (24), little axle (25), back-up ring (35), axle (36), jackscrew (34), trimming hand wheel (32) is formed, the long cover part of gear (23) is fixed on the head slide plate (41) by jackscrew (34), gear (22) is enclosed within on the little axle (25) that is loaded on trimming hand wheel (32), and mesh simultaneously with gear (23) (24), when trimming hand wheel (32) rotates, rotate in the thorny axle center of taking turns of little axle (25), gear (22) rotates around little axle (25), therefore, pinion wheel (22) is made pure rolling on gear (23) (24), driven gear (24) is done minor rotation, when gear (24) was thrown off with gear (22), fine setting was no longer worked.Clutch is by handle (28), wheel disc (30), screw (29), can go up the clutch body (20) that slides at axle (36), the pin (27) that axle (36) and clutch body (20) are rotated together, control clutch body (20) is gone up the elastic positioning device (26) of sliding stroke [by spring at axle (36), steel ball, jackscrew constitutes] etc. composition, screw (29) is the wheel disc (30) of band handgrip (31), clutch body (20), gear (24) is fixed on one, when being pulled outwardly wheel disc (30) with handle (28), clutch body (20) outwards slides along axle (36), elastic positioning device (26) makes its position that slides into that gear (24) and gear (22) are thrown off, when rotating handwheel by handgrip (31), because the cause of pin (27) in clutch body keyway, thereby can drive axle (36) and gear (12) along tooth bar (11) fast moving, in like manner, when gear (24) meshes with gear (22), the minor rotation that gear (24) obtains, also pass to rack-and-pinion through axle (36) by clutch body (20), realize that the low speed fine setting is mobile, computer plug-in card installing mechanism is by display screen (60) is installed, the panel of pilot lamp and keyboard, CPU board (45) with various chips (47) (49), the socket of band transmission cable (37), mount pad and dial hood are formed, two orthogonal display screens (60), regularly arranged keyboard (50), rationally thick trimming hand wheel of placing and the panel that is designed beautifully have constituted the outward appearance assembly of the head (3) of measuring machine.
The Weighting system of head is made up of upper and lower steel band (51), (54), pressing plate (57), guide wheel (55), guide wheel shaft, bearing, preloading spring (56), upper and lower counterweight (8) and counterweight mounting screw (52), upper and lower (51), (54) one of steel band links to each other with the head upper and lower end respectively, the other end is then strained by preloading spring (56) by pressing plate (57), balance weight hanging is on the pressing plate (57) of spring (56) upper end, and the flap of back (53) is used for installation, the debugging of counterweight (8) and spring (56).
In addition, measuring machine is subsidiary the temperature sensor (63) of Pasting on measured workpiece, and also there is the temperature sensor of a dip stick temperature head inside, they link to each other with computer respectively, temperature information is separately sent into computer, and former test result is revised in the back as calculated, shows on display screen.
Measuring machine has memory function, but deposits while surveying in the measurement, and the base bottom is provided with printer interface, the printer (62) of can pegging graft, and measurement result printed.
Claims (5)
1, a kind of single coordinate measuring machine that is applicable to the measurement mechanical accessory size, by comprising head, fuselage, the guide track system that is slidingly connected between head and the fuselage, the balance weight mechanism that head is steadily moved up and down, the grating scale, grating moves chi, compositions such as gauge head and measurement result display device, it is characterized in that: it is thick to realize that gauge head moves up and down, micro-adjusting mechanism is by being installed in the head, may command makes compositions such as the differential gear train of rack-and-pinion relative motion of head fuselage relative motion and its clutch, differential gear train is by modulus, external diameter is identical, and the gear wheel (23) that two different concentrics of the number of teeth are installed side by side, (24) and with its pinion wheel that meshes simultaneously (22) form, clutch can make gear wheel (24) and pinion wheel (22) clutch.
2, measuring machine according to claim 1, it is characterized in that: the guide track system that is slidingly connected between head and the fuselage, form by guide rail mechanism on the fuselage and the slide carriage mechanism on the head, guide rail mechanism is by " ∏ " shape guide rail reference for installation (61) that stretches out on the fuselage (1), press-fit two rectangular guideway bars (39) thereon, four " Γ " shape press strip formations such as (21), slide carriage mechanism by and the slide plate (41) of head (3) one, pressing plate formations such as (38), wherein, the guide rail bar can be high rigidity hardened steel or form by multistage, the spill slide inside surface that slide plate and pressing plate constitute can the bonding wear-resisting plastic mattress that self-lubricating property is arranged (40).
3, according to the measuring machine of claim 1 or 2, it is characterized in that: the balance weight mechanism that head (3) is steadily moved up and down, by an end link to each other with head (3), an end and plumbous counterweight (8) steel band that join, that have protective action (51), (54), guide wheel system (55), the lead that is arranged in fuselage (1) rectangular enclosure cooperates (8), preloading spring (56) etc. to form.
4, according to the measuring machine of claim 1 or 2, it is characterized in that: the measurement result display device is to be realized by the single-chip microcomputer computer apparatus that is located in the head, and it is by comprising that polylith integrated circuit board (45), cable (37), a plurality of button (50) and two display screens (60) etc. that can realize various functions form.
5, according to the measuring machine of claim 4, it is characterized in that: the measurement result temperature-compensated system is formed by being installed on the temperature sensor on the grating scale (9) and can being adhered to temperature sensor (63) on the measured workpiece (64), transmission cable, single-chip microcomputer etc.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 95205936 CN2236119Y (en) | 1995-03-22 | 1995-03-22 | Single-jig measuring machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 95205936 CN2236119Y (en) | 1995-03-22 | 1995-03-22 | Single-jig measuring machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2236119Y true CN2236119Y (en) | 1996-09-25 |
Family
ID=33858019
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 95205936 Expired - Fee Related CN2236119Y (en) | 1995-03-22 | 1995-03-22 | Single-jig measuring machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2236119Y (en) |
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| CN102713499A (en) * | 2010-01-20 | 2012-10-03 | 法罗技术股份有限公司 | Counter balance for coordinate measurement device |
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| US8537374B2 (en) | 2010-01-20 | 2013-09-17 | Faro Technologies, Inc. | Coordinate measuring machine having an illuminated probe end and method of operation |
| US8607536B2 (en) | 2011-01-14 | 2013-12-17 | Faro Technologies, Inc. | Case for a device |
| US8615893B2 (en) | 2010-01-20 | 2013-12-31 | Faro Technologies, Inc. | Portable articulated arm coordinate measuring machine having integrated software controls |
| US8630314B2 (en) | 2010-01-11 | 2014-01-14 | Faro Technologies, Inc. | Method and apparatus for synchronizing measurements taken by multiple metrology devices |
| US8677643B2 (en) | 2010-01-20 | 2014-03-25 | Faro Technologies, Inc. | Coordinate measurement machines with removable accessories |
| US8832954B2 (en) | 2010-01-20 | 2014-09-16 | Faro Technologies, Inc. | Coordinate measurement machines with removable accessories |
| US8875409B2 (en) | 2010-01-20 | 2014-11-04 | Faro Technologies, Inc. | Coordinate measurement machines with removable accessories |
| US8898919B2 (en) | 2010-01-20 | 2014-12-02 | Faro Technologies, Inc. | Coordinate measurement machine with distance meter used to establish frame of reference |
| US8997362B2 (en) | 2012-07-17 | 2015-04-07 | Faro Technologies, Inc. | Portable articulated arm coordinate measuring machine with optical communications bus |
| US9074883B2 (en) | 2009-03-25 | 2015-07-07 | Faro Technologies, Inc. | Device for optically scanning and measuring an environment |
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| USRE45854E1 (en) | 2006-07-03 | 2016-01-19 | Faro Technologies, Inc. | Method and an apparatus for capturing three-dimensional data of an area of space |
| US9329271B2 (en) | 2010-05-10 | 2016-05-03 | Faro Technologies, Inc. | Method for optically scanning and measuring an environment |
| US9372265B2 (en) | 2012-10-05 | 2016-06-21 | Faro Technologies, Inc. | Intermediate two-dimensional scanning with a three-dimensional scanner to speed registration |
| US9417316B2 (en) | 2009-11-20 | 2016-08-16 | Faro Technologies, Inc. | Device for optically scanning and measuring an environment |
| US9417056B2 (en) | 2012-01-25 | 2016-08-16 | Faro Technologies, Inc. | Device for optically scanning and measuring an environment |
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| US9607239B2 (en) | 2010-01-20 | 2017-03-28 | Faro Technologies, Inc. | Articulated arm coordinate measurement machine having a 2D camera and method of obtaining 3D representations |
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-
1995
- 1995-03-22 CN CN 95205936 patent/CN2236119Y/en not_active Expired - Fee Related
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| USRE45854E1 (en) | 2006-07-03 | 2016-01-19 | Faro Technologies, Inc. | Method and an apparatus for capturing three-dimensional data of an area of space |
| US9074883B2 (en) | 2009-03-25 | 2015-07-07 | Faro Technologies, Inc. | Device for optically scanning and measuring an environment |
| US9551575B2 (en) | 2009-03-25 | 2017-01-24 | Faro Technologies, Inc. | Laser scanner having a multi-color light source and real-time color receiver |
| US9417316B2 (en) | 2009-11-20 | 2016-08-16 | Faro Technologies, Inc. | Device for optically scanning and measuring an environment |
| US8630314B2 (en) | 2010-01-11 | 2014-01-14 | Faro Technologies, Inc. | Method and apparatus for synchronizing measurements taken by multiple metrology devices |
| CN102713499B (en) * | 2010-01-20 | 2014-07-09 | 法罗技术股份有限公司 | Counter balance for coordinate measurement device |
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| US8615893B2 (en) | 2010-01-20 | 2013-12-31 | Faro Technologies, Inc. | Portable articulated arm coordinate measuring machine having integrated software controls |
| US10060722B2 (en) | 2010-01-20 | 2018-08-28 | Faro Technologies, Inc. | Articulated arm coordinate measurement machine having a 2D camera and method of obtaining 3D representations |
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| US9607239B2 (en) | 2010-01-20 | 2017-03-28 | Faro Technologies, Inc. | Articulated arm coordinate measurement machine having a 2D camera and method of obtaining 3D representations |
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| US9329271B2 (en) | 2010-05-10 | 2016-05-03 | Faro Technologies, Inc. | Method for optically scanning and measuring an environment |
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| US9168654B2 (en) | 2010-11-16 | 2015-10-27 | Faro Technologies, Inc. | Coordinate measuring machines with dual layer arm |
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| US9417056B2 (en) | 2012-01-25 | 2016-08-16 | Faro Technologies, Inc. | Device for optically scanning and measuring an environment |
| US8997362B2 (en) | 2012-07-17 | 2015-04-07 | Faro Technologies, Inc. | Portable articulated arm coordinate measuring machine with optical communications bus |
| US10067231B2 (en) | 2012-10-05 | 2018-09-04 | Faro Technologies, Inc. | Registration calculation of three-dimensional scanner data performed between scans based on measurements by two-dimensional scanner |
| US9739886B2 (en) | 2012-10-05 | 2017-08-22 | Faro Technologies, Inc. | Using a two-dimensional scanner to speed registration of three-dimensional scan data |
| US9746559B2 (en) | 2012-10-05 | 2017-08-29 | Faro Technologies, Inc. | Using two-dimensional camera images to speed registration of three-dimensional scans |
| US9372265B2 (en) | 2012-10-05 | 2016-06-21 | Faro Technologies, Inc. | Intermediate two-dimensional scanning with a three-dimensional scanner to speed registration |
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| US9513107B2 (en) | 2012-10-05 | 2016-12-06 | Faro Technologies, Inc. | Registration calculation between three-dimensional (3D) scans based on two-dimensional (2D) scan data from a 3D scanner |
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