WO2001094200A1 - Aeronef comportant plusieurs cabines superieures et inferieures faisant office de compartiment a marchandises ou de cabines a passagers, et procede de chargement de marchandises sur un aeronef - Google Patents
Aeronef comportant plusieurs cabines superieures et inferieures faisant office de compartiment a marchandises ou de cabines a passagers, et procede de chargement de marchandises sur un aeronef Download PDFInfo
- Publication number
- WO2001094200A1 WO2001094200A1 PCT/JP2001/004726 JP0104726W WO0194200A1 WO 2001094200 A1 WO2001094200 A1 WO 2001094200A1 JP 0104726 W JP0104726 W JP 0104726W WO 0194200 A1 WO0194200 A1 WO 0194200A1
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- Prior art keywords
- luggage
- cabin
- aircraft
- compartment
- port
- Prior art date
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/18—Floors
- B64C1/20—Floors specially adapted for freight
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D11/00—Passenger or crew accommodation; Flight-deck installations not otherwise provided for
- B64D11/04—Galleys
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0018—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only
- B64C2001/0027—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only arranged one above the other
Definitions
- the present invention relates to an aircraft having a plurality of upper and lower layers of cabins functioning as a luggage compartment or a cabin on a fuselage, and to facilitate loading of luggage and a method of loading luggage on the aircraft.
- Figure 25 is a schematic perspective view of a freighter that carries air cargo
- Figure 26 is a cross-sectional view of the freighter (a cross-sectional view perpendicular to the longitudinal direction of the fuselage).
- 1 is the fuselage of the aircraft
- 2 is the main wing
- 3 is the tail.
- such a cargo aircraft is divided into an upper luggage compartment 10 and a lower luggage compartment 11 by a partition wall 14 extending in the longitudinal direction of the fuselage.
- Each of the lower luggage compartments 11 has luggage ports 0 2 3 and 2 3 which are opened and closed by luggage doors 0 1 2 and 1 2.
- the cargo machine has the luggage port 0 23 at one place at the front or rear of the fuselage 1 and the luggage port 23 at two places at the front and rear. .
- Luggage doors 1 and 2 and luggage doors 23 are provided on ordinary passenger aircraft to carry passenger luggage and paid luggage.
- the luggage when loading the luggage 13, the luggage is loaded into the upper luggage room 10 from the luggage port 0 2 3 opened in the upper luggage room 10, and the luggage 13 is placed on the upper floor 28. It is transported to a predetermined position in the upper luggage compartment '10 by a conveyor (not shown) extending in the longitudinal direction of the fuselage.
- a baggage is loaded into the lower luggage compartment 11 from a luggage port 23 opened in the lower luggage compartment 11, and a conveyor (not shown) is installed on the lower floor 19 to extend in the machine longitudinal direction.
- a conveyor (not shown) is installed on the lower floor 19 to extend in the machine longitudinal direction.
- the reverse operation is performed.
- the upper luggage compartment 10 and the lower luggage compartment 11 are respectively provided with luggage openings (0 2 3 and 2) opened and closed by the luggage doors (0 1 2 and 1 2), respectively. 3) It is configured to load or unload luggage from.
- the luggage door (0 1 2 or 1 2) that opens and closes the luggage port (0 2 3 or 2 3) has the same thickness and material as the fuselage 1 but has no notch in the door. Since it is necessary to have the same strength, it will be heavy and the pressure difference and temperature between the luggage door (0 1 2 or 1 2) and the luggage port (0 2 3 or 2 3) Since it is necessary to precisely seal the inside and outside of the aircraft with a large difference, it takes a lot of assembly man-hours to provide a luggage door (0 1 2 or 1 2) that opens and closes the luggage opening (0 2 3 or 2 3). And material costs are required.
- the luggage door which opens and closes the luggage port (0 2 3 or 2 3) which requires a large amount of assembly man-hours and material costs as described above. (0 1 2 or 1 2) is installed in both the upper luggage compartment 10 and the lower luggage compartment 11, which increases the cost of the aircraft, especially when retrofitting passenger aircraft to cargo aircraft The renovation man-hours are large and the cost of renovation is high.
- FIG. 24 is a partial cross-sectional plan view of a passenger aircraft according to the prior art.
- the passenger aircraft has gear train service spaces 505, 506 where the steedes work to serve food and drink in the passenger seat row in front of the center wing 525 of the fuselage 500, and on the rear side.
- a gear service space 507 is provided.
- the gear race service space 505, 506, 507 is equipped with wagons containing service goods, and service goods before landing at the destination in order to service passengers after the takeoff of the passenger aircraft. Is consumed and must be replaced with a wagon containing new service items while parked. At the time of the replacement, a new wagon from the gear service vehicle 503 was replaced from the emergency exit on the same floor as the passenger cabin.
- an object of the present invention is to provide a function of carrying luggage to each layer and a function of carrying luggage from each layer in an aircraft having a cabin functioning as a luggage room or a cabin in a fuselage and having a plurality of upper and lower cabins.
- the number of luggage entrances and luggage doors for loading and unloading luggage and the number of luggage doors are reduced without reducing the cost of the fuselage.
- Another object of the present invention is to provide a device and a method that can significantly reduce the number of remodeling steps and costs without requiring additional doors and luggage openings.
- Another object of the present invention is to provide a service for food and drink using a wagon according to the prior art so that the service can be performed for passengers after the airplane takes off and before landing at the destination.
- Goods are consumed and must be replaced with a wagon containing new service items while parked, and a new wagon from a gear train service car must be used on the same floor path as the passenger cabin when replacing the wagon
- Aircraft can be operated in the same time zone as passenger disembarkation time, shortening the time for passenger aircraft to park on the ground, enabling more flights to operate at a given time, reducing passenger waiting time, and airlines
- the purpose of the present invention is to provide an apparatus and a method that aim to improve the profitability of passengers and the convenience of passengers.
- the present invention relates to an aircraft having a cabin functioning as a luggage compartment or a cabin in a plurality of upper and lower layers, a first cabin having a luggage-only opening at a fuselage position facing the luggage compartment, which is opened and closed by a door that shields the outside of the aircraft.
- the luggage carried into the first cabin via the luggage exclusive port can be transferred to a second cabin that does not have the luggage exclusive opening directly above or immediately below, and the luggage from the second cabin can be transferred to the second cabin.
- a lift device configured to be transported to the first cabin is provided, and the load is carried in and out between the outside of the machine and the second cabin through the dedicated baggage port.
- the present invention uses the luggage port (luggage port) already provided on the aircraft, allowing luggage to be taken in and out of the luggage port, and opened and closed by a door that shields the outside from the fuselage position facing the luggage compartment.
- the loading / unloading of cargo is carried out between a first cabin having a dedicated baggage port to be loaded and a second cabin having no baggage dedicated port by a lifting device.
- a special luggage port is newly provided in the cabin that functions as a luggage compartment, so that the strength of the fuselage is not reduced, and for loading and unloading luggage without lowering the luggage loading and unloading functions.
- Aircraft costs can be reduced by reducing the number of luggage openings and luggage doors.
- the luggage can be loaded and unloaded without using the same floor of the cabin where passengers come and go during the same period of time as lifts and gets off.
- the luggage exclusive opening which is opened and closed by a door is provided to constitute the first cabin, and the first cabin is provided near the exclusive luggage opening.
- the lift device for transferring the cargo between the cabin of the first and the second cabins on the upper layer side may be provided,
- the cabin functioning as the luggage compartment When the cabin functioning as the luggage compartment is provided above and below the fuselage of the aircraft in a three-layer structure, the cabin functioning as a lower luggage compartment and the cabin functioning as a middle cargo compartment located immediately above the cabin.
- An elevator for transporting luggage between the first cabin functioning as the middle luggage room and the second cabin functioning as the uppermost luggage room, provided with a dedicated luggage port and configured as the first cabin. May be provided.
- a luggage port which is opened and closed by a door is provided only in the lower luggage compartment, the luggage is carried into the aircraft from the luggage port, and the luggage is vertically moved by the lifting device from the lower luggage port.
- the loading of cargo to the aircraft from the outside can reduce the height of lifting cargo from the ground, so that the cost of the cargo loading equipment on the ground can be reduced and the cargo Safety can be improved. Therefore, according to the invention, it is only necessary to provide one or a minimum number of doors for opening and closing the luggage port, which are heavy objects having the same thickness and material as the fuselage, and require an elaborate seal. Assembly man-hours and material costs are greatly reduced.
- the existing luggage port and door opened in the lower luggage compartment will be diverted, and the lift will be moved to the vicinity or to the luggage compartment of the same layer as the existing luggage compartment. If a device is provided, the luggage carried in from the existing luggage port can be easily transported to the upper luggage compartment by vertically moving the luggage device, and a new luggage port and a new luggage port can be transferred. It is not necessary to provide a door that opens and closes, and the renovation man-hour and cost can be reduced.
- each of the cabins of the plurality of tiers can receive and transfer luggage with the elevating device, and corresponds to luggage transferred by the elevating device. It is preferable to provide a horizontal transfer means for transferring the layer horizontally into the luggage compartment.
- the luggage port is provided at a plurality of locations in the corresponding luggage compartment, and the lifting device is provided near each of the luggage ports. According to this configuration, the load can be loaded and unloaded from a plurality of luggage openings provided in the front-rear direction of the fuselage, thereby further improving the work efficiency of loading the load.
- the lifting device comprises: a luggage stand on which luggage is loaded; an extendable link mechanism connected to a lower portion of the luggage stand and capable of extending and retracting in the vertical direction of the body; It may be configured to include an actuator for moving vertically, a luggage stand on which luggage is loaded, a rope connected to the luggage stand, and a rope for vertically moving the luggage and the rope are hung.
- a pulley and a drive unit connected to the rope and winding or unwinding the rope to move the luggage stand in the vertical direction of the vehicle body may be provided.
- the rope is connected to a luggage stand on which the load is loaded, and the rope is connected to a driving device via a slide, and the rope is wound or unreeled by the driving device. Since the platform is configured to be moved in the vertical direction of the fuselage, it is easy to increase the vertical movement height, and even in a cargo machine with three or more luggage compartments, luggage ports are provided for each layer. It is not necessary to provide The minimum number is required, and the reduction in the number of assembling steps and material costs of the fuselage becomes even more significant.
- the cabin functioning as the luggage compartment is partitioned by a partition wall, a drive source and a gear connected to the drive source are provided in the lift device, and a moving area of the lift device is driven before the lift device is driven. It is also an effective means of the present invention that the guide means for guiding the elevating and lowering device and the rack which engages with the gear are stored in the partition wall.
- a drive source and a gear connected to the drive source are provided in the lift device, the cabin functioning as the luggage compartment is partitioned by a partition wall, and the lift device is driven in the partition wall.
- a guide unit that guides the elevating device before driving the elevating device, and a moving mechanism that moves the elevating device such as a rack that engages with the gear.
- a gear service space is provided in the second cabin that functions as a guest room, and the elevating device that can move between the gear service space and the first cabin is provided.
- the present invention may also be configured such that, in the gear service space, luggage can be loaded or unloaded in the elevating device, and the load can be carried in and out between the gear service space and the outside. Is an effective means.
- a wagon can be carried in / out via the luggage port of the luggage compartment of the layer provided with a luggage port, and this wagon can be moved to the second cabin which functions as a passenger cabin by means of elevating means in the fuselage.
- FIG. 1 is a side view of a main part of a cargo loading device for a cargo machine according to a first embodiment of the present invention.
- FIG. 2 is a sectional view taken along line AA of FIG.
- FIG. 3A is a perspective view of the elevating device
- FIG. 3B is a cross-sectional view taken along line C-C of FIG.
- FIG. 4 is a diagram corresponding to FIG. 1 showing the second embodiment.
- FIG. 5 is a cross-sectional view of a principal part along the fuselage center line showing the third embodiment.
- FIG. 6 is a sectional view taken along line BB of FIG.
- FIG. 7 is a schematic perspective view of a freighter that performs air transportation of luggage according to the fourth embodiment.
- FIG. 8 is a sectional view taken along the line DD of FIG.
- FIG. 9 is a first perspective view of an elevating device according to a fourth embodiment.
- FIG. 10 is a second perspective view of the lifting apparatus according to the fourth embodiment.
- FIG. 11 is a third perspective view of the lifting device according to the fourth embodiment.
- FIG. 12 is a fourth perspective view of the lifting device according to the fourth embodiment.
- FIG. 13 is a fifth perspective view of the elevating device according to the fourth embodiment.
- FIG. 14 is an explanatory view illustrating an opening and closing device for an opening and closing floor according to a fourth embodiment.
- C FIG. 15 is an explanatory view illustrating a fixing device for a lower end of a guide rail according to the fourth embodiment.
- FIG. 16 is an explanatory diagram illustrating a stored state of the guide rail according to the fourth embodiment.
- FIG. 17 is an explanatory diagram illustrating a main part of a guide rail according to a fourth embodiment.
- FIG. 18 is an explanatory diagram illustrating the driving operation of the guide rail according to the fourth embodiment to the retracted state and the lowered state.
- FIG. 19 is an explanatory diagram for explaining a method of driving the lifting device according to the fourth embodiment. It is.
- FIG. 20 is an explanatory second diagram for explaining a method of driving the elevating device according to the fourth embodiment.
- FIG. 21 is a third explanatory diagram illustrating a method of driving the elevating device according to the fourth embodiment.
- FIG. 22 is a schematic sectional view of a passenger aircraft according to the fifth embodiment.
- FIG. 23 is a perspective view of an elevating device according to a fifth embodiment.
- FIG. 24 is a partial cross-sectional plan view of a passenger aircraft according to the related art. .
- FIG. 25 is a schematic perspective view of a freighter for carrying cargo by air according to the related art.
- FIG. 26 is a cross-sectional view of a freighter according to the related art. BEST MODE FOR CARRYING OUT THE INVENTION
- FIG. 1 is a side view of a main part of a cargo loading device of a cargo machine according to a first embodiment of the present invention
- FIG. 2 is a sectional view taken along line AA of FIG. 1
- FIG. 3 is a perspective view of a lifting device.
- FIG. 4 is a diagram corresponding to FIG. 1 showing the second embodiment
- FIG. 5 is a cross-sectional view of a main part along the fuselage center line showing the third embodiment
- FIG. FIG. 3 is a sectional view taken along line B.
- reference numeral 1 denotes a fuselage, and the inside of the fuselage 1 is formed by a partition wall 14 extending in the longitudinal direction of the fuselage. 10 and lower luggage compartment 11 on the lower side.
- Reference numeral 23 denotes a lower luggage port that opens to the lower luggage compartment 11; 12 denotes a luggage door that opens and closes the lower luggage port 23.
- the lower luggage port 23 and the luggage door 12 are shown in FIG. As shown in the figure, one location is provided near the front of the aircraft.
- the elevating device 15 vertically lifts the luggage 13 carried into the lower luggage compartment 11 and transfers it to the upper luggage compartment 10, the details of which will be described later.
- Reference numeral 17 denotes a lower-layer room conveyor extending in the longitudinal direction of the machine on the lower-layer floor surface 19 of the lower-layer baggage room 11, which is close to the lower-layer baggage port 23, and whose front end is close to the elevating device 15.
- the baggage 13 provided in contact with the lower baggage port 23 can be transported onto the elevating device 15.
- Reference numeral 16 denotes an upper-layer room conveyor extending in the longitudinal direction of the fuselage on the upper-layer floor surface 28 of the upper-layer luggage compartment 10 so that a front end thereof is close to an opening 24 in which the elevating device 15 is provided. It is provided so that it can receive the luggage transferred by the elevating device 15 and transfer it into the upper luggage room 10.
- Fig. 3 (a) and (b) which show the first example of the Mae Xiao 3 lifting device 15
- 152 is a luggage stand on which luggage is placed on the upper surface
- 153 is a pair of crosslinks The center of each cross link 153 is rotatably connected by a pin 155.
- the upper end of the cross link 15 3 is rotatably supported on both side surfaces 25 2 of the luggage stand 15 2 via pins 15 4.
- Rollers 255 are rotatably supported at the lower ends of the cross links 15 3 via pins 15 4, and each roller 255 is mounted on a floor 26 2 in the lower luggage compartment 11.
- the elevating device 15 moves in the lower luggage compartment 11 in the longitudinal direction. .
- a pin 154 is slidably fitted in a hole 153a formed in each of the upper end portions of the cross link 153.
- a roller 161 is rotatably fitted to the root of the 154.
- the roller 16 1 rolls along a groove 16 0 carved in the same direction as the rail 260 on both sides of the load table 15 2.
- the roller 161 moves along the groove 160 as 52 moves up and down due to the expansion and contraction of a hydraulic cylinder 151, which will be described later.
- 1 6 2 and 1 6 3 are snap rings for retaining.
- Reference numeral 156 denotes a crossbar, which is rotatably connected to the lower end of the pair of crosslinks 153 by a pin 157 so as to connect the lower ends of the crosslink 153.
- Reference numeral 151 denotes a hydraulic cylinder, which is interposed between the two crossbars 156 and 156 so as to be extendable and contractible.
- the hydraulic cylinder 151 is provided with fixing means, such as a magnet, a suction cup, and a port, for fixing the hydraulic cylinder 15 to the floor surface when the elevating device 15 is operated. It should be noted that a pneumatic cylinder, an electric actuator, or the like may be used instead of the hydraulic cylinder 151.
- the luggage 13 when the luggage 13 is loaded in the cabin, as shown by an arrow in FIG. 2, the luggage 13 is placed in the lower luggage port 23 provided in the lower luggage room 11. Then, the lower chamber conveyor 17 is driven, and the lower chamber conveyor 17 is driven to move horizontally to the position of the elevating device 15 as shown by the arrow in FIG.
- the lower room conveyor 17 on which the luggage 13 is mounted is provided.
- the luggage 13 may be moved horizontally and transported to a predetermined place.
- a luggage port (lower luggage port 2 3) is provided only in the lower luggage compartment 11 provided on the lower side of the fuselage 1, and luggage 13 is transferred from the lower luggage port 23.
- Carrying in the aircraft and carrying it into the upper luggage compartment (upper luggage compartment 10) can be performed by vertically moving the luggage 13 from the lower luggage port 23 with the lifting device 15. This eliminates the need to provide a luggage port that can be opened and closed by the luggage door in each of the upper luggage compartment 10 and the lower luggage compartment 11 as in the prior art.
- the luggage 13 stored in both the lower luggage compartment 11 and the upper luggage compartment 10 can be loaded and unloaded.
- a luggage door 23 for opening and closing the luggage port 23 is a heavy object having the same thickness and material as the fuselage 1 and requiring an elaborate seal. Alternatively, it is sufficient to provide a minimum number of parts, and the man-hour for assembling the body and the material cost are greatly reduced.
- the existing luggage port (luggage-only port) and luggage door that are open in the lower luggage compartment 11 will be diverted, and the elevating device 15 will be installed near this. Then, the luggage carried in from the existing luggage port can be easily transported to the upper luggage compartment 10 by vertically moving the luggage by the elevating device 15, and a new luggage port and luggage door are provided. It is possible to reduce the number of renovation steps and cost.
- FIG. 4 a second embodiment shown in FIG. 4 will be described.
- the lifting device 15 is arranged in front of the cargo aircraft, whereas the second embodiment is equipped with one lifting device 15 in front and behind the cargo aircraft.
- the luggage port 23 and the luggage door 12 are provided at two places before and after the lower luggage compartment 11 as shown in FIG.
- the lower-stage conveyor 17 and the upper-stage conveyor 16 are provided between the elevating units 15 and 15 in the lower-stage luggage room 11 and the upper-stage luggage room 10, respectively. I have.
- the load 13 can be loaded and unloaded from the luggage openings 23 provided at the front and rear, thereby improving the work efficiency of loading the load.
- Other configurations are the same as those of the first embodiment.
- FIG. 5 The difference from the first and second embodiments is that the first and second embodiments have a lifting device constituted by a luggage stand, a cross link, and a hydraulic mechanism, whereas the third embodiment has Is composed of a morning and evening meal.
- Reference numeral 20 denotes an elevating device for elevating and lowering these three luggage compartments 11, 21 and 10 and is configured as follows.
- reference numeral 201 denotes a luggage stand on which luggage 13 is mounted on the upper surface, which is mounted on a pulley 202 rotatably mounted at four (or more than five) positions at its end.
- the opening and closing holes 24 and 25 formed in the partition walls 14 and 14 are lifted and lowered. ing.
- Reference numeral 203 denotes a pulley rotatably attached to four places on the upper wall of the upper luggage compartment 10.
- the pulley 202 is provided corresponding to the pulley 202 of the luggage stand 201, and the pulley 202 is provided.
- the ropes 204 and 205 from above are bridged.
- Reference numerals 206 and 206 denote two elevators provided in the longitudinal direction of the fuselage, which use an electric motor or the like, and are provided with two ropes 204 and 2 which are wound around the pulleys 203 and 203.
- the luggage carrier 201 is moved up and down by winding or unwinding the ropes 204 and 205.
- the middle luggage compartment 21 has a middle luggage compartment 22 and although a luggage door 12 for opening and closing the door is provided, the middle-layer luggage door 22 and the luggage door 12 for opening and closing the middle luggage door may be omitted.
- the ropes 204, 205 are connected to the luggage stand 201 on which the load 13 is mounted, and the ropes 204, 205 are connected to the pulleys 202, 200.
- the luggage stand 201 is moved in the vertical direction of the vehicle by connecting or disconnecting the ropes 204 and 205 with the elevator 206 through the elevator 3 by way of 3. Therefore, it is easy to increase the vertical movement height, so that not only a three-layer luggage compartment as in this embodiment, but also a four- or There is no need to provide a luggage port, and the number of luggage ports and luggage doors is minimal, and the reduction in the number of assembling steps and material costs of the aircraft will be more significant.
- loading into the upper luggage compartment can be performed by vertically moving the luggage from the lower luggage port by the elevating device.
- the existing luggage port and door that are open to the lower luggage compartment are diverted, and if the lifting device is installed near this, the existing luggage port will be used.
- the lifting / lowering device By moving the loaded luggage vertically by the lifting / lowering device, it can be easily transported to the luggage compartment on the upper floor, and it is not necessary to provide a new luggage port and a door for opening and closing the luggage. Costs can be reduced.
- the number of luggage ports and opening / closing doors'' can be reduced without lowering the load / unload function of the load into / from the luggage compartment of each layer.
- the cost of the aircraft can be reduced, and when retrofitting a passenger aircraft to a freighter, the renovation man-hours and the renovation cost can be reduced.
- the luggage ports at a plurality of locations in the longitudinal direction of the fuselage, it is possible to load and unload luggage from the plurality of luggage ports, thereby further improving the work efficiency of loading the luggage.
- a rope is connected to a luggage stand on which luggage is mounted, the rope is connected to a driving device via a pulley, and the luggage table is wound or unreeled by the driving device, thereby moving the luggage stand in the vertical direction of the body.
- FIG. 7 is a schematic perspective view of a freighter that performs air transportation of luggage according to the fourth embodiment.
- the lifting device is configured by a luggage stand, a cross link, and a hydraulic mechanism
- the third embodiment is different from the first to third embodiments.
- the fourth embodiment is configured by a guide rail, a rack, and a gear combined with the rack, whereas the fourth embodiment is configured by a motor and a rope. .
- the body 301 has a luggage port 3 22 at the rear, and a luggage door 3 12 that can be opened and closed is arranged at the luggage port 3 22.
- a partition wall 347 is provided in the machine, and a conveyor 318 is configured on the partition wall 347 so that the container 313 loaded from the luggage port 322 can be transferred forward.
- a partition wall 3 4 8 forming a luggage compartment 3 10 is disposed above the partition wall 3 47 on the front side in the aircraft, and a lifting device 3 15 and a drawing are shown in front of the partition wall 3 48. There are no competitors. Then, the container 3 13 transported by the conveyor is stored in the upper surface 3 28 of the partition wall 3 48. ⁇ As shown in Fig. 8 (a), when the container 3 13 is stored in the luggage compartment 310, it is an operation of the aircraft, and the container 3 13 is moved from the luggage compartment 3 10 to the container 3 13 When loading and unloading, preparation for the operation of the lifting device (elevator) 3 15 is performed as shown in Fig. 8 (b).
- the lifting device 3 15 is a drive with a built-in motor as described later.
- the floor including the power source 303 is configured to be vertically movable.
- Fig. 8 (b) When moving the container 3 13 from the luggage room 3 10 to the middle room 3 2 1, first open the opening and closing floor 3 0 5, and then to the partition wall 3 4 8 as shown in Fig. 8 (b).
- the stored guide rail 304 is opened and its tip is fixed to the partition wall 347 as described later, and the rack fixed to the guide rail 304 and a gear (not shown) are joined.
- the lifting device 3 15 can be lowered.
- Fig. 8 (c) shows a state in which the lifting device (elevation evening) has descended to the middle room 3221.
- FIG. 9 is a perspective view of an elevating device according to a fourth embodiment.
- a rectangular opening 328a is opened in the floor surface 328 of the partition wall 348, and a lifting device 315 is arranged in the opening 328a.
- a mechanism used for the lifting / lowering operation of the lifting / lowering device 315 is arranged around the opening 3288a.
- a support rod 3 14 is held rotatably on one of the support rod supports 3 0 8 a, 3 9 9, 3 9 9 and 3 0 8 b, and the other support rod receiver 3 0 8 c, 3 0
- the other support rods 314 are rotatably held at 9, 309 and 308d.
- an after-mentioned actuary 338 (FIG. 18) is arranged in the middle of the support rod receivers 309, 309.
- the support rods 3 14 are provided in a pair on two opposite sides of the opening 3 28 a.
- the support bar 314 is rotatably fitted in the opening of the rack head 334a.
- the lifting device 315 is disposed in the opening 3288a, and the walls 315b, 315b, 315c are arranged on three sides on the floor 315a of the lifting device.
- a gear receiver 3 2 3, 3 2 3 is provided on the outside of the wall 3 15 b, and a tip 3 2 3 a, 3 2 3 a of the gear receiver 3 2 3 a has a gear shaft 3 1 6 ( (Fig. 17) is rotatably fitted.
- a sprocket 319 is fixed to one end of the gear shaft 316, and an elevator gear 317 is fixed alongside the sprocket 319.
- a motor 306 and a reduction gear unit 307 are arranged, and the driving force of the motor 306 is controlled by the gear unit 307.
- the chain is transmitted from an output gear (not shown) to the sprocket 319 by a chain 320 stretched over the sprocket 319, and the transmission force is transmitted to the elevator gear 317. . Therefore, When the elevator gear 317 rotates, the lifting device 315 is configured to be able to descend in combination with a rack (not shown).
- FIG. 10 shows a state in which the opening / closing floor 30.5 arranged on the floor 3226 of the middle room 3221 (FIG. 8) is opened in preparation for the descent of the elevating device 315.
- Fig. 11 shows that, after opening the opening / closing floor 305, the upper end of the guide rail 304 stored under the elevating device 315 is rotated, and This figure shows a state in which it is fixed and held to a partition wall 347 having a floor surface 326 of Fig. 1 (Fig. 8). From this state, the lifting device 3 15 can be lowered on the floor 3 26 of the middle room 3 2 1 (FIG. 8).
- Fig. 12 shows a state in which the container 3 13 is placed on the elevating device 3 15 on the floor 3 26 of the middle room 3 21 (Fig. 8). From this state, the container 3 13 can be carried to the luggage room 3 10 (FIG. 8) as shown in FIG. Next, details of each mechanism will be described.
- Fig. 14 is an enlarged view of section C in Fig. 8 (b) illustrating the base of the opening / closing floor 3 05 that can be opened and closed on the floor surface 3 26 of the middle room 3 2 1 (Fig. 8). It is.
- a hinge 3 29 is provided on a floor 3 2 6, and one end of an opening and closing floor 3 2 5 to which an opening and closing floor 3 0 5 is attached is fixed to a movable piece of the hinge 3 2 9. ing.
- a connection portion 324 is provided on the opening / closing floor base 325.
- a lever 330 is provided below the floor surface 326 so as to be rotatable about an axis 330a, and an opening 330b formed at the tip of the lever 330 is provided.
- a connecting plate (not shown) is arranged between the connecting portion 3 24 and the opening 3 24 a provided in the connecting portion 3 24.
- the shaft center 330a of the lever 330 is connected to a motor (not shown).
- the opening / closing mechanism of the opening / closing floor 3 05 is configured as described above, when the lever 3 3 0 is in the solid line position, the opening / closing floor 3 0 5 is arranged parallel to the floor 3 2 6 and the lifting device 3 The opening where 1 5 is placed is closed, but the lever 3 30 rotates clockwise, and when it reaches the virtual line position, the opening and closing floor 3 05 stands up, and the lifting device 3 15 is located An opening is formed. 15 is an enlarged view of a portion C in FIG. 8 (b), in which the opening / closing floor 305 is opened, and thereafter, the distal end side of the guide rail 304 is moved to the middle room 3221 (FIG. FIG.
- FIG. 8 shows a state of being fixedly held on a partition wall 347 having a floor surface 326 of FIG.
- a snap ring 332 is rotatably disposed on the partition wall 347, and a pin 3 is provided at the lower end of the guide rail 304.
- the pin 304a which has been implanted and rotated from the left in FIG. 15, is supplemented by a snap ring 332, in which case a mechanism (not shown) is used to electrically or manually As a result, the snap ring 332 rotates 90 ° and is held at that position.
- FIG. 8B is an enlarged view of a portion D in FIG. 8 (b), and is an explanatory diagram showing the storage and arrangement of the guide rail 304 and the rack 331.
- the support rod arm 3 3 3 fixed to the support rod 3 1 4 has an opening 3 3 3 a at the tip, while it is suspended on the support rod 3 1 4 via the rack head 3 3 4 a.
- an opening hole 3 3 4 c is formed, and the second connection end 3 having the opening hole 3 3 4 c as a rotation axis. 36 is rotatably disposed, and the second connection end 336 is fixed to the tip of a guide rail 304 having a rack 331.
- the second connection end 336 has an opening 3336a, and the end between the opening 3336a and the tip end opening 333a of the support rod arm 3333 has two ends.
- a connecting rod 335 having a pin rotatably connected to the opening hole is disposed.
- the end of the support rod 390 is held rotatably at the mounting part 339, and the other end side
- the movable rod 3 3 8a is arranged in a stretchable manner.
- a support rod arm 3 3 7 is fixedly attached to the support rod 3 1 4, and the tip of the support rod arm 3 3 7 can rotate around the tip pin 3 3 7 a of the movable rod 3 3 8 a. It is connected to.
- the movable arm 338 a which was extended when the actuator 338 was driven, expands and contracts, and the support rod 314 rotates clockwise in FIG.
- the guide rails 304 and the racks 331, which were stored in a horizontal state are clocked with the opening holes 3 3 4c as rotation axes.
- the guide rail 304 and the rack 331 are in a vertical state.
- the details of the gear shaft 3 16 and the gear 3 17 shown in FIG. 9 are shown in FIG. 17.
- two gears 3 17 are arranged at a predetermined distance on the gear shaft 3 16.
- two racks 3 3 1 and 3 3 1 that match the gears 3 17 and 3 17 are provided on the guide rail 304. Have been.
- FIG. 21 is an enlarged view of a portion E in FIG. 8 (b).
- a motor 303 is disposed in the driving source 303, and a gear 303 fixed to the motor rotating shaft is provided.
- a gear section 307 is constituted by the intermediate gear 340, gears 341 and 324, etc., and a sprocket 334, 334 and a sprocket 334 having the rotation center of the gear 341 and 342 in the same axis.
- Chains 320 and 320 extend between the rack-side sprockets 319 and 319, respectively.
- the rotational driving force of the motor 306 is transmitted to the sprockets 319 and 319 by the chain 322, and the gear shaft 316 is rotated to rotate the gear 317.
- the elevating device 3 15 descends, and the container 3 13 placed on the elevating device 3 15 descends.
- the lift device is provided with a drive source and a gear connected to the drive source, the luggage compartment is partitioned by a partition wall, and the lift A guide means for driving the device and a rack coupled with the gear are stored, and guide means for guiding the lifting device before driving the lifting device, and a movement-related mechanism such as a rack coupled with the gear are provided. Since it is configured to appear in the movement area of the lifting device, when the lifting device is not driven, the movement-related mechanism is stored in the partition wall. I can carry out my work safely.
- FIG. FIG. 22 is a schematic cross-sectional view of a passenger aircraft according to the fifth embodiment, and a perspective view of the lifting device according to the fifth embodiment.
- the cabins are partitioned by partition walls 414, 415, and 416, and a second-floor guest room 410, a first-floor guest room 4 2 1, and a luggage room 4 1 1 are provided. It has been done.
- the cabin 4 2 1 on the first floor can enter and exit through the passenger entrance 501 as shown in FIG.
- luggage door 4 1 2 in the luggage compartment 4 1 luggage can be taken in and out through the luggage opening (luggage opening) 4 2 3.
- the gear service space 4 19 is usually located in the cabin where passengers can enter and exit, especially when the passengers ascend and descend on the passenger aircraft on the floor 4 2 6 in front of the entrance on both sides of the gear train service space. It is located where it passes.
- gear train service space 4 19 As shown in Fig. 23, in the gear racer service space 4 19, a part of the gear train 4 09, where a cooking range, refrigerator, etc. are arranged above the gear wheel inner wall 407, and ⁇ , wagon A lift room stop space 4 17 where the 4 13 is arranged is provided in the gear train service space 4 19 so as to open.
- the floor space 4 26 is open in the lift room stop space 4 17, and communicates with the lower luggage room 4 11.
- a lift room 401 carrying a plurality of wagons 4 13 is arranged between these lift room stop spaces so as to be able to move up and down, and the lift room 401 is moved up and down in the gear train service space 4 19. It is configured to stop at the room stop space 4 17 and stop on the floor 4 27 in the lower luggage room 4 11.
- a pulley 4002a that rotatably supports the rope 404a, a pulley 4002b that rotatably supports the rope 404b, and a rope 404c are provided above the vicinity of 1a.
- a pulley 402c that rotatably supports and a pulley 402c that rotatably supports the rope 400d are rotatably disposed.
- Pulleys 400a and 400b are arranged above the pulleys 402c and 402d.
- the pulley 403a has two recesses, rotatably supports the ropes 404a, 404c, and the pulley 403b also has two recesses, 04 b and 404 d are rotatably supported.
- a motor 406 is arranged in the second floor guest room 410, and a winding pobin 43 1 a is provided at both ends of the rotating shaft of the motor. 4 3 1b is fixed.
- Each of the pobbins 4 3 1 and 4 3 1 b is provided with two rope winding portions arranged in the axial direction, and the rope winding portion of the bobbin 4 3 1 a has ropes 4 0 4 a and 4 4 c.
- One end of 404 d is fixed.
- Mouth 4 0 4a is pulley 4 0 3a, 4 0 2a
- rope 4 0 4b is pulley 4 0 3b, 4 0 2b
- rope 4 0 4c is pulley 4 0 3a
- the rope is connected to the pulleys 400b and the other end of the rope is fixed to the upper surface 401a of the lift room 401, respectively. ing.
- the lifting chamber 401 rises by the length of the winding 40 m of the motor 406, and the length of the unwinding amount of the rope 404 of the motor 406
- the lift chamber 401 is configured to descend.
- the wagon 413 is loaded in the lift room 401, and the motor 406 is rotated in the reverse direction to rotate the rope 404.
- the lift room 4 0 1 descends, and the wagon 4 13 can be carried to the baggage room 4 1 1 by stopping at the baggage room 4 1 1.
- the cargo 4 13 can be carried out from the luggage opening 4 2 3.
- a new wagon 4 13 containing necessary items is carried from the luggage slot 4 23 and loaded into the elevator room 401 to carry it to the gear train service space 4 19. You can enter.
- the fifth embodiment uses the elevator room 401 without moving the wagon 4 13 from the gear train service space 4 19 through the floor in the same cabin to the outside.
- Transport between the gear racer service space 4 19 of the wagon 4 13 and the luggage compartment 4 11 1, and the wagon 4 13 can be transported from the load port 4 2 3 provided in the luggage compartment 4 1 1
- This can be done in the same time zone, reducing the time for passenger aircraft to park on the ground and allowing many flights to operate at a certain time, reducing the waiting time for passengers, improving the profitability of airline companies and the Convenience can be achieved.
- the present invention relates to an aircraft having a cabin functioning as a luggage compartment or a passenger cabin in an upper and lower plurality of layers, A first cabin having a mouth and the first key;
- the luggage carried into the cabin via the luggage port can be transferred to the second cabin directly above or immediately below without the luggage port, and the load from the second cabin can be transferred to the first cabin.
- a lift device configured so as to be capable of loading and unloading the luggage between the outside and the second cabin through the luggage dedicated port.
- the present invention can use the luggage port (luggage port) already provided on the aircraft to load and unload the luggage through the luggage port, and to provide a door to the outside at the fuselage position facing the luggage compartment.
- the first cabin having a dedicated baggage port to be opened and closed, and the second cabin not having the dedicated baggage port are configured to carry in / out a baggage by a lifting device, so that a cabin that functions as a luggage compartment.
- the number of luggage ports for loading and unloading luggage and the number of luggage doors are reduced without reducing the strength of the fuselage by installing a new luggage port specially at the same time, and without lowering the luggage loading and unloading functions. As a result, the aircraft cost can be reduced.
- a luggage port that is opened and closed by a door is provided only in the lower luggage compartment, and the luggage is loaded into the cabin from the luggage port, and is loaded into the upper luggage compartment by vertically moving the luggage by the elevating device.
- This can be done by moving the upper baggage compartment and the lower baggage compartment, unlike the prior art, without having to provide a luggage opening that can be opened and closed by a door. Baggage to be stored in both luggage compartments on the upper level can be loaded and unloaded.
- the present invention is a heavy object having the same thickness and material as the fuselage, and only one or a minimum number of luggage opening / closing doors requiring a precise seal need be provided.
- the number of assembling steps and material costs are greatly reduced.
- the height of the top layer of a three-layer aircraft is generally about 10 meters above the ground, cargo from outside the aircraft is limited to the middle layer, and the cargo is moved to the top floor by an onboard elevator. By doing so, the occupational safety of cargo loading workers will also be improved.
- the lifting device when converting a passenger aircraft into a cargo aircraft, If the lifting device is provided near the existing luggage port or in the luggage compartment near the same layer as the existing luggage port, the luggage carried in from the existing luggage port can be transferred to the elevating device. By moving vertically, it can be easily transported to the upper luggage compartment, and it is not necessary to provide a new luggage port and a door to open and close the luggage compartment, thus reducing the number of renovation steps and renovation costs Can be.
- the present invention provides a gear laser service space in the second cabin that functions as a cabin, and the lifting device capable of moving between the gear train service space and the first cabin.
- luggage In the gear train service space, luggage is loaded into the lifting device or configured to be able to be taken out, and between the gear train service space and the outside of the machine, the luggage can be loaded and unloaded.
- a wagon can be loaded and unloaded through the dedicated luggage port of the luggage compartment of the layer provided with a dedicated port, and the wagon is moved into the gear race service space on the same floor as the second cap pin, which functions as a passenger cabin by means of elevating and lowering in the cabin.
- the wagon By carrying in, the wagon is taken in and out using the emergency exit as in the prior art, and after the passengers disembark, the wagon is carried in on the same floor as the passenger cabin, and is carried into the gear train service space through the passenger passage.
Description
Claims
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/048,912 US6808142B2 (en) | 2000-06-06 | 2001-06-05 | Aircraft with a plurality of upper and lower cabins functioning as cargo compartments or passenger cabins and method of loading cargos for aircraft |
EP01934543A EP1211174B1 (en) | 2000-06-06 | 2001-06-05 | Aircraft with a plurality of upper and lower cabins functioning as cargo compartments or passenger cabins and method of loading cargos for aircraft |
DE60133078T DE60133078T2 (de) | 2000-06-06 | 2001-06-05 | Flugzeug mit einer mehrzahl von oberen und unteren, als passagierkabinen oder frachtabteilungen funktionierenden, kabinen und verfahren zum laden von fracht auf ein flugzeug |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2000-169574 | 2000-06-06 | ||
JP2000169574 | 2000-06-06 | ||
JP2000349833 | 2000-11-16 | ||
JP2000-349833 | 2000-11-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2001094200A1 true WO2001094200A1 (fr) | 2001-12-13 |
Family
ID=26593434
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/JP2001/004726 WO2001094200A1 (fr) | 2000-06-06 | 2001-06-05 | Aeronef comportant plusieurs cabines superieures et inferieures faisant office de compartiment a marchandises ou de cabines a passagers, et procede de chargement de marchandises sur un aeronef |
Country Status (4)
Country | Link |
---|---|
US (1) | US6808142B2 (ja) |
EP (2) | EP1211174B1 (ja) |
DE (1) | DE60133078T2 (ja) |
WO (1) | WO2001094200A1 (ja) |
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JP2011515272A (ja) * | 2008-03-28 | 2011-05-19 | エアバス オペラツィオンス ゲゼルシャフト ミット ベシュレンクテル ハフツング | バーンスルー耐性を示す航空機の胴体 |
US9878770B2 (en) | 2008-03-28 | 2018-01-30 | Airbus Operations Gmbh | Aircraft fuselage having burnthrough resistant components |
JP2015518556A (ja) * | 2012-03-28 | 2015-07-02 | ビーイー・エアロスペース・インコーポレーテッド | 収容可能扉を備える吊下げギャレー・インサート及び吊下げギャレー・インサートを含むギャレー |
JP2017013775A (ja) * | 2015-07-02 | 2017-01-19 | ザ・ボーイング・カンパニーThe Boeing Company | 航空機で使用するための貨物を保管する載貨カルーセルおよび方法 |
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DE60133078T2 (de) | 2009-02-26 |
US6808142B2 (en) | 2004-10-26 |
US20020148928A1 (en) | 2002-10-17 |
EP1211174A1 (en) | 2002-06-05 |
EP1873059A3 (en) | 2012-04-11 |
EP1211174B1 (en) | 2008-03-05 |
DE60133078D1 (de) | 2008-04-17 |
EP1873059A2 (en) | 2008-01-02 |
EP1211174A4 (en) | 2006-06-07 |
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