CN106628229B - The application of front frame posture aircraft carrying platform - Google Patents

The application of front frame posture aircraft carrying platform Download PDF

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Publication number
CN106628229B
CN106628229B CN201610796137.1A CN201610796137A CN106628229B CN 106628229 B CN106628229 B CN 106628229B CN 201610796137 A CN201610796137 A CN 201610796137A CN 106628229 B CN106628229 B CN 106628229B
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China
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aircraft
track
cantilever crane
platform
main
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CN106628229A (en
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马宏
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Chongqing opputi Technology Co.,Ltd.
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马宏
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/22Ground or aircraft-carrier-deck installations installed for handling aircraft
    • B64F1/225Towing trucks
    • B64F1/227Towing trucks adapted for directly connecting to aircraft, e.g. trucks without tow-bars

Abstract

The application of front frame posture aircraft carrying platform, is related to transporting equipment applied technical field.It is characterized by: step 1: pilot observes the display data of pool machine display screen in an aircraft;Step 2: when aircraft landing behind ground, slided into main platform body along transition ramp, nose-gear catch withstands aircraft nose-gear;Step 3: before cantilever crane track of the boarding gantry on cantilever crane moves to the passenger door of aircraft, opening the passenger door of aircraft, passenger is made to leave aircraft along boarding gantry;At the same time, cantilever crane track of the shipping loading frame on cantilever crane moves to aircraft hold in front of the door, and lower aircraft will be carried with machine cargo by opening cargo door;Step 4: after passenger and cargo are away from aircraft, aircraft is transported to stop position along airport track by front frame posture aircraft carrying platform.

Description

The application of front frame posture aircraft carrying platform
Technical field
The application of front frame posture aircraft carrying platform, is related to the applied technical field of transporting equipment.
Background technique
With the fast development of high speed information industry, adaptable transport service is also being grown rapidly therewith.Trip, material flow All what is maked rapid progress change quietly occurs for logical speed, and the radius of action of people is increasing, and the range of logistics is got over Come wider.Air-transport industry is quickly grown, and in recent years for domestic, is constantly expanded newly-increased course line, is expanded airport.
The course line bring that ground installation related to shipping increasingly highlights aviation development is inadaptable.
Summary of the invention
It is well known that the people for taking aircraft (aircraft) perhaps notice aircraft on ground or take off or land Different from automobile, drop (wheel) when aircraft lands, then with aircraft engine (turbofan, if Will be bigger using turbojet oil consumption) it is mover runner to airplane parking area, therefore oil consumption is big (especially in aircraft low speed Oil consumption is especially huge when being moved below 80 section), noise is big, easy aspirated foreign body causes failure, inhaled if there is personnel walk about also to have The danger entered.As " aerial liner of number AI619, will fly to Hyderabad from Mumbai at that time, due to aircraft copilot Get signal wrong, when starting engine, a ground crew is inhaled into engine."
To overcome the shortcomings of the prior art:
The first purpose of the application is that ground cart is replaced to draw aircraft;
The second purpose of the application is to reduce aircraft oil consumption, uses surface power supply supplying oil and gas as far as possible;
The third purpose of the application is to improve the ground of aircraft to rise and fall safety;
The fourth purpose of the application is to mitigate visitor, flow of goods pressure.
The application adopts the following technical scheme that achieve the above object
One, front frame posture aircraft carrying platform
1, front frame posture aircraft carrying platform, comprising: fuselage profile 1, main landing gear position 2, nose-gear position 3, Main platform body 10, cantilever crane 20, shipping loading frame 30, boarding gantry 40, rear thruster 50, airport track 60;
Main platform body 10 includes: main carrying platform 101, rear thruster track 102, ear platform 103, equipment box 104, transition ramp 105, radial trolley 106, main trolley 107, radial trolley movable axis 108, front chassis 109, nose-gear catch 110, preceding rise and fall Body panel 111;
Cantilever crane 20 includes: cantilever crane track 201, cantilever crane crossbeam 202, cantilever crane trolley 203, pool machine display screen 204, display screen branch Column 205;
Shipping loading frame 30 includes: rail is slided in baggage conveyor 301, belt support 302, loading frame end carriage 303, shipping Road 305, hoistable platform 306, crane 307, hoistable platform pedestal 308, hoistable platform idler wheel 309, sliding platform 310, sliding Platform roller 311;
Boarding gantry 40 includes: connecting bridge 401, bridge-frame end-beam 403, gantry sliding rail 405, is stepped on flexible airstair 402 Machine mouth 406, flexible vestibule diaphragm 407, shelter bridge supporting plate 408, crane 409, gantry idler wheel 410;
There are diesel engine, generator, bleed machine in equipment box 104;(diesel engine, generator, bleed machine in equipment box are to boat Pocket power supply, gas supply;Diesel engine, generator, bleed machine are that existing equipment repeats no more)
It is characterized by:
Main carrying platform 101 is "convex" shaped structure in the rear portion of main platform body 10, main platform body 10, and middle and back is square Shape, on both sides of the middle are connected with symmetrical ear platform 103, the part outstanding before main platform body 10 of nose-gear platform 111;
Equipment box 104 is housed on ear platform 103;
Main 101 end of carrying platform connection transition ramp 105 (is detailed in the I of Figure 18 along transition ramp uplink convenient for aircraft Partial enlarged view);
The section of transition ramp 105 is streamlined;
The rearward lower of main carrying platform 101 is connected with radial trolley 106;
Radial trolley 106 is equipped with four wheels below, and the four wheels of radial trolley 106 connect radial trolley movable axis 108;(convenient for turning along airport track 60)
Main trolley 107 is connected with below the middle part of main carrying platform 101;It is connected below the front of nose-gear platform 111 There is front chassis 109;
Cantilever crane track 201 has two groups, and every group is parallel rectilinear orbit;
Main trolley 107 is equipped with four wheels below;
Every group of 201 end of cantilever crane track is separately connected 103 front end of ear platform and nose-gear platform 111;
Organic field track 60 in airport, the track of airport track 60 have parallel four;(substitute sliding for the prior art Road)
The four wheels of radial trolley 106 and main trolley 107 are located on four tracks on airport track 60;Front chassis 109 are located in two inner tracks of airport track 60;
201 front end of cantilever crane track connects cantilever crane crossbeam 202, and cantilever crane crossbeam 202 is between two arms mounted track 201, with arm Mounted track 201 is vertical;
The lower linking arm rack trolley 203 of cantilever crane crossbeam 202;The wheel of cantilever crane trolley 203 is respectively seated at airport track 60 (cantilever crane trolley 203 plays supporting arm frame track 201, cantilever crane crossbeam 202, and can support whole front frame posture in two inner tracks Aircraft carrying platform moves on airport track 60)
Shipping loading frame 30 is housed on left side cantilever crane track 201;(cargo is helped to transport aircraft)
Boarding gantry 40 is housed on right arm mounted track 201;(shelter bridge of substitution existing equipment, can make passenger pass through boarding Gantry 40 climbs up aircraft, and alleviates because of the frequent congestion of aircraft landing)
(being detailed in Figure of description 1-5,17-19)
2, the front frame posture aircraft carrying platform, it is characterised in that: the radial direction trolley 106 is symmetrical 2 pairs.(bearing capacity is big)
3, the front frame posture aircraft carrying platform, it is characterised in that: the radial direction trolley 106 connects radial trolley Movable axis 108, (turning convenient for main carrying platform 101)
4, the front frame posture aircraft carrying platform, it is characterised in that: after being equipped on the main carrying platform 101 Thruster track 102, thruster track 102 after rear thruster 50 connects.(because the engine of aircraft can only carry out retreating, So thruster can be convenient for aircraft pushing down main carrying platform 101 after installing additional)
5, the front frame posture aircraft carrying platform, it is characterised in that: connected on the nose-gear platform 111 Nose-gear catch 110, the section of nose-gear catch 110 are trapezoidal catch.(convenient for stopping aircraft nose-gear)
6, the front frame posture aircraft carrying platform, it is characterised in that: be connected on 202 middle part of cantilever crane crossbeam aobvious Display screen pillar 205, pool machine display screen 204 connect display screen pillar 205.(so that pilot observes data)
7, the front frame posture aircraft carrying platform, it is characterised in that: nose-gear catch 110 is rubber catch.
8, the front frame posture aircraft carrying platform, it is characterised in that: the generator cable connection in equipment box 104 Aircraft.(APU on the aircraft of the alternative prior art)
9, the front frame posture aircraft carrying platform, it is characterised in that: the bleed machine gas source pipe in equipment box 104 Connect aircraft.(APU on the aircraft of the alternative prior art, so-called APU be the prior art aircraft on load and be used for The device of aircraft engine start premise power supply source and gas source)
10, the front frame posture aircraft carrying platform, it is characterised in that: the generator cable in equipment box 104 connects It connects rear thruster 50 and provides electric power for rear thruster.
11, the front frame posture aircraft carrying platform, it is characterised in that: the generator cable in equipment box 104 connects Boarding gantry 40 is connect as the power supply of boarding gantry 40.
12, the front frame posture aircraft carrying platform, it is characterised in that: the generator cable in equipment box 104 connects Shipping loading frame 30 is connect as the power supply of shipping loading frame 30.
13, the front frame posture aircraft carrying platform, it is characterised in that: the bleed machine in equipment box 104 is aviation Engine gas supply in device.
14, the front frame posture aircraft carrying platform, it is characterised in that: the bleed machine in equipment box 104 is aviation Air-conditioning gas supply in device.
Two, mobile shelter bridge
1, mobile shelter bridge, comprising: connecting bridge 401, flexible airstair 402, bridge-frame end-beam 403, gantry sliding rail 405, boarding gate 406, flexible vestibule diaphragm 407, shelter bridge supporting plate 408, crane 409, gantry idler wheel 410, bridge import 411, rolling bridge wheel 412;
It is characterized by: mobile shelter bridge main body is boarding gantry 40, connecting bridge 401 connects boarding gate 406, boarding gate 406 connect flexible vestibule diaphragm 407, (when passing through airport lounge boarding convenient for passenger, flexible vestibule diaphragm 407 is docked with passenger door)
Connecting bridge 401 is horizontal connecting bridge;
Flexible airstair 402 is telescopic, the upper end connection connecting bridge 401 for the airstair 402 that stretches, lower end connecting bridge import 411;
411 bottom of bridge import connects gantry idler wheel 410;Gantry idler wheel 410 is located on gantry sliding rail 405, gantry 405 both ends of sliding rail connect bridge-frame end-beam 403;
Rolling bridge wheel 412 is located on cantilever crane track 201;
401 bottom connecting corridor bridgework plate 408 of connecting bridge, shelter bridge supporting plate 408 connect two groups of cranes 409;
2, the mobile shelter bridge, it is characterised in that: connecting bridge 401 is horizontal connecting bridge.
3, the mobile shelter bridge, it is characterised in that: the flexible vestibule diaphragm 407 is rubber and plastic flexibility vestibule diaphragm.
4, the mobile shelter bridge, it is characterised in that: the rolling bridge wheel 412 is the idler wheel for covering rubber.
5, the mobile shelter bridge, it is characterised in that: the gantry idler wheel 410 is the idler wheel for covering rubber.
Three, shipping loading frame
1, shipping loading frame 30 includes: baggage conveyor 301, belt support 302, loading frame end carriage 303, conveyer belt are low Hold support 304, shipping sliding rail 305, hoistable platform 306, crane 307, hoistable platform pedestal 308, hoistable platform idler wheel 309, the high-end support sliding block 313 of sliding platform 310, sliding platform idler wheel 311, loading frame idler wheel 312, conveyer belt, conveyer belt branch Brace 314, belt support 302;
It is characterized by:
Baggage conveyor 301 is flat conveyer belt, one end high and another end low;(convenient for cargo is transmitted to height by lower Place) baggage conveyor 301 low side and high-end is connected separately with two groups of belt supports 302, two groups of conveyer belt branch of low side below The lower connection conveyer belt low side support 304 of frame 302;The lower high-end support sliding block of connection conveyer belt of two groups of high-end belt supports 302 313;(the high-end support sliding block 313 of conveyer belt is moved along shipping sliding rail 305 can be such that the high-end of conveyer belt is raised and lowered, just In aircraft hold doors conveyer belt alignment type is different and that height is different, spare parts of goods can use baggage conveyor 301 will Cargo is transported to aircraft hold)
Conveyer belt low side support 304 connects shipping sliding rail 305, and the high-end support sliding block 313 of conveyer belt is sleeved on shipping On sliding rail 305;
306 lower part of hoistable platform connects crane 307, the crane of 307 staggered form of crane;
The lower connection hoistable platform pedestal 308 of crane 307;Hoistable platform pedestal 308 connects hoistable platform idler wheel 309;It rises Drop platform roller 309 is located on shipping sliding rail 305;
The both ends of shipping sliding rail 305 are all connected with loading frame end carriage 303;
Loading frame end carriage 303 is lower to connect loading frame idler wheel 312;Loading frame idler wheel 312 is located on cantilever crane track 201;
Belt support 302 connects conveyer belt support arm 314.
2, the shipping loading frame, it is characterised in that: baggage conveyor 301 is that multilayer belt carcass rubber presses conveyer belt.
3, the shipping loading frame, it is characterised in that: rail is slided in the shipping of 306 lower part of sliding platform 310 and hoistable platform Road 305 is two parallel tracks.
4, the shipping loading frame, it is characterised in that: rail is slided in the shipping of 306 lower part of sliding platform 310 and hoistable platform Road 305 is three parallel tracks.
5,310 lower part of sliding platform connects sliding platform idler wheel 311, and sliding platform idler wheel 311 is located at shipping sliding rail On road 305;(effect of sliding platform is by large cargo such as the cargo of container class by being moved under aircraft hold door at a distance Side, then cargo hold doorway is lifted to by hoistable platform 306)
Four, rear thruster
1, rear thruster includes: roller 501, roller axle 502, roller support 503, roller spring 504, support 505, connecting rod 506, towing bracket 508, linear motor rotor 509, linear motor stator electric 510;
It is characterized by: rear thruster front end is connected with roller 501, there are roller axle 502, roller axle in the column center of roller 501 502 connection roller supports 503;
Roller support 503 and roller spring 504 have multiple groups, and roller support 503 connects roller spring 504, multiple groups roller 504 connecting support 505 of bracket 503 and roller spring;
Support 505 is the support of strip;Support 505 or so respectively has one, and the center line of two supports is straight in same On line, connecting rod 506 is connected among two supports 505;
Support 505 is located on rear thruster track 102.
2, the rear thruster, it is characterised in that: support 505 connects towing bracket 508, and towing bracket 508 connects straight line Rotor 509;Towing bracket 508 connects linear motor stator electric 510.
3, the rear thruster, it is characterised in that: have spring spool outside roller spring 504.
4, the rear thruster, it is characterised in that: 501 housing rubber sleeve of roller.
5, the rear thruster, it is characterised in that: roller 501 is rubber-plastics material roller.
Five, the application of front frame posture aircraft carrying platform
1, front frame posture aircraft carrying platform, comprising: fuselage profile 1, main landing gear position 2, nose-gear position 3, Main platform body 10, cantilever crane 20, shipping loading frame 30, boarding gantry 40, rear thruster 50, airport track 60;
Main platform body 10 includes: main carrying platform 101, rear thruster track 102, ear platform 103, equipment box 104, transition ramp 105, radial trolley 106, main trolley 107, radial trolley movable axis 108, front chassis 109, nose-gear catch 110, preceding rise and fall Body panel 111;
Cantilever crane 20 includes: cantilever crane track 201, cantilever crane crossbeam 202, cantilever crane trolley 203, pool machine display screen 204, display screen branch Column 205;
There are diesel engine, generator, bleed machine in equipment box 104;
Main carrying platform 101 is "convex" shaped structure in the rear portion of main platform body 10, main platform body 10, and middle and back is square Shape, on both sides of the middle are connected with symmetrical ear platform 103, the part outstanding before main platform body 10 of nose-gear platform 111;Ear Equipment box 104 is housed on platform 103;
Main 101 end of carrying platform connects transition ramp 105;The section of transition ramp 105 is streamlined;Main carrying platform 101 rearward lower is connected with radial trolley 106;Radial trolley 106 is equipped with four wheels below, and four of radial trolley 106 Wheel connects radial trolley movable axis 108;Main trolley 107 is connected with below the middle part of main carrying platform 101;Nose-gear platform Front chassis 109 is connected with below 111 front;Front below be connected with front chassis 109;Cantilever crane track 201 has two groups, every group For parallel rectilinear orbit;Main trolley 107 is equipped with four wheels below;Every group of 201 end of cantilever crane track is separately connected ear platform 103 Front end and nose-gear platform 111;
Organic field track 60 in airport, the track of airport track 60 have parallel four;Radial trolley 106 and main trolley 107 four wheels are located on four tracks on airport track 60;Front chassis 109 is located in two of airport track 60 On siding track;201 front end of cantilever crane track connects cantilever crane crossbeam 202, and cantilever crane crossbeam 202 is between two arms mounted track 201, with arm Mounted track 201 is vertical;The lower linking arm rack trolley 203 of cantilever crane crossbeam 202;The wheel of cantilever crane trolley 203 is respectively seated at airport rail In two inner tracks in road 60;
Shipping loading frame 30 is housed on left side cantilever crane track 201;
Boarding gantry 40 is housed on right arm mounted track 201;
The radial direction trolley 106 is symmetrical 2 pairs;
The radial direction trolley 106 connects radial trolley movable axis 108,
Rear thruster track 102, thruster track 102 after rear thruster 50 connects are housed on the main carrying platform 101;
Nose-gear catch 110 is connected on the nose-gear platform 111, the section of nose-gear catch 110 is ladder Shape catch;
Display screen pillar 205 is connected on 202 middle part of cantilever crane crossbeam, pool machine display screen 204 connects display screen pillar 205;
The application of front frame posture aircraft carrying platform, it is characterised in that:
Step 1: pilot in an aircraft, observes the display data of pool machine display screen 204;
Step 2: when aircraft landing behind ground, slided into main platform body 10 along transition ramp 105, nose-gear wheel Gear 110 withstands aircraft nose-gear;
Step 3: before cantilever crane track 201 of the boarding gantry 40 on cantilever crane 20 moves to the passenger door of aircraft, opening boat The passenger door of pocket makes passenger leave aircraft along boarding gantry 40;At the same time, arm of the shipping loading frame 30 on cantilever crane 20 Mounted track 201 moves to aircraft hold in front of the door, and lower aircraft will be carried with machine cargo by opening cargo door;
Step 4: after passenger and cargo are away from aircraft, front frame posture aircraft carrying platform will navigate along airport track 60 Pocket is transported to stop position.
2, the application of the front frame posture aircraft carrying platform, it is characterised in that:
Step 5: when aircraft will take off, pilot's machine display screen 204 on the berth reads related data;
Step 6: before cantilever crane track 201 of the boarding gantry 40 on cantilever crane 20 moves to the passenger door of aircraft, opening boat The passenger door of pocket makes passenger climb up aircraft along boarding gantry 40;At the same time, arm of the shipping loading frame 30 on cantilever crane 20 Mounted track 201 moves to aircraft hold in front of the door, and aircraft will be transported with the cargo of confidential transport by opening cargo door;
Step 7: closing the passenger door and cargo door of aircraft;
Step 8: aircraft is transported on airport taxiway by front frame posture aircraft carrying platform;
Step 9: aircraft release front frame posture aircraft carrying platform is served taxiway by thruster 50 after starting.
Beneficial effect
1, due to the present invention use be driven by electricity it is fuel-efficient compared with ground mover.
2, compared with the ground mover of the prior art, (it can be aircraft under normal conditions in aircraft, can also use In other aircrafts such as dirigible) it directly draws after gun off the runway, save aircraft fuel oil.
3, compared with the ground mover of the prior art, (it can be aircraft under normal conditions in aircraft, can also use In other aircrafts such as dirigible) it directly draws after gun off the runway, saving the abrasion of aircraft critical component, (for example aircraft starts Machine etc.).
4, the loading capacity of aircraft it is big as Air Passenger company 380 type passenger planes, maximum take-off weight is 560 tons, uses rail Road substitute taxiway can investment price it is close, but maintenance cost reduce;Taxiway very important person's working hour carves cleaning, and track then need not.
5, because airplane parking area needs high-intensitive ground, and the platform of the application is located on track, therefore is saved High-intensitive airplane parking area.
6, by the rear thruster in main platform body 10, airport trailer is saved.
Detailed description of the invention
Fig. 1: front frame posture aircraft carrying platform top view
Fig. 2: front frame posture aircraft carrying platform A-A face schematic diagram
Fig. 3: front frame posture aircraft carrying platform B-B face schematic diagram
Fig. 4: front frame posture aircraft carrying platform C-C face schematic diagram
Fig. 5: front frame posture aircraft carrying platform and aircraft position schematic side view
Fig. 6: boarding gantry main view
Fig. 7: boarding gantry left view
Fig. 8: boarding gantry right view
Fig. 9: shipping loading frame main view
Figure 10: shipping loading frame rearview
Figure 11: rear thruster main view enlarged drawing
Figure 12: rear thruster A to partial enlarged view
Figure 13: rear thruster top view
Figure 14: cantilever crane trolley main view
Figure 15: cantilever crane trolley left view
Figure 16: cantilever crane trolley top view
Figure 17: airport track top view
Figure 18: I partial enlarged view
Figure 19: II partial enlarged view
Figure 20: III partial enlarged view
Figure 21: IV partial enlarged view
Figure 22: V partial enlarged view
Figure 23: VI partial enlarged view
Figure 24: VII partial enlarged view
In figure: 1 fuselage profile, 2 main landing gear positions, 3 nose-gear positions, 10 main platform bodies, 20 cantilever cranes, 30 shippings dress Thruster behind carrier, 40 boarding gantries, 50,60 airport tracks,
Thruster track, 103 ear platforms, 104 equipment boxs, 105 transition ramps, 106 radial platforms behind 101 main carrying platforms, 102 Vehicle, 107 main trolleys, 108 radial trolley movable axis, 109 front chassis, 110 nose-gear catch, 111 nose-gear platforms,
201 cantilever crane tracks, 202 cantilever crane crossbeams, 203 cantilever crane trolleys, 204 pool machine display screens, 205 display screen pillars,
301 baggage conveyors, 302 belt supports, 303 loading frame end carriages, 304 conveyer belt low side supports, 305 shippings are sliding Dynamic rail road, 306 hoistable platforms, 307 cranes, 308 hoistable platform pedestals, 309 hoistable platform idler wheels, 310 sliding platforms, 311 Sliding platform idler wheel, 312 loading frame idler wheels, the high-end support sliding block of 313 conveyer belts, 314 conveyer belt support arms,
401 connecting bridges, 402 flexible airstairs, 403 bridge-frame end-beams, 405 gantry sliding rails, 406 boarding gates, 407 flexibilities Vestibule diaphragm, 408 shelter bridge supporting plates, 409 cranes, 410 gantry idler wheels, 411 bridge imports, 412 rolling bridge wheels,
501 rollers, 502 roller axles, 503 roller supports, 504 roller springs, 505 supports, 506 connecting rods, 508 traction branch Frame, 509 rotor of straight line, 510 linear motor stator electrics,
203.1 frameworks, 203.2 wheel to, 203.3 cartridges, 203.4 sliding sleeves, 203.5 hydraulic damper, 203.6 pivoted arms Formula axle box.
1: Figure 19 II partial enlarged view of note is a partial enlarged view of cantilever crane trolley main view, it is intended that instruction cantilever crane trolley Position when use.
2: Figure 21 IV partial enlarged view of note is practical be exactly shipping loading frame 30 top view, IV partial enlargement can be in conjunction with figure 1 front frame posture aircraft carrying platform top view more clearly reflects the position where it and effect.
Specific embodiment
The application is described further with reference to the accompanying drawings and examples.
Embodiment 1
1, front frame posture aircraft carrying platform, comprising: fuselage profile 1, main landing gear position 2, nose-gear position 3, Main platform body 10, cantilever crane 20, shipping loading frame 30, boarding gantry 40, rear thruster 50, airport track 60;
Main platform body 10 includes: main carrying platform 101, rear thruster track 102, ear platform 103, equipment box 104, transition ramp 105, radial trolley 106, main trolley 107, radial trolley movable axis 108, front chassis 109, nose-gear catch 110, preceding rise and fall Body panel 111;
Cantilever crane 20 includes: cantilever crane track 201, cantilever crane crossbeam 202, cantilever crane trolley 203, pool machine display screen 204, display screen branch Column 205;
Shipping loading frame 30 includes: rail is slided in baggage conveyor 301, belt support 302, loading frame end carriage 303, shipping Road 305, hoistable platform 306, crane 307, hoistable platform pedestal 308, hoistable platform idler wheel 309, sliding platform 310, sliding Platform roller 311;
Boarding gantry 40 includes: connecting bridge 401, bridge-frame end-beam 403, gantry sliding rail 405, is stepped on flexible airstair 402 Machine mouth 406, flexible vestibule diaphragm 407, shelter bridge supporting plate 408, crane 409, gantry idler wheel 410;
There are diesel engine, generator, bleed machine in equipment box 104;(diesel engine, generator, bleed machine in equipment box are to boat Pocket power supply, gas supply;Diesel engine, generator, bleed machine are that existing equipment repeats no more)
It is characterized by:
Main carrying platform 101 is "convex" shaped structure in the rear portion of main platform body 10, main platform body 10, and middle and back is square Shape, on both sides of the middle are connected with symmetrical ear platform 103, the part outstanding before main platform body 10 of nose-gear platform 111;
Equipment box 104 is housed on ear platform 103;
Main 101 end of carrying platform connection transition ramp 105 (is detailed in the I of Figure 18 along transition ramp uplink convenient for aircraft Partial enlarged view);
The section of transition ramp 105 is streamlined;
The rearward lower of main carrying platform 101 is connected with radial trolley 106;
Radial trolley 106 is equipped with four wheels below, and the four wheels of radial trolley 106 connect radial trolley movable axis 108;(convenient for turning along airport track 60)
Main trolley 107 is connected with below the middle part of main carrying platform 101;It is connected below the front of nose-gear platform 111 There is front chassis 109;
Cantilever crane track 201 has two groups, and every group is parallel rectilinear orbit;
Main trolley 107 is equipped with four wheels below;
Every group of 201 end of cantilever crane track is separately connected 103 front end of ear platform and nose-gear platform 111;
Organic field track 60 in airport, the track of airport track 60 have parallel four;(replace sliding for the prior art Road)
The four wheels of radial trolley 106 and main trolley 107 are located on four tracks on airport track 60;Front chassis 109 are located in two inner tracks of airport track 60;
201 front end of cantilever crane track connects cantilever crane crossbeam 202, and cantilever crane crossbeam 202 is between two arms mounted track 201, with arm Mounted track 201 is vertical;
The lower linking arm rack trolley 203 of cantilever crane crossbeam 202;The wheel of cantilever crane trolley 203 is respectively seated at airport track 60 (cantilever crane trolley 203 plays supporting arm frame track 201, cantilever crane crossbeam 202, and can support whole front frame posture in two inner tracks Aircraft carrying platform moves on airport track 60)
Shipping loading frame 30 is housed on left side cantilever crane track 201;(cargo is helped to transport aircraft)
Boarding gantry 40 is housed on right arm mounted track 201;(shelter bridge of substitution existing equipment, can make passenger pass through boarding Gantry 40 climbs up aircraft, and alleviates because of the frequent congestion of aircraft landing)
2, the front frame posture aircraft carrying platform, it is characterised in that: the radial direction trolley 106 is symmetrical 2 pairs.(bearing capacity is big)
3, the front frame posture aircraft carrying platform, it is characterised in that: the radial direction trolley 106 connects radial trolley Movable axis 108, (turning convenient for main carrying platform 101)
4, the front frame posture aircraft carrying platform, it is characterised in that: after being equipped on the main carrying platform 101 Thruster track 102, thruster track 102 after rear thruster 50 connects.(because the engine of aircraft can only carry out retreating, So thruster can be convenient for aircraft pushing down main carrying platform 101 after installing additional)
5, the front frame posture aircraft carrying platform, it is characterised in that: connected on the nose-gear platform 111 Nose-gear catch 110, the section of nose-gear catch 110 are trapezoidal catch.(convenient for stopping aircraft nose-gear)
6, the front frame posture aircraft carrying platform, it is characterised in that: be connected on 202 middle part of cantilever crane crossbeam aobvious Display screen pillar 205, pool machine display screen 204 connect display screen pillar 205.(so that pilot observes data)
7, the front frame posture aircraft carrying platform, it is characterised in that: nose-gear catch 110 is rubber catch.
8, the front frame posture aircraft carrying platform, it is characterised in that: the generator cable connection in equipment box 104 Aircraft.(APU on the aircraft of the alternative prior art)
9, the front frame posture aircraft carrying platform, it is characterised in that: the bleed machine gas source pipe in equipment box 104 Connect aircraft.(APU on the aircraft of the alternative prior art, so-called APU be the prior art aircraft on load and be used for The device of aircraft engine start premise power supply source and gas source)
10, the front frame posture aircraft carrying platform, it is characterised in that: the generator cable in equipment box 104 connects It connects rear thruster 50 and provides electric power for rear thruster.
11, the front frame posture aircraft carrying platform, it is characterised in that: the generator cable in equipment box 104 connects Boarding gantry 40 is connect as the power supply of boarding gantry 40.
12, the front frame posture aircraft carrying platform, it is characterised in that: the generator cable in equipment box 104 connects Shipping loading frame 30 is connect as the power supply of shipping loading frame 30.
13, the front frame posture aircraft carrying platform, it is characterised in that: the bleed machine in equipment box 104 is aviation Engine gas supply in device.
14, the front frame posture aircraft carrying platform, it is characterised in that: the bleed machine in equipment box 104 is aviation Air-conditioning gas supply in device.
Embodiment 2
1, mobile shelter bridge, comprising: connecting bridge 401, flexible airstair 402, bridge-frame end-beam 403, gantry sliding rail 405, boarding gate 406, flexible vestibule diaphragm 407, shelter bridge supporting plate 408, crane 409, gantry idler wheel 410, bridge import 411, rolling bridge wheel 412;
It is characterized by: mobile shelter bridge main body is boarding gantry 40, connecting bridge 401 connects boarding gate 406, boarding gate 406 connect flexible vestibule diaphragm 407, (when passing through airport lounge boarding convenient for passenger, flexible vestibule diaphragm 407 is docked with passenger door)
Connecting bridge 401 is horizontal connecting bridge;
Flexible airstair 402 is telescopic, the upper end connection connecting bridge 401 for the airstair 402 that stretches, lower end connecting bridge import 411;
411 bottom of bridge import connects gantry idler wheel 410;Gantry idler wheel 410 is located on gantry sliding rail 405, gantry 405 both ends of sliding rail connect bridge-frame end-beam 403;
Rolling bridge wheel 412 is located on cantilever crane track 201;
401 bottom connecting corridor bridgework plate 408 of connecting bridge, shelter bridge supporting plate 408 connect two groups of cranes 409;
2, the mobile shelter bridge, it is characterised in that: connecting bridge 401 is horizontal connecting bridge.
3, the mobile shelter bridge, it is characterised in that: the flexible vestibule diaphragm 407 is rubber and plastic flexibility vestibule diaphragm.
4, the mobile shelter bridge, it is characterised in that: the rolling bridge wheel 412 is the idler wheel for covering rubber.
5, the mobile shelter bridge, it is characterised in that: the gantry idler wheel 410 is the idler wheel for covering rubber.
Embodiment 3
1, shipping loading frame 30 includes: baggage conveyor 301, belt support 302, loading frame end carriage 303, conveyer belt are low Hold support 304, shipping sliding rail 305, hoistable platform 306, crane 307, hoistable platform pedestal 308, hoistable platform idler wheel 309, the high-end support sliding block 313 of sliding platform 310, sliding platform idler wheel 311, loading frame idler wheel 312, conveyer belt, conveyer belt branch Brace 314, belt support 302;
It is characterized by:
Baggage conveyor 301 is flat conveyer belt, one end high and another end low;(convenient for cargo is transmitted to height by lower Place) baggage conveyor 301 low side and high-end is connected separately with two groups of belt supports 302, two groups of conveyer belt branch of low side below The lower connection conveyer belt low side support 304 of frame 302;The lower high-end support sliding block of connection conveyer belt of two groups of high-end belt supports 302 313;(the high-end support sliding block 313 of conveyer belt is moved along shipping sliding rail 305 can be such that the high-end of conveyer belt is raised and lowered, just In aircraft hold doors conveyer belt alignment type is different and that height is different, spare parts of goods can use baggage conveyor 301 will Cargo is transported to aircraft hold)
Conveyer belt low side support 304 connects shipping sliding rail 305, and the high-end support sliding block 313 of conveyer belt is sleeved on shipping On sliding rail 305;
306 lower part of hoistable platform connects crane 307, the crane of 307 staggered form of crane;
The lower connection hoistable platform pedestal 308 of crane 307;Hoistable platform pedestal 308 connects hoistable platform idler wheel 309;It rises Drop platform roller 309 is located on shipping sliding rail 305;
The both ends of shipping sliding rail 305 are all connected with loading frame end carriage 303;
Loading frame end carriage 303 is lower to connect loading frame idler wheel 312;Loading frame idler wheel 312 is located on cantilever crane track 201;
Belt support 302 connects conveyer belt support arm 314.
2, the shipping loading frame, it is characterised in that: baggage conveyor 301 is that multilayer belt carcass rubber presses conveyer belt.
3, the shipping loading frame, it is characterised in that: rail is slided in the shipping of 306 lower part of sliding platform 310 and hoistable platform Road 305 is two parallel tracks.
4, the shipping loading frame, it is characterised in that: rail is slided in the shipping of 306 lower part of sliding platform 310 and hoistable platform Road 305 is three parallel tracks.
5,310 lower part of sliding platform connects sliding platform idler wheel 311, and sliding platform idler wheel 311 is located at shipping sliding rail On road 305;(effect of sliding platform is by large cargo such as the cargo of container class by being moved under aircraft hold door at a distance Side, then cargo hold doorway is lifted to by hoistable platform 306)
Embodiment 4
1, rear thruster includes: roller 501, roller axle 502, roller support 503, roller spring 504, support 505, connecting rod 506, towing bracket 508, linear motor rotor 509, linear motor stator electric 510;
It is characterized by: rear thruster front end is connected with roller 501, there are roller axle 502, roller axle in the column center of roller 501 502 connection roller supports 503;
Roller support 503 and roller spring 504 have multiple groups, and roller support 503 connects roller spring 504, multiple groups roller 504 connecting support 505 of bracket 503 and roller spring;
Support 505 is the support of strip;Support 505 or so respectively has one, and the center line of two supports is straight in same On line, connecting rod 506 is connected among two supports 505;
Support 505 is located on rear thruster track 102.
2, the rear thruster, it is characterised in that: support 505 connects towing bracket 508, and towing bracket 508 connects straight line Rotor 509;Towing bracket 508 connects linear motor stator electric 510.
3, the rear thruster, it is characterised in that: have spring spool outside roller spring 504.
4, the rear thruster, it is characterised in that: 501 housing rubber sleeve of roller.
5, the rear thruster, it is characterised in that: roller 501 is rubber-plastics material roller.
Embodiment 5
1, the structure of front frame posture aircraft carrying platform, comprising: fuselage profile 1, main landing gear position 2, nose-gear Position 3, main platform body 10, cantilever crane 20, shipping loading frame 30, boarding gantry 40, rear thruster 50, airport track 60;
Main platform body 10 includes: main carrying platform 101, rear thruster track 102, ear platform 103, equipment box 104, transition ramp 105, radial trolley 106, main trolley 107, radial trolley movable axis 108, front chassis 109, nose-gear catch 110, preceding rise and fall Body panel 111;
Cantilever crane 20 includes: cantilever crane track 201, cantilever crane crossbeam 202, cantilever crane trolley 203, pool machine display screen 204, display screen branch Column 205;
There are diesel engine, generator, bleed machine in equipment box 104;
Main carrying platform 101 is "convex" shaped structure in the rear portion of main platform body 10, main platform body 10, and middle and back is square Shape, on both sides of the middle are connected with symmetrical ear platform 103, the part outstanding before main platform body 10 of nose-gear platform 111;Ear Equipment box 104 is housed on platform 103;
Main 101 end of carrying platform connects transition ramp 105;The section of transition ramp 105 is streamlined;Main carrying platform 101 rearward lower is connected with radial trolley 106;Radial trolley 106 is equipped with four wheels below, and four of radial trolley 106 Wheel connects radial trolley movable axis 108;Main trolley 107 is connected with below the middle part of main carrying platform 101;Nose-gear platform Front chassis 109 is connected with below 111 front;Front below be connected with front chassis 109;Cantilever crane track 201 has two groups, every group For parallel rectilinear orbit;Main trolley 107 is equipped with four wheels below;Every group of 201 end of cantilever crane track is separately connected ear platform 103 Front end and nose-gear platform 111;
Organic field track 60 in airport, the track of airport track 60 have parallel four;Radial trolley 106 and main trolley 107 four wheels are located on four tracks on airport track 60;Front chassis 109 is located in two of airport track 60 On siding track;201 front end of cantilever crane track connects cantilever crane crossbeam 202, and cantilever crane crossbeam 202 is between two arms mounted track 201, with arm Mounted track 201 is vertical;The lower linking arm rack trolley 203 of cantilever crane crossbeam 202;The wheel of cantilever crane trolley 203 is respectively seated at airport rail In two inner tracks in road 60;
Shipping loading frame 30 is housed on left side cantilever crane track 201;
Boarding gantry 40 is housed on right arm mounted track 201;
The radial direction trolley 106 is symmetrical 2 pairs;
The radial direction trolley 106 connects radial trolley movable axis 108,
Rear thruster track 102, thruster track 102 after rear thruster 50 connects are housed on the main carrying platform 101;
Nose-gear catch 110 is connected on the nose-gear platform 111, the section of nose-gear catch 110 is ladder Shape catch;
Display screen pillar 205 is connected on 202 middle part of cantilever crane crossbeam, pool machine display screen 204 connects display screen pillar 205;
The application of front frame posture aircraft carrying platform, it is characterised in that:
Step 1: pilot in an aircraft, observes the display data of pool machine display screen 204;
Step 2: when aircraft landing behind ground, slided into main platform body 10 along transition ramp 105, nose-gear wheel Gear 110 withstands aircraft nose-gear;
Step 3: before cantilever crane track 201 of the boarding gantry 40 on cantilever crane 20 moves to the passenger door of aircraft, opening boat The passenger door of pocket makes passenger leave aircraft along boarding gantry 40;At the same time, arm of the shipping loading frame 30 on cantilever crane 20 Mounted track 201 moves to aircraft hold in front of the door, and lower aircraft will be carried with machine cargo by opening cargo door;
Step 4: after passenger and cargo are away from aircraft, front frame posture aircraft carrying platform will navigate along airport track 60 Pocket is transported to stop position.
2, the application of the front frame posture aircraft carrying platform, it is characterised in that:
Step 5: when aircraft will take off, pilot's machine display screen 204 on the berth reads related data;
Step 6: before cantilever crane track 201 of the boarding gantry 40 on cantilever crane 20 moves to the passenger door of aircraft, opening boat The passenger door of pocket makes passenger climb up aircraft along boarding gantry 40;At the same time, arm of the shipping loading frame 30 on cantilever crane 20 Mounted track 201 moves to aircraft hold in front of the door, and aircraft will be transported with the cargo of confidential transport by opening cargo door;
Step 7: closing the passenger door and cargo door of aircraft;
Step 8: aircraft is transported on airport taxiway by front frame posture aircraft carrying platform;
Step 9: aircraft release front frame posture aircraft carrying platform is served taxiway by thruster 50 after starting.
In addition to technical characteristic described herein, remaining is knowledge well known to one of ordinary skill in the art, is not existed herein It repeats.

Claims (2)

1. the application of front frame posture aircraft carrying platform, front frame posture aircraft carrying platform includes: fuselage profile, leads and rise and fall Rack position, nose-gear position, main platform body, cantilever crane, shipping loading frame, boarding gantry, rear thruster, airport track;
Main platform body includes: main carrying platform, rear thruster track, ear platform, equipment box, transition ramp, radial trolley, main trolley, Radial trolley movable axis, front chassis, nose-gear catch, nose-gear platform;
Cantilever crane includes: cantilever crane track, cantilever crane crossbeam, cantilever crane trolley, pool machine display screen, display screen pillar;
There are diesel engine, generator, bleed machine in equipment box;
For main carrying platform at the rear portion of main platform body, main platform body is "convex" shaped structure, and middle and back is rectangle, and on both sides of the middle connects It is connected to symmetrical ear platform, nose-gear platform part outstanding before main platform body;Equipment box is housed on ear platform;
Main carrying platform end connects transition ramp;The section of transition ramp is streamlined;The rearward lower of main carrying platform connects It is connected to radial trolley;Four wheels are housed, the four wheels of radial trolley connect radial trolley movable axis below radial trolley;It is main Main trolley is connected with below the middle part of carrying platform;Front chassis is connected with below the front of nose-gear platform;Cantilever crane track has Two groups, every group is parallel rectilinear orbit;Four wheels are housed below main trolley;Every group of cantilever crane track end is separately connected ear platform Front end and nose-gear platform;
Organic field track in airport, the track of airport track have parallel four;The four wheels of radial trolley and main trolley are equal It is located on four tracks on the track of airport;Front chassis is located in two inner tracks of airport track;Cantilever crane track front end Cantilever crane crossbeam is connected, cantilever crane crossbeam is vertical with cantilever crane track between two arms mounted track;Linking arm pallet under cantilever crane crossbeam Vehicle;The wheel of cantilever crane trolley is respectively seated in two inner tracks of airport track;
Shipping loading frame is housed on the cantilever crane track of left side;
Boarding gantry is housed on right arm mounted track;
The radial direction trolley connects radial trolley movable axis,
Rear thruster track, thruster track after rear thruster connection are housed on the main carrying platform;
Nose-gear catch is connected on the nose-gear platform, the section of nose-gear catch is trapezoidal catch;
Display screen pillar is connected in the middle part of cantilever crane crossbeam, pool machine display screen connects display screen pillar;
The application of front frame posture aircraft carrying platform, it is characterised in that:
Step 1: pilot observes the display data of pool machine display screen in an aircraft;
Step 2: when aircraft landing behind ground, slided into main platform body along transition ramp, nose-gear catch withstands boat Pocket nose-gear;
Step 3: before cantilever crane track of the boarding gantry on cantilever crane moves to the passenger door of aircraft, opening the main cabin of aircraft Door, makes passenger leave aircraft along boarding gantry;At the same time, cantilever crane track of the shipping loading frame on cantilever crane moves to aviation Before device cargo door, lower aircraft will be carried with machine cargo by opening cargo door;
Step 4: after passenger and cargo are away from aircraft, front frame posture aircraft carrying platform transports aircraft along airport track It is sent to stop position.
2. the application of front frame posture aircraft carrying platform as described in claim 1, it is characterised in that:
Step 5: when aircraft will take off, pilot's machine display screen on the berth reads related data;
Step 6: before cantilever crane track of the boarding gantry on cantilever crane moves to the passenger door of aircraft, opening the passenger door of aircraft Passenger is set to climb up aircraft along boarding gantry;At the same time, cantilever crane track of the shipping loading frame on cantilever crane moves to aircraft Before cargo door, aircraft will be transported with the cargo of confidential transport by opening cargo door;
Step 7: closing the passenger door and cargo door of aircraft;
Step 8: aircraft is transported on airport taxiway by front frame posture aircraft carrying platform;
Step 9: aircraft release front frame posture aircraft carrying platform is served taxiway by thruster after starting.
CN201610796137.1A 2016-08-31 2016-08-31 The application of front frame posture aircraft carrying platform Active CN106628229B (en)

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KR20110058023A (en) * 2009-11-25 2011-06-01 (주)에이비텍 The boarding bridge with minute approaching device and shock-absorber part and operation method thereof
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CN101982373B (en) * 2010-10-14 2014-09-10 深圳市好时代专用挂车有限公司 Boarding vehicle
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