CN106628228B - The application of thruster afterwards - Google Patents
The application of thruster afterwards Download PDFInfo
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- CN106628228B CN106628228B CN201610777567.9A CN201610777567A CN106628228B CN 106628228 B CN106628228 B CN 106628228B CN 201610777567 A CN201610777567 A CN 201610777567A CN 106628228 B CN106628228 B CN 106628228B
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- roller
- support
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND 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
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/22—Ground or aircraft-carrier-deck installations installed for handling aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND 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
- B64F1/00—Ground or aircraft-carrier-deck installations
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND 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
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/36—Other airport installations
Abstract
Thruster application afterwards is related to air transportation ground-support equipment applied technical field.It include: roller, roller axle, roller support, roller spring, support, connecting rod, towing bracket, linear motor rotor, linear motor stator electric；It is characterized by: step 1: when aircraft needs to set sail, pilot enters aircraft, and after pilot obtains the instruction of setting sail of ground aviation management system, pilot assigns instruction to thruster after ground installation；Step 2: the main carrying platform of main platform body takes aircraft by taxiway to；Step 3: pilot assigns thruster after instruction is opened, and the towing bracket of rear thruster moves backward along rear thruster track, and support is driven to move backward；Step 4: the roller of rear thruster then pushes the main landing gear of aircraft to move backward；Step 6: rear thruster by aircraft along transition ramp push down main carrying platform after reset.
Description
Technical field
The application of thruster afterwards is related to air transportation ground-support equipment applied technical field.
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 make great efforts to mitigate air transportation visitor, flow of goods pressure；
The fifth purpose of the application is the large-scale ground trailer of substitution, and investment reduction cuts operating costs.
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；
Airport track 60 has four parallel tracks；
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 I innings of Figure 18 convenient for aircraft along transition ramp uplink
Portion's enlarged drawing)；
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, 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；
A set of roller support 503 and roller spring 504 are one group, and roller support 503 and roller spring 504 have multiple groups,
Roller support 503 connects roller spring 504,504 connecting support 505 of multiple groups roller support 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.
6, the rear thruster, it is characterised in that: roller support 503 and roller spring 504 have four groups.
7, the rear thruster, it is characterised in that: roller support 503 and roller spring 504 have eight groups.
(be detailed in Figure of description Figure 11-13 and Figure 20, the effect of other figures be after further reflection thruster in the application
Effect in technical solution)
Three, the application of rear thruster
1, rear thruster includes: roller 501, roller axle 502, roller support 503, roller spring 504, support 505, connection
Bar 506, towing bracket 508, linear motor rotor 509, linear motor stator electric 510；
Thruster front end is connected with roller 501 afterwards, and there is roller axle 502 at the column center of roller 501, and roller axle 502 connects roller
Bracket 503；
A set of roller support 503 and roller spring 504 are one group, and roller support 503 and roller spring 504 have multiple groups,
Roller support 503 connects roller spring 504,504 connecting support 505 of multiple groups roller support 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 on same straight line, two supports 505
Centre connection connecting rod 506；Support 505 is located on rear thruster track 102；
Support 505 connects towing bracket 508, and towing bracket 508 connects linear motor rotor 509；Towing bracket 508 connects
Linear motor stator electric 510；
Afterwards thruster application it is characterized by:
Step 1: when aircraft needs to set sail, pilot enters aircraft, and pilot obtains rising for ground aviation management system
After boat instruction, pilot assigns instruction to thruster after ground installation；
Step 2: the main carrying platform 101 of main platform body 10 takes aircraft by taxiway to；
Step 3: pilot assign instruction open after thruster, the towing bracket 508 of rear thruster along rear thruster track 102 backward
Movement, (i.e. just in the opposite direction with aircraft head and the tail) drive support 505 to move backward；
Step 4: the roller 501 of rear thruster then pushes the main landing gear of aircraft to move backward；(roller can roll guarantor
Protecting main landing gear reduces abrasion)
Step 5: rear thruster by aircraft along transition ramp 105 push down main carrying platform 101 after reset.
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, aircraft surface trailer is substituted.
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；
Airport track 60 has four parallel tracks；
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 I innings of Figure 18 convenient for aircraft along transition ramp uplink
Portion's enlarged drawing)；
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, 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；
A set of roller support 503 and roller spring 504 are one group, and roller support 503 and roller spring 504 have multiple groups,
Roller support 503 connects roller spring 504,504 connecting support 505 of multiple groups roller support 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.
6, the rear thruster, it is characterised in that: roller support 503 and roller spring 504 have four groups.
7, the rear thruster, it is characterised in that: roller support 503 and roller spring 504 have eight groups.
Embodiment 3
1, rear thruster includes: roller 501, roller axle 502, roller support 503, roller spring 504, support 505, connection
Bar 506, towing bracket 508, linear motor rotor 509, linear motor stator electric 510；
Thruster front end is connected with roller 501 afterwards, and there is roller axle 502 at the column center of roller 501, and roller axle 502 connects roller
Bracket 503；
A set of roller support 503 and roller spring 504 are one group, and roller support 503 and roller spring 504 have multiple groups,
Roller support 503 connects roller spring 504,504 connecting support 505 of multiple groups roller support 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 on same straight line, two supports 505
Centre connection connecting rod 506；Support 505 is located on rear thruster track 102；
Support 505 connects towing bracket 508, and towing bracket 508 connects linear motor rotor 509；Towing bracket 508 connects
Linear motor stator electric 510；
Afterwards thruster application it is characterized by:
Step 1: when aircraft needs to set sail, pilot enters aircraft, and pilot obtains rising for ground aviation management system
After boat instruction, pilot assigns instruction to thruster after ground installation；
Step 2: the main carrying platform 101 of main platform body 10 takes aircraft by taxiway to；
Step 3: pilot assign instruction open after thruster, the towing bracket 508 of rear thruster along rear thruster track 102 backward
Movement, (i.e. just in the opposite direction with aircraft head and the tail) drive support 505 to move backward；
Step 4: the roller 501 of rear thruster then pushes the main landing gear of aircraft to move backward；(roller can roll guarantor
Protecting main landing gear reduces abrasion)
Step 5: rear thruster by aircraft along transition ramp 105 push down main carrying platform 101 after reset.
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 (1)
1. the application of thruster after, rear thruster include: roller, roller axle, roller support, roller spring, support, connecting rod, traction
Bracket, linear motor rotor, linear motor stator electric；
Thruster front end is connected with roller afterwards, and there are roller axle, roller axis connection roller support in the column center of roller；
A set of roller support and roller spring are one group, and roller support and roller spring have multiple groups, and roller support connects roller
Spring, multiple groups roller support and roller spring connecting support；
Support is the support of strip；Support or so respectively has one, and the center line of two supports is on same straight line, two branch
Seat is intermediate to connect connecting rod；Support is located on rear thruster track；
Support connects towing bracket, and towing bracket connects linear motor rotor；Towing bracket connects linear motor stator electric；
The application of thruster afterwards, it is characterised in that:
Step 1: when aircraft needs to set sail, pilot enters aircraft, and pilot obtains the finger that sets sail of ground aviation management system
After order, pilot assigns instruction to thruster after ground installation；
Step 2: the main carrying platform of main platform body takes aircraft by taxiway to；
Step 3: pilot assigns thruster after instruction is opened, and the towing bracket of rear thruster moves backward along rear thruster track, drives
Support moves backward；
Step 4: the roller of rear thruster then pushes the main landing gear of aircraft to move backward；
Step 5: rear thruster by aircraft along transition ramp push down main carrying platform after reset.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610777567.9A CN106628228B (en) | 2016-08-31 | 2016-08-31 | The application of thruster afterwards |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610777567.9A CN106628228B (en) | 2016-08-31 | 2016-08-31 | The application of thruster afterwards |
Publications (2)
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| CN106628228A CN106628228A (en) | 2017-05-10 |
| CN106628228B true CN106628228B (en) | 2018-12-21 |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1990011933A1 (en) * | 1989-03-31 | 1990-10-18 | Tana-Jyrä Ky | A wheeled transfer device for moving an aircraft |
| DE3931646A1 (en) * | 1989-09-22 | 1991-04-04 | Gutehoffnungshuette Man | Towing aircraft tractor without tow-bar - has gripper and sensor rollers mounted on swing arm on parallel axis |
| US5248115A (en) * | 1991-06-12 | 1993-09-28 | Riva Calzoni S.P.A. | Device for gripping and handling helicopters, particularly for ships' decks, platforms and the like |
| CN103025610A (en) * | 2010-06-09 | 2013-04-03 | 以色列宇航工业有限公司 | Vehicle for towing an airplane |
| CN205366100U (en) * | 2015-09-22 | 2016-07-06 | 成都成设航空科技有限公司 | Aircraft draw gear |
-
2016
- 2016-08-31 CN CN201610777567.9A patent/CN106628228B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1990011933A1 (en) * | 1989-03-31 | 1990-10-18 | Tana-Jyrä Ky | A wheeled transfer device for moving an aircraft |
| DE3931646A1 (en) * | 1989-09-22 | 1991-04-04 | Gutehoffnungshuette Man | Towing aircraft tractor without tow-bar - has gripper and sensor rollers mounted on swing arm on parallel axis |
| US5248115A (en) * | 1991-06-12 | 1993-09-28 | Riva Calzoni S.P.A. | Device for gripping and handling helicopters, particularly for ships' decks, platforms and the like |
| CN103025610A (en) * | 2010-06-09 | 2013-04-03 | 以色列宇航工业有限公司 | Vehicle for towing an airplane |
| CN205366100U (en) * | 2015-09-22 | 2016-07-06 | 成都成设航空科技有限公司 | Aircraft draw gear |
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| CN106628228A (en) | 2017-05-10 |
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Effective date of registration: 20191128 Address after: 314205 No. 1 Cangqing Road, Xincang Town, Pinghu City, Jiaxing City, Zhejiang Province Patentee after: Zhejiang Huanyu Auto Parts Co., Ltd Address before: 314400 room 2, building five, 303 Li, Nanyuan, Jiaxing, Haining, Zhejiang Patentee before: Ma Hong |