CN106608365A - Front frame aircraft carrying platform - Google Patents
Front frame aircraft carrying platform Download PDFInfo
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- CN106608365A CN106608365A CN201610796243.XA CN201610796243A CN106608365A CN 106608365 A CN106608365 A CN 106608365A CN 201610796243 A CN201610796243 A CN 201610796243A CN 106608365 A CN106608365 A CN 106608365A
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- Prior art keywords
- platform
- track
- chassis
- arm support
- main
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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
- B64F1/225—Towing trucks
- B64F1/227—Towing trucks adapted for directly connecting to aircraft, e.g. trucks without tow-bars
Abstract
The invention discloses a front frame aircraft carrying platform, and relates to the technical field of transportation equipment. The front frame aircraft carrying platform is characterized in that a main bearing platform is at the back part of a platform main body; the platform main body is a convex structure; the middle back part is rectangular; two sides of the middle are connected with left and right symmetric lug tables; a front undercarriage platform is at the projected part in front of the platform main body; equipment boxes are mounted on the lug tables; the tail end of the main bearing platform is connected with a transition slope way; the section of the transition slope way is streamlined; a radial trolley is connected below the back part of the main bearing platform; four wheels are mounted below the radial trolley; the four wheels of the radial trolley are connected with a movable shaft of the radial trolley; a main trolley is connected below the middle part of the main bearing platform; a front trolley is connected below the front part of the front undercarriage platform, and is placed on two inner rails of airport rails; the front end of an arm frame rail is connected with an arm frame cross beam; and wheels of an arm rest trolley are respectively placed on two inner side rails of the airport rails.
Description
Technical field
Front frame posture airborne vehicle carrying platform, is related to equipment technology field of transport.
Background technology
With the fast development of high speed information industry, adaptable transport service is also in fast development therewith.Trip, material flow
Logical speed all make rapid progress quietly occur change, the radius of action of people is increasing, and the scope of logistics is got over
Come wider.Air-transport industry quickly grows, and in recent years for the country, constantly expands newly-increased course line, expands airport.
It is inadaptable that the course line that ground installation related to shipping increasingly highlights aviation development is brought.
The content of the invention
It is well known that the people for taking airborne vehicle (aircraft) perhaps notice airborne vehicle on ground or take off or land
Different from automobile, drop (wheel) during aircraft lands, then with airborne vehicle engine (turbofan, if
Will be bigger using turbojet oil consumption) it is mover runner to airplane parking area, therefore oil consumption is big (particularly in airborne vehicle low speed
When being moved below 80 section, oil consumption is especially huge), noise is big, easy Foreign body aspiration causes failure, inhaled if personnel walk about
The danger for entering.As " aerial liner of numbering AI619 will be flown to Hyderabad from Mumbai, at that time due to airborne vehicle copilot
Get signal wrong, when starting engine, a ground crew is inhaled in engine.”
To overcome the shortcomings of that prior art is present：
One of purpose of the application is that instead of ground go-cart traction airborne vehicle；
The two of the purpose of the application are to reduce airborne vehicle oil consumption, as far as possible using surface power supply supplying oil and gas；
The three of the purpose of the application are that the ground for improving airborne vehicle is risen and fallen safety；
The four of the purpose of the application are to mitigate visitor, flow of goods pressure.
The application is adopted the following technical scheme that for achieving the above object：
First, front frame posture airborne vehicle carrying platform
1st, front frame posture airborne vehicle carrying platform, including：Fuselage profile 1, main landing gear position 2, nose-gear position 3,
Main platform body 10, arm support 20, shipping loading frame 30, boarding crane span structure 40, rear thruster 50, airport track 60；
Main platform body 10 is included：Main carrying platform 101, rear thruster track 102, ear platform 103, equipment box 104, transition ramp
105th, radial direction chassis 106, main chassis 107, radial direction chassis movable axis 108, front chassis 109, nose-gear catch 110, front rise and fall
Body panel 111；
Arm support 20 is included：Arm support track 201, arm support crossbeam 202, arm support chassis 203, pool machine display screen 204, display screen
Post 205；
Shipping loading frame 30 is included：Baggage conveyor 301, belt support 302, loading frame end carriage 303, shipping slip rail
Road 305, hoistable platform 306, crane 307, hoistable platform base 308, hoistable platform roller 309, sliding platform 310, slip
Platform roller 311；
Boarding crane span structure 40 is included：Connecting bridge 401, flexible airstair 402, bridge-frame end-beam 403, crane span structure sliding rail 405, step on
Machine mouth 406, flexible vestibule diaphragm 407, shelter bridge supporting plate 408, crane 409, crane span structure roller 410；
Airport track 60 has four parallel tracks；
There are diesel engine, electromotor, bleed machine in equipment box 104；(diesel engine, electromotor, bleed machine in equipment box is to boat
Pocket is powered, is supplied；Diesel engine, electromotor, bleed machine are existing equipment and repeat no more)
It is characterized in that：
Main carrying platform 101 is "convex" shaped structure in the rear portion of main platform body 10, main platform body 10, and postmedian is square
Shape, middle part both sides are connected with symmetrical ear platform 103, the prominent part before main platform body 10 of nose-gear platform 111；
Equipment box 104 is housed on ear platform 103；
Connection transition ramp 105 in 101 end of main carrying platform (is easy to airborne vehicle to refer to I local of figure along transition ramp is up
Enlarged drawing)；
The section of transition ramp 105 is streamlined；
The rearward lower of main carrying platform 101 is connected with radial direction chassis 106；
Radial direction chassis 106 is equipped with four wheels, the four wheels connection radial direction chassis movable axis of radial direction chassis 106 below
108；(being easy to turn along airport track 60)
Main chassis 107 is connected with below the middle part of main carrying platform 101；The front portion of nose-gear platform 111 connects below
There are front chassis 109；
Arm support track 201 has two groups, and per group is parallel rectilinear orbit；
Main chassis 107 is equipped with four wheels below；
Distinguish 103 front end of engaging lug platform and nose-gear platform 111 in every group of 201 end of arm support track；
Organic field track 60 in airport, the track of airport track 60 have parallel four；Sliding for prior art is substituted (
Road)
The four wheels of radial direction chassis 106 and main chassis 107 are seated on four tracks on airport track 60；Front chassis
109 are seated in two inner tracks of airport track 60；
201 front end of arm support track connection arm support crossbeam 202, arm support crossbeam 202 between two arms mounted track 201, with arm
Mounted track 201 is vertical；
202 times linking arm rack trolleys 203 of arm support crossbeam；The wheel of arm support chassis 203 is respectively seated at airport track 60
In two inner tracks (203 supporting arm frame tracks 201 of arm support chassis, arm support crossbeam 202, and overall front frame posture can be supported
Airborne vehicle carrying platform is moved on airport track 60)
Shipping loading frame 30 is housed on left side arm support track 201；(helping goods to transport airborne vehicle)
Boarding crane span structure 40 is housed on right arm mounted track 201；(shelter bridge of existing equipment is substituted, passenger can be made to pass through boarding
Crane span structure 40 climbs up airborne vehicle, and alleviates because of airborne vehicle landing frequently congestion)
(referring to Figure of description 1-5,17-19)
2nd, described front frame posture airborne vehicle carrying platform, it is characterised in that：Described radial direction chassis 106 is symmetrical
2 couple.(bearing capacity is big)
3rd, described front frame posture airborne vehicle carrying platform, it is characterised in that：The radial direction chassis 106 connects radial direction chassis
Movable axis 108, (being easy to main carrying platform 101 to turn)
4th, described front frame posture airborne vehicle carrying platform, it is characterised in that：After being equipped with described main carrying platform 101
Thruster track 102, thruster track 102 after the connection of rear thruster 50.(because the engine of airborne vehicle can only carry out retreating,
So install rear thruster additional can be easy to for airborne vehicle to push main carrying platform 101)
5th, described front frame posture airborne vehicle carrying platform, it is characterised in that：Connect on described nose-gear platform 111
Nose-gear catch 110, the section of nose-gear catch 110 is trapezoidal catch.(being easy to stop airborne vehicle nose-gear)
6th, described front frame posture airborne vehicle carrying platform, it is characterised in that：It is connected with the middle part of arm support crossbeam 202 aobvious
Display screen pillar 205, pool machine display screen 204 connect display screen pillar 205.(so that pilot's observed data)
7th, described front frame posture airborne vehicle carrying platform, it is characterised in that：Nose-gear catch 110 is rubber catch.
8th, described front frame posture airborne vehicle carrying platform, it is characterised in that：Generator cable connection in equipment box 104
Airborne vehicle.(APU on the airborne vehicle of alternative prior art)
9th, described front frame posture airborne vehicle carrying platform, it is characterised in that：Bleed machine gas source pipe in equipment box 104
Connection airborne vehicle.(APU on the airborne vehicle of alternative prior art, so-called APU are to load to be used on the airborne vehicle of prior art
The device of airborne vehicle engine start premise power supply source and source of the gas)
10th, described front frame posture airborne vehicle carrying platform, it is characterised in that：Generator cable in equipment box 104 connects
Connect rear thruster 50 electric power is provided for rear thruster.
11st, described front frame posture airborne vehicle carrying platform, it is characterised in that：Generator cable in equipment box 104 connects
Connect boarding crane span structure 40 to power for boarding crane span structure 40.
12nd, described front frame posture airborne vehicle carrying platform, it is characterised in that：Generator cable in equipment box 104 connects
Connect shipping loading frame 30 to power for shipping loading frame 30.
13rd, described front frame posture airborne vehicle carrying platform, it is characterised in that：Bleed machine in equipment box 104 is aviation
Electromotor supply in device.
14th, described front frame posture airborne vehicle carrying platform, it is characterised in that：Bleed machine in equipment box 104 is aviation
Air-conditioning supply in device.
2nd, portable shelter bridge
1st, portable shelter bridge, including：Connecting bridge 401, flexible airstair 402, bridge-frame end-beam 403, crane span structure sliding rail
405th, boarding gate 406, flexible vestibule diaphragm 407, shelter bridge supporting plate 408, crane 409, crane span structure roller 410, bridge import 411, rolling bridge wheel
412；
It is characterized in that：Portable shelter bridge main body be boarding crane span structure 40, connecting bridge 401 connection boarding gate 406, boarding gate
The flexible vestibule diaphragm 407 of 406 connections, (when being easy to passenger to pass through airport lounge boarding, 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 of the airstair 402 that stretches, lower end cross structure import
411；
411 bottom of bridge import connects crane span structure roller 410；Crane span structure roller 410 is seated on crane span structure sliding rail 405, crane span structure
405 two ends of sliding rail connect bridge-frame end-beam 403；
Rolling bridge wheel 412 is seated on arm support track 201；
401 bottom connecting corridor bridgework plate 408 of connecting bridge, shelter bridge supporting plate 408 connect two groups of cranes 409；
2nd, described portable shelter bridge, it is characterised in that：Connecting bridge 401 is horizontal connecting bridge.
3rd, described portable shelter bridge, it is characterised in that：Described flexible vestibule diaphragm 407 is rubber and plastic flexibility vestibule diaphragm.
4th, described portable shelter bridge, it is characterised in that：Roller of the described rolling bridge wheel 412 for set rubber.
5th, described portable shelter bridge, it is characterised in that：Roller of the described crane span structure roller 410 for set rubber.
3rd, shipping loading frame
1st, shipping loading frame 30 is included：Baggage conveyor 301, belt support 302, loading frame end carriage 303, conveyer belt are low
End bearing 304, shipping sliding rail 305, hoistable platform 306, crane 307, hoistable platform base 308, hoistable platform roller
309th, the high-end bearing slide block 313, conveyer belt of sliding platform 310, sliding platform roller 311, loading frame roller 312, conveyer belt
Brace 314, belt support 302；
It is characterized in that：
Baggage conveyor 301 is flat conveyer belt, and higher end is low；(it is easy to for goods to be sent to height by lower
Place) baggage conveyor 301 low side and high-end is connected to two groups of belt supports 302, two groups of conveyer belts of low side below
302 times connection conveyer belt low side bearings 304 of frame；The high-end high-end bearing slide block of two groups of belt supports, 302 times connection conveyer belts
313；(the high-end bearing slide block of conveyer belt 313 is raised and lowered can the high-end of conveyer belt along 305 movement of shipping sliding rail, just
In conveyer belt is aligned the aircraft hold door that type is different and height is different, spare parts of goods can be incited somebody to action with baggage conveyor 301
Goods is transported to aircraft hold)
The connection of conveyer belt low side bearing 304 shipping sliding rail 305, the high-end bearing slide block of conveyer belt 313 are sleeved on shipping
On sliding rail 305；
306 bottom of hoistable platform connects crane 307, the crane of 307 staggered form of crane；
307 times connection hoistable platform bases 308 of crane；The connection hoistable platform of hoistable platform base 308 roller 309；Rise
Drop platform roller 309 is seated on shipping sliding rail 305；
The two ends of shipping sliding rail 305 are all connected with loading frame end carriage 303；
303 times connection loading frame rollers 312 of loading frame end carriage；Loading frame roller 312 is seated on arm support track 201；
The connection conveyer belt of belt support 302 support arm 314.
2nd, the shipping loading frame, it is characterised in that：Baggage conveyor 301 is that multilamellar belt carcass rubber presses conveyer belt.
3rd, the shipping loading frame, it is characterised in that：The shipping slip rail of 306 bottom of sliding platform 310 and hoistable platform
Road 305 is two parallel tracks.
4th, the shipping loading frame, it is characterised in that：The shipping slip rail of 306 bottom of sliding platform 310 and hoistable platform
Road 305 is three parallel tracks.
5th, 310 bottom of sliding platform connection sliding platform roller 311, sliding platform roller 311 is seated in shipping slip rail
On road 305；(effect of sliding platform is by being moved under aircraft hold door at a distance by the goods of large cargo such as container class
Side, then cargo hold doorway is lifted to by hoistable platform 306)
4th, rear thruster
1st, rear thruster is included：Roller 501, roller axle 502, roller support 503, roller spring 504, bearing 505, connecting rod
506th, towing bracket 508, linear motor rotor 509, linear motor stator electric 510；
It is characterized in that：Thruster front end is connected with roller 501 afterwards, and there are roller axle 502, roller axle in the post center of roller 501
502 connection roller supports 503；
Roller support 503 and roller spring 504 have multigroup, the connection roller of roller support 503 spring 504, multigroup roller
504 connects bearing 505 of support 503 and roller spring；
Bearing of the bearing 505 for strip；Bearing 505 or so respectively has one, and the centrage of two bearings is straight in same
On line, in the middle of two bearings 505, connect connecting rod 506；
Bearing 505 is seated on rear thruster track 102.
2nd, described rear thruster, it is characterised in that：Bearing 505 connects towing bracket 508, the connection straight line of towing bracket 508
Rotor 509；Towing bracket 508 connects linear motor stator electric 510.
3rd, described rear thruster, it is characterised in that：There is spring spool outside roller spring 504.
4th, described rear thruster, it is characterised in that：501 overcoat rubber sleeve of roller.
5th, described rear thruster, it is characterised in that：Roller 501 is rubber-plastics material roller.
Beneficial effect
1st, as the present invention is fuel-efficient compared with ground mover using driven by power.
2nd, compared with the ground mover of prior art, (can be airborne vehicle under normal circumstances, it is also possible to use in airborne vehicle
In other airborne vehicles such as dirigible) directly draw after gun off the runway, save airborne vehicle fuel oil.
3rd, compared with the ground mover of prior art, (can be airborne vehicle under normal circumstances, it is also possible to use in airborne vehicle
In other airborne vehicles such as dirigible) directly draw after gun off the runway, (such as airborne vehicle starts to save the abrasion of airborne vehicle critical component
Machine etc.).
4th, the loading capacity of airborne vehicle it is big such as 380 type passenger planes of Air Passenger company, 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 man-hour carves cleaning, and track then need not.
5th, because airplane parking area needs the ground of high intensity, and the platform of the application is located on track, therefore is saved
The airplane parking area of high intensity.
6th, by the rear thruster in main platform body 10, save airport trailer.
Description of the drawings
Fig. 1：Front frame posture airborne vehicle carrying platform top view
Fig. 2：Front frame posture airborne vehicle carrying platform A-A faces schematic diagram
Fig. 3：Front frame posture airborne vehicle carrying platform B-B faces schematic diagram
Fig. 4：Front frame posture airborne vehicle carrying platform C-C faces schematic diagram
Fig. 5：Front frame posture airborne vehicle carrying platform and aircraft position schematic side view
Fig. 6：Boarding crane span structure front view
Fig. 7：Boarding crane span structure left view
Fig. 8：Boarding crane span structure right view
Fig. 9：Shipping loading frame front view
Figure 10：Shipping loading frame rearview
Figure 11：Thruster main view enlarged drawing afterwards
Figure 12：Thruster A is to partial enlarged drawing afterwards
Figure 13：Thruster top view afterwards
Figure 14：Arm support chassis front view
Figure 15：Arm support chassis left view
Figure 16：Arm support chassis top view
Figure 17：Airport track top view
Figure 18：I partial enlarged drawing
Figure 19：II partial enlarged drawing
Figure 20：III partial enlarged drawing
Figure 21：IV partial enlarged drawing
Figure 22：V partial enlarged drawing
Figure 23：VI partial enlarged drawing
Figure 24：VII partial enlarged drawing
In figure：1 fuselage profile, 2 main landing gear positions, 3 nose-gear positions, 10 main platform bodies, 20 arm supports, 30 shippings dress
Carrier, 40 boarding crane span structures, thruster after 50,60 airport tracks,
101 main carrying platforms, thruster track, 103 ear platforms, 104 equipment boxs, 105 transition ramps, 106 radial direction platforms after 102
Car, 107 main chassis, 108 radial direction chassis movable axis, 109 front chassis, 110 nose-gear catch, 111 nose-gear platforms,
201 arm support tracks, 202 arm support crossbeams, 203 arm support chassis, 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 bearings, 305 shippings are slided
Dynamic rail road, 306 hoistable platforms, 307 cranes, 308 hoistable platform bases, 309 hoistable platform rollers, 310 sliding platforms, 311
Sliding platform roller, 312 loading frame rollers, the high-end bearing slide block of 313 conveyer belts, 314 conveyer belt support arms,
It is 401 connecting bridges, 402 flexible airstairs, 403 bridge-frame end-beams, 405 crane span structure sliding rails, 406 boarding gates, 407 flexible
Vestibule diaphragm, 408 shelter bridge supporting plates, 409 cranes, 410 crane span structure rollers, 411 bridge imports, 412 rolling bridge wheels,
501 rollers, 502 roller axles, 503 roller supports, 504 roller springs, 505 bearings, 506 connecting rods, 508 tractions
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.
Note 1：II partial enlarged drawings of Figure 19 are a partial enlarged drawings of arm support chassis front view, it is intended that indicate arm support chassis
Position during use.
Note 2：IV partial enlarged drawings of Figure 21 are actual be exactly shipping loading frame 30 top view, IV partial enlargement can be with reference to figure
1 front frame posture airborne vehicle carrying platform top view more clearly reflects its position being located and effect.
Specific embodiment
With reference to the accompanying drawings and examples the application is described further.
Embodiment 1
1st, front frame posture airborne vehicle carrying platform, including：Fuselage profile 1, main landing gear position 2, nose-gear position 3,
Main platform body 10, arm support 20, shipping loading frame 30, boarding crane span structure 40, rear thruster 50, airport track 60；
Main platform body 10 is included：Main carrying platform 101, rear thruster track 102, ear platform 103, equipment box 104, transition ramp
105th, radial direction chassis 106, main chassis 107, radial direction chassis movable axis 108, front chassis 109, nose-gear catch 110, front rise and fall
Body panel 111；
Arm support 20 is included：Arm support track 201, arm support crossbeam 202, arm support chassis 203, pool machine display screen 204, display screen
Post 205；
Shipping loading frame 30 is included：Baggage conveyor 301, belt support 302, loading frame end carriage 303, shipping slip rail
Road 305, hoistable platform 306, crane 307, hoistable platform base 308, hoistable platform roller 309, sliding platform 310, slip
Platform roller 311；
Boarding crane span structure 40 is included：Connecting bridge 401, flexible airstair 402, bridge-frame end-beam 403, crane span structure sliding rail 405, step on
Machine mouth 406, flexible vestibule diaphragm 407, shelter bridge supporting plate 408, crane 409, crane span structure roller 410；
Airport track 60 has four parallel tracks；
There are diesel engine, electromotor, bleed machine in equipment box 104；(diesel engine, electromotor, bleed machine in equipment box is to boat
Pocket is powered, is supplied；Diesel engine, electromotor, bleed machine are existing equipment and repeat no more)
It is characterized in that：
Main carrying platform 101 is "convex" shaped structure in the rear portion of main platform body 10, main platform body 10, and postmedian is square
Shape, middle part both sides are connected with symmetrical ear platform 103, the prominent part before main platform body 10 of nose-gear platform 111；
Equipment box 104 is housed on ear platform 103；
Connection transition ramp 105 in 101 end of main carrying platform (is easy to airborne vehicle to refer to I local of figure along transition ramp is up
Enlarged drawing)；
The section of transition ramp 105 is streamlined；
The rearward lower of main carrying platform 101 is connected with radial direction chassis 106；
Radial direction chassis 106 is equipped with four wheels, the four wheels connection radial direction chassis movable axis of radial direction chassis 106 below
108；(being easy to turn along airport track 60)
Main chassis 107 is connected with below the middle part of main carrying platform 101；The front portion of nose-gear platform 111 connects below
There are front chassis 109；
Arm support track 201 has two groups, and per group is parallel rectilinear orbit；
Main chassis 107 is equipped with four wheels below；
Distinguish 103 front end of engaging lug platform and nose-gear platform 111 in every group of 201 end of arm support track；
Organic field track 60 in airport, the track of airport track 60 have parallel four；Sliding for prior art is replaced (
Road)
The four wheels of radial direction chassis 106 and main chassis 107 are seated on four tracks on airport track 60；Front chassis
109 are seated in two inner tracks of airport track 60；
201 front end of arm support track connection arm support crossbeam 202, arm support crossbeam 202 between two arms mounted track 201, with arm
Mounted track 201 is vertical；
202 times linking arm rack trolleys 203 of arm support crossbeam；The wheel of arm support chassis 203 is respectively seated at airport track 60
In two inner tracks (203 supporting arm frame tracks 201 of arm support chassis, arm support crossbeam 202, and overall front frame posture can be supported
Airborne vehicle carrying platform is moved on airport track 60)
Shipping loading frame 30 is housed on left side arm support track 201；(helping goods to transport airborne vehicle)
Boarding crane span structure 40 is housed on right arm mounted track 201；(shelter bridge of existing equipment is substituted, passenger can be made to pass through boarding
Crane span structure 40 climbs up airborne vehicle, and alleviates because of airborne vehicle landing frequently congestion)
2nd, described front frame posture airborne vehicle carrying platform, it is characterised in that：Described radial direction chassis 106 is symmetrical
2 couple.(bearing capacity is big)
3rd, described front frame posture airborne vehicle carrying platform, it is characterised in that：The radial direction chassis 106 connects radial direction chassis
Movable axis 108, (being easy to main carrying platform 101 to turn)
4th, described front frame posture airborne vehicle carrying platform, it is characterised in that：After being equipped with described main carrying platform 101
Thruster track 102, thruster track 102 after the connection of rear thruster 50.(because the engine of airborne vehicle can only carry out retreating,
So install rear thruster additional can be easy to for airborne vehicle to push main carrying platform 101)
5th, described front frame posture airborne vehicle carrying platform, it is characterised in that：Connect on described nose-gear platform 111
Nose-gear catch 110, the section of nose-gear catch 110 is trapezoidal catch.(being easy to stop airborne vehicle nose-gear)
6th, described front frame posture airborne vehicle carrying platform, it is characterised in that：It is connected with the middle part of arm support crossbeam 202 aobvious
Display screen pillar 205, pool machine display screen 204 connect display screen pillar 205.(so that pilot's observed data)
7th, described front frame posture airborne vehicle carrying platform, it is characterised in that：Nose-gear catch 110 is rubber catch.
8th, described front frame posture airborne vehicle carrying platform, it is characterised in that：Generator cable connection in equipment box 104
Airborne vehicle.(APU on the airborne vehicle of alternative prior art)
9th, described front frame posture airborne vehicle carrying platform, it is characterised in that：Bleed machine gas source pipe in equipment box 104
Connection airborne vehicle.(APU on the airborne vehicle of alternative prior art, so-called APU are to load to be used on the airborne vehicle of prior art
The device of airborne vehicle engine start premise power supply source and source of the gas)
10th, described front frame posture airborne vehicle carrying platform, it is characterised in that：Generator cable in equipment box 104 connects
Connect rear thruster 50 electric power is provided for rear thruster.
11st, described front frame posture airborne vehicle carrying platform, it is characterised in that：Generator cable in equipment box 104 connects
Connect boarding crane span structure 40 to power for boarding crane span structure 40.
12nd, described front frame posture airborne vehicle carrying platform, it is characterised in that：Generator cable in equipment box 104 connects
Connect shipping loading frame 30 to power for shipping loading frame 30.
13rd, described front frame posture airborne vehicle carrying platform, it is characterised in that：Bleed machine in equipment box 104 is aviation
Electromotor supply in device.
14th, described front frame posture airborne vehicle carrying platform, it is characterised in that：Bleed machine in equipment box 104 is aviation
Air-conditioning supply in device.
Embodiment 2
1st, portable shelter bridge, including：Connecting bridge 401, flexible airstair 402, bridge-frame end-beam 403, crane span structure sliding rail
405th, boarding gate 406, flexible vestibule diaphragm 407, shelter bridge supporting plate 408, crane 409, crane span structure roller 410, bridge import 411, rolling bridge wheel
412；
It is characterized in that：Portable shelter bridge main body be boarding crane span structure 40, connecting bridge 401 connection boarding gate 406, boarding gate
The flexible vestibule diaphragm 407 of 406 connections, (when being easy to passenger to pass through airport lounge boarding, 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 of the airstair 402 that stretches, lower end cross structure import
411；
411 bottom of bridge import connects crane span structure roller 410；Crane span structure roller 410 is seated on crane span structure sliding rail 405, crane span structure
405 two ends of sliding rail connect bridge-frame end-beam 403；
Rolling bridge wheel 412 is seated on arm support track 201；
401 bottom connecting corridor bridgework plate 408 of connecting bridge, shelter bridge supporting plate 408 connect two groups of cranes 409；
2nd, described portable shelter bridge, it is characterised in that：Connecting bridge 401 is horizontal connecting bridge.
3rd, described portable shelter bridge, it is characterised in that：Described flexible vestibule diaphragm 407 is rubber and plastic flexibility vestibule diaphragm.
4th, described portable shelter bridge, it is characterised in that：Roller of the described rolling bridge wheel 412 for set rubber.
5th, described portable shelter bridge, it is characterised in that：Roller of the described crane span structure roller 410 for set rubber.
Embodiment 3
1st, shipping loading frame is included：Baggage conveyor 301, belt support 302, loading frame end carriage 303, conveyer belt low side
Bearing 304, shipping sliding rail 305, hoistable platform 306, crane 307, hoistable platform base 308, hoistable platform roller
309th, the high-end bearing slide block 313, conveyer belt of sliding platform 310, sliding platform roller 311, loading frame roller 312, conveyer belt
Brace 314, belt support 302；
It is characterized in that：
Baggage conveyor 301 is flat conveyer belt, and higher end is low；(it is easy to for goods to be sent to height by lower
Place) baggage conveyor 301 low side and high-end is connected to two groups of belt supports 302, two groups of conveyer belts of low side below
302 times connection conveyer belt low side bearings 304 of frame；The high-end high-end bearing slide block of two groups of belt supports, 302 times connection conveyer belts
313；(the high-end bearing slide block of conveyer belt 313 is raised and lowered can the high-end of conveyer belt along 305 movement of shipping sliding rail, just
In conveyer belt is aligned the aircraft hold door that type is different and height is different, spare parts of goods can be incited somebody to action with baggage conveyor 301
Goods is transported to aircraft hold)
The connection of conveyer belt low side bearing 304 shipping sliding rail 305, the high-end bearing slide block of conveyer belt 313 are sleeved on shipping
On sliding rail 305；
306 bottom of hoistable platform connects crane 307, the crane of 307 staggered form of crane；
307 times connection hoistable platform bases 308 of crane；The connection hoistable platform of hoistable platform base 308 roller 309；Rise
Drop platform roller 309 is seated on shipping sliding rail 305；
The two ends of shipping sliding rail 305 are all connected with loading frame end carriage 303；
303 times connection loading frame rollers 312 of loading frame end carriage；Loading frame roller 312 is seated on arm support track 201；
The connection conveyer belt of belt support 302 support arm 314.
2nd, the shipping loading frame, it is characterised in that：Baggage conveyor 301 is that multilamellar belt carcass rubber presses conveyer belt.
3rd, the shipping loading frame, it is characterised in that：The shipping slip rail of 306 bottom of sliding platform 310 and hoistable platform
Road 305 is two parallel tracks.
4th, the shipping loading frame, it is characterised in that：The shipping slip rail of 306 bottom of sliding platform 310 and hoistable platform
Road 305 is three parallel tracks.
5th, 310 bottom of sliding platform connection sliding platform roller 311, sliding platform roller 311 is seated in shipping slip rail
On road 305；(effect of sliding platform is by being moved under aircraft hold door at a distance by the goods of large cargo such as container class
Side, then cargo hold doorway is lifted to by hoistable platform 306)
Embodiment 4
1st, rear thruster is included：Roller 501, roller axle 502, roller support 503, roller spring 504, bearing 505, connecting rod
506th, towing bracket 508, linear motor rotor 509, linear motor stator electric 510；
It is characterized in that：Thruster front end is connected with roller 501 afterwards, and there are roller axle 502, roller axle in the post center of roller 501
502 connection roller supports 503；
Roller support 503 and roller spring 504 have multigroup, the connection roller of roller support 503 spring 504, multigroup roller
504 connects bearing 505 of support 503 and roller spring；
Bearing of the bearing 505 for strip；Bearing 505 or so respectively has one, and the centrage of two bearings is straight in same
On line, in the middle of two bearings 505, connect connecting rod 506；
Bearing 505 is seated on rear thruster track 102.
2nd, described rear thruster, it is characterised in that：Bearing 505 connects towing bracket 508, the connection straight line of towing bracket 508
Rotor 509；Towing bracket 508 connects linear motor stator electric 510.
3rd, described rear thruster, it is characterised in that：There is spring spool outside roller spring 504.
4th, described rear thruster, it is characterised in that：501 overcoat rubber sleeve of roller.
5th, described rear thruster, it is characterised in that：Roller 501 is rubber-plastics material roller.
In addition to technical characteristic described herein, remaining is knowledge known to one of ordinary skill in the art, and here does not exist
Repeat.
Claims (8)
1. front frame posture airborne vehicle carrying platform, including：Fuselage profile, main landing gear position, nose-gear position, platform master
Body, arm support, shipping loading frame, boarding crane span structure, rear thruster, airport track；
Main platform body is included：Main carrying platform, rear thruster track, ear platform, equipment box, transition ramp, radial direction chassis, main chassis,
Radial direction chassis movable axis, front chassis, nose-gear catch, nose-gear platform；
Arm support is included：Arm support track, arm support crossbeam, arm support chassis, pool machine display screen, display screen pillar；
Shipping loading frame is included：Baggage conveyor, belt support, loading frame end carriage, shipping sliding rail, hoistable platform, liter
Drop frame, hoistable platform base, hoistable platform roller, sliding platform, sliding platform roller；
Boarding crane span structure is included：Connecting bridge, flexible airstair, bridge-frame end-beam, crane span structure sliding rail, boarding gate, flexible vestibule diaphragm, shelter bridge
Supporting plate, crane, crane span structure roller；
Airport track has four parallel tracks；
There are diesel engine, electromotor, bleed machine in equipment box；
It is characterized in that：
At the rear portion of main platform body, main platform body is "convex" shaped structure to main carrying platform, and postmedian is rectangle, and middle part both sides connect
It is connected to symmetrical ear platform, the prominent part before main platform body of nose-gear platform；
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 is connected with radial direction chassis；
Four wheels, the four wheels connection radial direction chassis movable axis of radial direction chassis are housed below radial direction chassis；
Main chassis is connected with below the middle part of main carrying platform；The front portion of nose-gear platform is connected with front chassis below；
Arm support track has two groups, and per group is parallel rectilinear orbit；
Four wheels are housed below main chassis；
Every group of arm support track end difference engaging lug 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 direction chassis and main chassis are seated on four tracks on the track of airport；Front chassis are seated in airport rail
On two inner orbits in road；
Arm support track front end connects arm support crossbeam, and arm support crossbeam is between two arms mounted track, vertical with arm support track；
Linking arm rack trolley under arm support crossbeam；The wheel of arm support chassis is respectively seated in two inner tracks of airport track；
Shipping loading frame is housed on the arm support track of left side；
Boarding crane span structure is housed on right arm mounted track.
2. front frame posture airborne vehicle carrying platform as claimed in claim 1, it is characterised in that：Described radial direction chassis is left and right
Symmetrical 2 couple.
3. front frame posture airborne vehicle carrying platform as claimed in claim 1, it is characterised in that：The radial direction chassis connection is radially
Chassis movable axis.
4. front frame posture airborne vehicle carrying platform as claimed in claim 1, it is characterised in that：Fill on described main carrying platform
There are rear thruster track, thruster track after rear thruster connection.
5. front frame posture airborne vehicle carrying platform as claimed in claim 1, it is characterised in that：On described nose-gear platform
Connection nose-gear catch, the section of nose-gear catch is trapezoidal catch.
6. front frame posture airborne vehicle carrying platform as claimed in claim 1, it is characterised in that：Connect in the middle part of arm support crossbeam
There are display screen pillar, pool machine display screen connection display screen pillar.
7. front frame posture airborne vehicle carrying platform as claimed in claim 1, it is characterised in that：Nose-gear catch is rubber wheel
Gear.
8. front frame posture airborne vehicle carrying platform as claimed in claim 1, it is characterised in that：Generator cable in equipment box
Connection airborne vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610796243.XA CN106608365A (en) | 2016-08-31 | 2016-08-31 | Front frame aircraft carrying platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610796243.XA CN106608365A (en) | 2016-08-31 | 2016-08-31 | Front frame aircraft carrying platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106608365A true CN106608365A (en) | 2017-05-03 |
Family
ID=58614938
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610796243.XA Withdrawn CN106608365A (en) | 2016-08-31 | 2016-08-31 | Front frame aircraft carrying platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106608365A (en) |
-
2016
- 2016-08-31 CN CN201610796243.XA patent/CN106608365A/en not_active Withdrawn
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| PB01 | Publication | ||
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Application publication date: 20170503 |