CN106314819A - Buffering type automatic lifting conveying platform device for helicopter - Google Patents
Buffering type automatic lifting conveying platform device for helicopter Download PDFInfo
- Publication number
- CN106314819A CN106314819A CN201610831773.3A CN201610831773A CN106314819A CN 106314819 A CN106314819 A CN 106314819A CN 201610831773 A CN201610831773 A CN 201610831773A CN 106314819 A CN106314819 A CN 106314819A
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- Prior art keywords
- shipping platform
- oil cylinder
- platform
- axle
- helicopter
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- 230000003139 buffering effect Effects 0.000 title claims abstract description 11
- 238000005096 rolling process Methods 0.000 claims abstract description 20
- 230000033001 locomotion Effects 0.000 claims description 12
- 230000005540 biological transmission Effects 0.000 claims description 8
- 230000001360 synchronised effect Effects 0.000 claims description 5
- 238000013016 damping Methods 0.000 claims description 4
- 230000000694 effects Effects 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 4
- 239000000835 fiber Substances 0.000 claims description 3
- 239000000463 material Substances 0.000 claims description 3
- 229910000831 Steel Inorganic materials 0.000 claims description 2
- 238000009434 installation Methods 0.000 claims description 2
- 239000010959 steel Substances 0.000 claims description 2
- 241000209140 Triticum Species 0.000 claims 1
- 235000021307 Triticum Nutrition 0.000 claims 1
- 229920001596 poly (chlorostyrenes) Polymers 0.000 claims 1
- 125000000391 vinyl group Chemical group [H]C([*])=C([H])[H] 0.000 claims 1
- 229920002554 vinyl polymer Polymers 0.000 claims 1
- 238000010276 construction Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
Classifications
-
- 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 for handling aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
- Bearings For Parts Moving Linearly (AREA)
Abstract
The invention discloses a buffering type automatic lifting conveying platform device for a helicopter. The buffering type automatic lifting conveying platform device for the helicopter comprises a conveying platform, a distance adjusting device, a lifting device, walking devices, a buffering device and a control system. The walking devices are symmetrically installed at the bottom of the conveying platform. The two ends of the distance adjusting device are connected with conveying platform bodies respectively and used for adjusting the distance between the conveying platform bodies. The lifting device is connected with the conveying platform and used for adjusting rolling and lifting of rollers on the conveying platform. The buffering device is fixed to the conveying platform. The control system is arranged in the conveying platform, and a control button of the control system is installed on the conveying platform. The buffering type automatic lifting conveying platform device for the helicopter is simple in structure, complete in control function, reliable in walking and turning and convenient to operate, the skid-mounted helicopter can be automatically lifted to the conveying platform, and automatic lifting and automatic loading and unloading of the skid-mounted helicopter can be achieved.
Description
Technical field
The slide-type helicopter that the present invention relates to a kind of band skid plate drops to ground, is moved automatically into the dress of hangar
Put, be specifically related to a kind of buffer-type helicopter and automatically lift shipping platform device.
Background technology
Along with the development of science and technology, the use of slide-type helicopter is more and more extensive, and the slide-type for band skid plate is gone straight up to
Move storehouse problem after machine landing and be always focus of concern.At present, prior art is to allow slide-type helicopter drop to specify
Place on, place personnel subsequently tail arrange cable wire, utilize winch adjust fuselage enter hangar direction, then with traction
Car is drawn to hangar.This technology takes time and effort, and in order to more easily slide-type helicopter be moved into hangar, saves not
Necessary human resources, therefore develops a kind of simple in construction, automatically lifts on shipping platform by slide-type helicopter, control merit
Can be perfect, walking turns to reliable, easy to operate, it is achieved slide-type helicopter automatically lift and the buffer-type of automatic loading and unloading is gone straight up to
It is particularly important that shipping platform device lifted automatically by machine.
Summary of the invention
It is an object of the invention to provide a kind of simple in construction, automatically slide-type helicopter is lifted on shipping platform, control
Perfect in shape and function processed, walking turns to reliable, easy to operate, it is achieved automatically lifting and automatic loading and unloading of slide-type helicopter.
For reaching above-mentioned purpose, the technical solution adopted in the present invention is as follows:
A kind of buffer-type helicopter lifts shipping platform device automatically, including: shipping platform, adjustable distance device, lift
Device, running gear, buffer unit, control system；Described shipping platform is symmetrically mounted at the bottom of described running gear；Described adjustable
Spacing device includes that axle III and oil cylinder V, the oil cylinder V of described adjustable distance device are fixed on the side of described shipping platform opening
On, described lifting apparatus is connected with described shipping platform, and described lifting apparatus is positioned at the middle part of described shipping platform；Described control
System is placed in the inside of described shipping platform, and the control knob of described control system is arranged on described shipping platform；Described fortune
Defeated platform includes that shipping platform I and shipping platform II, the bottom of described shipping platform I and described shipping platform II are respectively symmetrically installed
Four overlap described running gear；Described shipping platform I and described shipping platform II is concave structure, and described shipping platform I is with described
The platform both sides of shipping platform II respectively have rectangle air cushion groove；Described buffer unit includes air cushion and source of the gas, and described air cushion is pacified
Being placed in described rectangle air cushion groove, described air cushion uses pvc material, and solid reliable intensity is high, within described air cushion
Levels distributed fibers silk, plays effective supporting role；Described source of the gas is respectively and fixedly installed to described shipping platform I with described
On the table top of shipping platform II, when helicopter skid plate is during being lifted, the two ends of skid plate fall and put down in described transport
Time on platform, start described source of the gas, described air cushion gassy, play the effect of support, buffering, vibration damping for whole fuselage.
Further, the described shipping platform I and the described shipping platform II oil cylinder V phase by described adjustable distance device
Even；Respectively have a symmetrical ear type groove inside the concave structure of described shipping platform I and described shipping platform II, be used for coordinating
The rolling that described lifting apparatus controls two rollers by four oil cylinders promotes, it is achieved the easy motion of described lifting apparatus；Institute
The side stating shipping platform II projection has circular port, it is simple to the installation of the axle III in described adjustable distance device；Described
Shipping platform I and described shipping platform II is high intensity I-steel weldment.
Further, the described axle III of described adjustable distance device is fixedly mounted on the circular port of described shipping platform II
In；The oil cylinder seat of described oil cylinder V is fixedly mounted on the side of described shipping platform I projection, the cylinder rod of described oil cylinder V
Top be enclosed within described axle III by oscillating bearing；After slide-type helicopter lands, described control system controls described oil cylinder
The cylinder rod of V is elongated to certain length, moves to slide-type helicopter by driving described running gear to move whole device
Under skid plate, the most described control system control again described oil cylinder V cylinder rod retract, thus regulate described shipping platform I with
Distance between described shipping platform II.
Further, described lifting apparatus includes oil cylinder I, oil cylinder II, oil cylinder III, oil cylinder IV, fixed support I, fixes and prop up
Frame II, fixed support III, fixed support IV, roller I, roller II, axle I, axle II；Described oil cylinder I is arranged on described fixed support
On I, described oil cylinder II is arranged on described fixed support II, and described fixed support I, described fixed support II are fixedly mounted on institute
Stating on shipping platform I, described oil cylinder III is arranged on described fixed support III, and described oil cylinder IV is arranged on described fixed support
On IV, described fixed support III, described fixed support IV are fixedly mounted on described shipping platform II；Described oil cylinder I, oil cylinder
The top of the cylinder rod of II is respectively fitted over the two ends of described axle I, described oil cylinder III, the cylinder rod of oil cylinder IV by oscillating bearing
Top be respectively fitted over the two ends of described axle II by oscillating bearing, described roller I is connected with described axle I, described roller II with
Described axle II connects, and the two ends of described axle I are stuck in the ear type groove of described shipping platform I, and the two ends of described axle II are stuck in described
In the ear type groove of shipping platform II, it is simple to described oil cylinder I, the flexible drive described axle I of cylinder rod of oil cylinder II, described axle II edge
The movement locus motion of ear type groove, it is achieved the rolling of described roller I and described roller II promotes and lifts；As described roller I and
When described roller II is positioned under the skid plate of slide-type helicopter, described control system control described oil cylinder I, described oil cylinder II,
Described oil cylinder III, the cylinder rod of described oil cylinder IV synchronize elongation, and described oil cylinder I, the thrust of described oil cylinder II are converted into described axle
The rolling of I, described oil cylinder III, the thrust of described oil cylinder IV is converted into the rolling of described axle II, thus along described shipping platform I
Move with the ear type groove course bearing of described shipping platform II, by described roller I and the synchronous rolling of described roller II
Promote thus realize lifting of slide-type helicopter.
Further, described running gear includes that Mecanum wheel and power transmission shaft, described power transmission shaft have four sets, described Mike
Na Mu wheel has eight sets, described power transmission shaft to be separately fixed at described shipping platform I and the bottom of described shipping platform II, described Mike
Na Mu wheel is connected with described power transmission shaft, and described Mecanum wheel is by its motion of Direct wheel drives system drive.
Further, described control knob includes forwarding button, back, stop button, turns to button, described advance
Described in button control, Mecanum wheel travels forward, described back control described Mecanum wheel retreat, described in stop
The only stopping of Mecanum wheel described in button control, described in turn in Mecanum wheel motion described in button control and adjust motion side
To.
Implementing one buffer-type helicopter of the present invention and automatically lift shipping platform device, it has the beneficial effects that:
(1) using one buffer-type helicopter of the present invention automatically to lift shipping platform device, simple in construction, automatically by skid
Formula helicopter is lifted on shipping platform, controls perfect in shape and function, and walking turns to reliable, easy to operate；
Lifting apparatus the most of the present invention uses reliable frame for movement to realize automatically lifting and oneself of slide-type helicopter
Dynamic handling.
Accompanying drawing explanation
Fig. 1: one buffer-type helicopter of the present invention lifts shipping platform device front view automatically；
Fig. 2: one buffer-type helicopter of the present invention lifts shipping platform device top view automatically；
Fig. 3: one buffer-type helicopter of the present invention lifts shipping platform device 3 dimensional drawing automatically.
In figure: 1 shipping platform, 11 shipping platform I, 12 shipping platform II, 2 adjustable distance devices, 21 axles
III, 22 oil cylinder V, 3 lifting apparatus, 31 oil cylinder I, 32 oil cylinder II, 33 oil cylinder III, 34 oil cylinder IV, 35 is solid
Fixed rack I, 36 fixed support II, 37 fixed support III, 38 fixed support IV, 391 roller I, 392 roller II,
393 axle I, 394 axle II, 4 running gear 41 Mecanum wheel, 5 control knobs, 51 forwarding buttons, after 52
Moving back button, 53 stop buttons, 54 turn to button, 6 air cushions.
Detailed description of the invention
Below in conjunction with the accompanying drawings the present invention is further described through.
As shown in Figure 1, 2, 3, a kind of buffer-type helicopter lifts shipping platform device automatically, including: shipping platform 1, can
Adjust spacing device 2, lifting apparatus 3, running gear 4, buffer unit, control system；Described shipping platform 1 is symmetrically mounted at the bottom of institute
State running gear 4；Described adjustable distance device 2 includes axle III21 and oil cylinder V22, the oil cylinder V22 of described adjustable distance device 2
Being fixed on the side of described shipping platform 1 opening, described lifting apparatus 3 is connected with described shipping platform 1, described lifting apparatus
3 middle parts being positioned at described shipping platform 1；Described control system is placed in the inside of described shipping platform 1, the control of described control system
Button 5 processed is arranged on described shipping platform 1；Described shipping platform 1 includes shipping platform I11 and shipping platform II12, described
The bottom of shipping platform I11 and described shipping platform II12 is respectively symmetrically installed the four described running gears of set 4；Described shipping platform
I11 and described shipping platform II12 is concave structure, and described shipping platform I11 is each with the platform both sides of described shipping platform II12
Have rectangle air cushion groove；Described buffer unit includes that air cushion 6 and source of the gas, described air cushion 6 are placed in described rectangle air cushion groove
In, described air cushion 6 uses pvc material, and solid reliable intensity is high, the levels distributed fibers silk within described air cushion 6,
Play effective supporting role；Described source of the gas is respectively and fixedly installed to described shipping platform I11 and described shipping platform II12's
On table top, when helicopter skid plate is during being lifted, when the two ends of skid plate fall on described shipping platform 1, start
Described source of the gas, described air cushion 6 gassy, plays the effect of support, buffering, vibration damping for whole fuselage；Described adjustable distance fills
The described axle III21 put is fixedly mounted in the circular port of described shipping platform II12；The fixing peace of the oil cylinder seat of described oil cylinder V22
Being contained on the side of described shipping platform I11 projection, the top of the cylinder rod of described oil cylinder V22 is enclosed within by oscillating bearing
On described axle III21；After slide-type helicopter lands, described control system controls the cylinder rod of described oil cylinder V22 and is elongated to one
Measured length, by driving described running gear 4 to move under the skid plate that whole device moves to slide-type helicopter, then described
Control system controls the cylinder rod of described oil cylinder V22 again and retracts, thus regulates described shipping platform I11 and described shipping platform
Distance between II12；Described lifting apparatus 3 includes oil cylinder I31, oil cylinder II32, oil cylinder III33, oil cylinder IV34, fixed support
I35, fixed support II36, fixed support III37, fixed support IV38, roller I391, roller II392, axle I393, axle
II394；Described oil cylinder I31 is arranged on described fixed support I35, and described oil cylinder II32 is arranged on described fixed support II36
On, described fixed support I35, described fixed support II36 are fixedly mounted on described shipping platform I11, described oil cylinder III33
Being arranged on described fixed support III37, described oil cylinder IV34 is arranged on described fixed support IV38, described fixed support
III37, described fixed support IV38 are fixedly mounted on described shipping platform II12；Described oil cylinder I31, the oil cylinder of oil cylinder II32
The top of bar is respectively fitted over the two ends of described axle I393 by oscillating bearing, described oil cylinder III33, the cylinder rod of oil cylinder IV34
Top is respectively fitted over the two ends of described axle II394 by oscillating bearing, and described roller I391 is connected with described axle I393, described rolling
Sub-II392 is connected with described axle II394, and the two ends of described axle I393 are stuck in the ear type groove of described shipping platform I11, described axle
The two ends of II394 are stuck in the ear type groove of described shipping platform II12, it is simple to described oil cylinder I31, the cylinder rod of oil cylinder II32
Flexible described axle I393, described axle II394 is driven to move along the movement locus of ear type groove, it is achieved described roller I391 and described
The rolling of roller II392 promotes and lifts；When described roller I391 and described roller II392 is positioned at the skid plate of slide-type helicopter
Time lower, described control system controls described oil cylinder I31, described oil cylinder II32, described oil cylinder III33, the oil of described oil cylinder IV34
Cylinder rod synchronizes elongation, and described oil cylinder I31, the thrust of described oil cylinder II32 are converted into the rolling of described axle I393, described oil cylinder
III33, the thrust of described oil cylinder IV34 are converted into the rolling of described axle II394, thus along described shipping platform I11 and described fortune
The ear type groove course bearing of defeated platform II12 moves, by described roller I391 and the synchronous rolling of described roller II392
Promote thus realize lifting of slide-type helicopter.
As shown in Figure 1, 2, 3, a kind of buffer-type helicopter lifts the method for work concrete steps of shipping platform device automatically
As follows: aircraft landing to ground, the cylinder rod of the oil cylinder V22 that control system controls adjustable distance device 2 is elongated to certain length,
Pressing forwarding button 51, mobile a kind of buffer-type helicopter lifts shipping platform device automatically to slide-type helicopter position, drives
Mecanum wheel 41 mobile platform in dynamic running gear 4 is under the skid plate of slide-type helicopter, and then control system is controlled again
The cylinder rod of liquefaction cylinder V22 is retracted, thus the distance regulated between described shipping platform I11 and described shipping platform II12 is
Zero, under now roller I391 and roller II392 is placed exactly in the skid plate of slide-type helicopter；Control system control oil cylinder I31,
Oil cylinder II32, oil cylinder III33, the cylinder rod of oil cylinder IV34 synchronize elongation, and oil cylinder I31, the thrust of oil cylinder II32 are converted into axle
The rolling of I393, oil cylinder III33, the thrust of oil cylinder IV34 is converted into the rolling of described axle II394, thus along shipping platform I11
Move with the ear type groove course bearing of shipping platform II12, promoted by the synchronous rolling of roller I391 and roller II392
Thus realize lifting of slide-type helicopter, slide-type helicopter is departed from ground, when the two ends of skid plate fall in described transport
Time on platform 1, start described source of the gas, described air cushion 6 gassy, play the effect of support, buffering, vibration damping for whole fuselage；
Then move whole device by the Mecanum wheel 41 in running gear 4, make slide-type helicopter move into hangar；By can
Adjusting spacing device 2 spacing between shipping platform I11 and shipping platform II12 will to be made to tune up, lifting apparatus 3 is by roller I391
With the synchronous rolling of roller II392 by the landing of slide-type helicopter, slide-type helicopter falls to the ground the most at last.
The foregoing is only presently preferred embodiments of the present invention, not in order to limit the present invention, all essences in the present invention
Any amendment, equivalent and the improvement etc. made within god and principle, should be included within the scope of the present invention.
Claims (6)
1. a buffer-type helicopter lifts shipping platform device automatically, it is characterised in that including: shipping platform (1), adjustable
Away from device (2), lifting apparatus (3), running gear (4), buffer unit, control system；Described shipping platform (1) bottom symmetrical is pacified
Fill described running gear (4)；Described adjustable distance device (2) includes axle III (21) and oil cylinder V (22), and described adjustable distance fills
The oil cylinder V (22) putting (2) is fixed on the side of described shipping platform (1) opening, and described lifting apparatus (3) is put down with described transport
Platform (1) is connected, and described lifting apparatus (3) is positioned at the middle part of described shipping platform (1)；Described control system is placed in described transport and puts down
The inside of platform (1), the control knob (5) of described control system is arranged on described shipping platform (1)；Described shipping platform (1)
Including shipping platform I (11) and shipping platform II (12), described shipping platform I (11) and the bottom of described shipping platform II (12)
Respectively it is symmetrically installed the described running gear of four set (4)；Described shipping platform I (11) and described shipping platform II (12) are spill knot
Structure, described shipping platform I (11) respectively has rectangle air cushion groove with the platform both sides of described shipping platform II (12)；Described buffering
Device includes that air cushion (6) and source of the gas, described air cushion (6) are placed in described rectangle air cushion groove, and described air cushion (6) uses polychlorostyrene
Vinyl material, solid reliable intensity is high, the levels distributed fibers silk that described air cushion (6) is internal, plays effective supporting role；
Described source of the gas is respectively and fixedly installed on the table top of described shipping platform I (11) and described shipping platform II (12), works as helicopter
Skid plate is during being lifted, and the two ends of skid plate fall when described shipping platform (1) is upper, start described source of the gas, described
Air cushion (6) gassy, plays the effect of support, buffering, vibration damping for whole fuselage.
2. a kind of buffer-type helicopter as claimed in claim 1 lifts shipping platform device automatically, it is characterised in that described fortune
Defeated platform I (11) is connected by the oil cylinder V (22) of described adjustable distance device (2) with described shipping platform II (12)；Described fortune
Respectively have a symmetrical ear type groove inside the concave structure of defeated platform I (11) and described shipping platform II (12), be used for coordinating
The rolling that described lifting apparatus (3) controls two rollers by four oil cylinders promotes, it is achieved the steady fortune of described lifting apparatus (3)
Dynamic；The side of described shipping platform II (12) projection has circular port, it is simple to the axle in described adjustable distance device (2)
The installation of III (21)；Described shipping platform I (11) and described shipping platform II (12) are high intensity I-steel weldment.
3. a kind of buffer-type helicopter as claimed in claim 1 lifts shipping platform device automatically, and its described adjustable distance fills
Put, it is characterised in that described axle III (21) is fixedly mounted in the circular port of described shipping platform II (12)；Described oil cylinder V
(22) oil cylinder seat is fixedly mounted on the side of described shipping platform I (11) projection, the cylinder rod of described oil cylinder V (22)
Top be enclosed within described axle III (21) by oscillating bearing；After slide-type helicopter lands, described control system controls described
The cylinder rod of oil cylinder V (22) is elongated to certain length, by driving the mobile whole device of described running gear (4) to move to skid
Under the skid plate of formula helicopter, the most described control system controls the cylinder rod of described oil cylinder V (22) again and retracts, thus regulates institute
State the distance between shipping platform I (11) and described shipping platform II (12).
4. a kind of buffer-type helicopter as claimed in claim 1 lifts shipping platform device automatically, it is characterised in that described torr
Lift device (3) to include oil cylinder I (31), oil cylinder II (32), oil cylinder III (33), oil cylinder IV (34), fixed support I (35), fix and prop up
Frame II (36), fixed support III (37), fixed support IV (38), roller I (391), roller II (392), axle I (393), axle II
(394)；Described oil cylinder I (31) is arranged on described fixed support I (35), and described oil cylinder II (32) is arranged on described fixed support
On II (36), described fixed support I (35), described fixed support II (36) are fixedly mounted on described shipping platform I (11), institute
Stating oil cylinder III (33) to be arranged on described fixed support III (37), described oil cylinder IV (34) is arranged on described fixed support IV
(38), on, described fixed support III (37), described fixed support IV (38) are fixedly mounted on described shipping platform II (12)；
Described oil cylinder I (31), the top of cylinder rod of oil cylinder II (32) are respectively fitted over the two ends of described axle I (393) by oscillating bearing,
Described oil cylinder III (33), the top of cylinder rod of oil cylinder IV (34) are respectively fitted over the two of described axle II (394) by oscillating bearing
End, described roller I (391) is connected with described axle I (393), and described roller II (392) is connected with described axle II (394), described axle
The two ends of I (393) are stuck in the ear type groove of described shipping platform I (11), and the two ends of described axle II (394) are stuck in described transport and put down
In the ear type groove of platform II (12), it is simple to described oil cylinder I (31), the flexible drive described axle I of cylinder rod of oil cylinder II (32)
(393), described axle II (394) is moved along the movement locus of ear type groove, it is achieved described roller I (391) and described roller II
(392) rolling promotes and lifts；When described roller I (391) and described roller II (392) are positioned at the skid plate of slide-type helicopter
Time lower, described control system controls described oil cylinder I (31), described oil cylinder II (32), described oil cylinder III (33), described oil cylinder IV
(34) cylinder rod synchronizes elongation, and described oil cylinder I (31), the thrust of described oil cylinder II (32) are converted into the rolling of described axle I (393)
Dynamic, described oil cylinder III (33), the thrust of described oil cylinder IV (34) are converted into the rolling of described axle II (394), thus along described fortune
The ear type groove course bearing of defeated platform I (11) and described shipping platform II (12) moves, by described roller I (391) and
The synchronous rolling of described roller II (392) promotes thus realizes lifting of slide-type helicopter.
5. a kind of buffer-type helicopter as claimed in claim 1 lifts shipping platform device automatically, it is characterised in that described row
Walking apparatus (4) includes Mecanum wheel (41) and power transmission shaft, and described power transmission shaft has four sets, described Mecanum wheel (41) to have eight
Set, described power transmission shaft is separately fixed at described shipping platform I (11) and the bottom of described shipping platform II (12), and described Mike receives
Nurse wheel (41) is connected with described power transmission shaft, and described Mecanum wheel (41) is by its motion of Direct wheel drives system drive.
6. a kind of buffer-type helicopter as claimed in claim 1 lifts shipping platform device automatically, it is characterised in that described control
Button processed (5) includes forwarding button (51), back (52), stop button (53), turns to button (54), described forwarding button
(51) controlling described Mecanum wheel (41) to travel forward, described back (52) controls described Mecanum wheel (41) and carries out
Retreat, described stop button (53) controls the stopping of described Mecanum wheel (41), described in turn to button (54) to control described wheat
Ke Namu wheel (41) motion adjusts the direction of motion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610831773.3A CN106314819B (en) | 2016-09-19 | 2016-09-19 | A kind of buffer-type helicopter lifts shipping platform device automatically |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610831773.3A CN106314819B (en) | 2016-09-19 | 2016-09-19 | A kind of buffer-type helicopter lifts shipping platform device automatically |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106314819A true CN106314819A (en) | 2017-01-11 |
| CN106314819B CN106314819B (en) | 2019-01-04 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610831773.3A Active CN106314819B (en) | 2016-09-19 | 2016-09-19 | A kind of buffer-type helicopter lifts shipping platform device automatically |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109665115A (en) * | 2018-12-29 | 2019-04-23 | 飞智控（天津）科技有限公司 | Helicopter transport system and transportation resources |
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| JP2011046364A (en) * | 2009-08-28 | 2011-03-10 | Yanmar Co Ltd | On-vehicle device for transportation of unmanned helicopter |
| CN103085982A (en) * | 2012-12-11 | 2013-05-08 | 沈阳北方交通重工有限公司 | Device for protecting nose landing gear of rodless aircraft tractor |
| CN103754288A (en) * | 2013-12-04 | 2014-04-30 | 海丰通航科技有限公司 | Movable heliport |
| JP2015193358A (en) * | 2014-03-26 | 2015-11-05 | 有限会社フジカ | tsunami countermeasure device |
| CN206141852U (en) * | 2016-09-19 | 2017-05-03 | 青岛科技大学 | Automatic transportation platform device of lifting of buffering formula helicopter |
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2016
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4123020A (en) * | 1976-02-23 | 1978-10-31 | Kazimierz Korsak | VTOL launching and retrieval systems |
| EP0564687B1 (en) * | 1992-04-10 | 1997-07-23 | Doll Fahrzeugbau Gmbh | Towing device |
| JP2011046364A (en) * | 2009-08-28 | 2011-03-10 | Yanmar Co Ltd | On-vehicle device for transportation of unmanned helicopter |
| CN103085982A (en) * | 2012-12-11 | 2013-05-08 | 沈阳北方交通重工有限公司 | Device for protecting nose landing gear of rodless aircraft tractor |
| CN103754288A (en) * | 2013-12-04 | 2014-04-30 | 海丰通航科技有限公司 | Movable heliport |
| JP2015193358A (en) * | 2014-03-26 | 2015-11-05 | 有限会社フジカ | tsunami countermeasure device |
| CN206141852U (en) * | 2016-09-19 | 2017-05-03 | 青岛科技大学 | Automatic transportation platform device of lifting of buffering formula helicopter |
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| CN109665115A (en) * | 2018-12-29 | 2019-04-23 | 飞智控（天津）科技有限公司 | Helicopter transport system and transportation resources |
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| Publication number | Publication date |
|---|---|
| CN106314819B (en) | 2019-01-04 |
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