CN203681882U - Remote control aeroplane trailer - Google Patents
Remote control aeroplane trailer Download PDFInfo
- Publication number
- CN203681882U CN203681882U CN201320846413.2U CN201320846413U CN203681882U CN 203681882 U CN203681882 U CN 203681882U CN 201320846413 U CN201320846413 U CN 201320846413U CN 203681882 U CN203681882 U CN 203681882U
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- CN
- China
- Prior art keywords
- wheel
- shovel board
- oil cylinder
- frame
- trailer
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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- 239000000203 mixture Substances 0.000 claims description 10
- 238000000034 method Methods 0.000 abstract description 3
- 239000003921 oil Substances 0.000 description 18
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000000151 deposition Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000295 fuel oil Substances 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
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Abstract
The utility model relates to a remote control aeroplane trailer. The remote control aeroplane trailer comprises a housing, a machine frame, driving wheels, universal wheels, a signal receiver, a battery box, a plane wheel trailing mechanism and an oil cylinder. The housing is arranged outside the machine frame, the driving wheels and the universal wheels are arranged at both ends of the machine frame, the battery box, the signal receiver, the plane wheel trailing mechanism and the oil cylinder are arranged on the machine frame, and the plane wheel trailing mechanism is connected with the oil cylinder. According to the remote control aeroplane trailer, the plane wheel trailing mechanism, the driving wheels and the universal wheels are controlled to work through an external remote control device, so that ground trailing processes of general aeroplanes can be achieved more safely, more rapidly and more economically.
Description
Technical field
The utility model relates to a kind of telecontrolled aircraft trailer.
Background technology
At present, general aviation aircraft ground tows is mainly had bar or is completed without bar trailer by the ground identical with transport airliners.Have bar trailer to be connected to aircraft nose-gear assigned address by a drawbar one end, the other end is connected on trailer post bolt and evades activity.Need to fastening structure, aircraft nose wheel be fixed and be given rise to certain altitude without bar trailer and evade activity.When these two kinds of modes tow for aircraft floor, in function, there is certain deficiency.First, operating personal must carry out operation on operator's compartment or service platform, has so just limited in operating personal operation process particularly effective observation of obstacle of surrounding environment.Secondly,, because above-mentioned tractor truck must be provided for platform or the operator's compartment of operator's operation, make the physical size of vehicle larger.Be unfavorable for carrying out operation and depositing at small space.The trailer that fuel oil drives also brings certain fire safety hidden danger in the time approaching aircraft operation, and when the work of internal field, noise is larger.Vehicle and aircraft connection work complexity.There is bar trailer owing to being hingedly connected with aircraft by turning to for 2 times, in the direction control of carrying out operation, just have very large difficulty and potential safety hazard.Large-scalely need to embrace act to aircraft nose wheel without bar trailer, because size of wheel before large-scale transport airliners and Small Universal space shuttle differs larger, can not accomplish compatibility.The observation to surrounding environment in the work that aircraft is carried out or towed of sealing driving compartment has obstacle, and existing actual job need separately send observer to participate in guiding.
Summary of the invention
The utility model, just for the problems referred to above, provides a kind of telecontrolled aircraft trailer.To achieve these goals, the utility model adopts following technical scheme, comprise shell, frame, driving wheel, cardan wheel, signal receiver, battery case, wheel tractor and oil cylinder, shell is positioned at the outside of frame, driving wheel and cardan wheel lay respectively at the two ends of frame, battery case, signal receiver, wheel tractor and oil cylinder are all arranged in frame, and wheel tractor is connected with oil cylinder; Described wheel tractor comprises shovel board, shovel board axle, wheel blend stop, ratchet pin, and shovel board is arranged on shovel board axle, can rotate around shovel board axle, and wheel blend stop is between shovel board, and ratchet pin is positioned at the top of shovel board.Described driving wheel and the top of cardan wheel are provided with respectively driving wheel support and caster bracket.Between described shovel board, be also provided with front-wheel backing plate.Described wheel blend stop is detouchable, is plugged in the insert row in shovel board.Described wheel tractor is positioned at outside shell.In described frame, be also provided with oil pump station,, it is connected with oil cylinder.Ratchet pin is realized rotation by the ratchet of below.
the beneficial effects of the utility model:
The novel work of controlling wheel tractor, driving wheel and cardan wheel by external remote control device of the utility model, realization that can be safer, quicker, more economical is evaded operation to the ground of general aviation aircraft.
accompanying drawing explanation:
Fig. 1 is external structure schematic diagram of the present utility model.In Fig. 1,1 is shell, and 2 is wheel tractor.Fig. 2 is inner structure schematic diagram of the present utility model.In Fig. 2,3 is oil cylinder, and 4 is battery case, and 5 is front-wheel backing plate, and 6 is ratchet pin, 7 is wheel blend stop, and 8 is shovel board axle, and 9 is shovel board, and 10 is driving wheel, and 11 is driving wheel support, 12 is frame, and 13 is cardan wheel, and 14 is caster bracket, and 15 is signal receiver, and 16 is oil pump station.
the specific embodiment:
As seen from Figure 1, Figure 2, the utility model comprises shell, frame, driving wheel, cardan wheel, signal receiver, battery case, wheel tractor and oil cylinder, shell is positioned at the outside of frame, driving wheel and cardan wheel lay respectively at the two ends of frame, battery case, signal receiver, wheel tractor and oil cylinder are all arranged in frame, and wheel tractor is connected with oil cylinder; Described wheel tractor comprises shovel board, shovel board axle, wheel blend stop, ratchet pin, and shovel board is arranged on shovel board axle, can rotate around shovel board axle, and wheel blend stop is between shovel board, and ratchet pin is positioned at the top of shovel board.Described driving wheel and the top of cardan wheel are provided with respectively driving wheel support and caster bracket.Between described shovel board, be also provided with front-wheel backing plate.Described wheel blend stop is detouchable, is plugged in the insert row in shovel board.Described wheel tractor is positioned at outside shell.In described frame, be also provided with oil pump station,, it is connected with oil cylinder.Ratchet pin is realized rotation by the ratchet of below.Accompanying drawings one-off process of the present utility model, remote controller transmits control signal to control the work of whole device to signal receiver, in the time embracing the wheel of act aircraft, oil cylinder first stretches out, shovel board is down to extreme lower position, control car load and move until front-wheel backing plate touches wheel to wheel, then manually insert wheel shelves bar.After wheel shelves bar inserts, control oil cylinder and shrink, shovel board upward movement, until wheel is liftoff and reach appropriate clearance, manually makes its contact wheel by bottom ratchet wheel pin, completes the ground that can carry out aircraft after aforesaid operations and moves operation.Behind desired location, oppositely complete above-mentioned behaviour.Battery in battery case provides Electronmotive Force for oil pump station, and oil pump station is converted into hydraulic coupling and is transferred to oil cylinder, makes oil cylinder work.
Claims (6)
1.
a kind of telecontrolled aircraft trailer, it is characterized in that, comprise shell, frame, driving wheel, cardan wheel, signal receiver, battery case, wheel tractor and oil cylinder, shell is positioned at the outside of frame, driving wheel and cardan wheel lay respectively at the two ends of frame, battery case, signal receiver, wheel tractor and oil cylinder are all arranged in frame, and wheel tractor is connected with oil cylinder;
described wheel tractor comprises shovel board, shovel board axle, wheel blend stop, ratchet pin, and shovel board is arranged on shovel board axle, can rotate around shovel board axle, and wheel blend stop is between shovel board, and ratchet pin is positioned at the top of shovel board.
2.
telecontrolled aircraft trailer according to claim 1, is characterized in that, described driving wheel and the top of cardan wheel are provided with respectively driving wheel support and caster bracket.
3.
telecontrolled aircraft trailer according to claim 1, is characterized in that, is also provided with front-wheel backing plate between described shovel board.
4.
telecontrolled aircraft trailer according to claim 1, is characterized in that, described wheel blend stop is detouchable, is plugged in the insert row in shovel board.
5.
telecontrolled aircraft trailer according to claim 1, is characterized in that, described wheel tractor is positioned at outside shell.
6.
telecontrolled aircraft trailer according to claim 1, is characterized in that, is also provided with oil pump station in described frame, and it is connected with oil cylinder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320846413.2U CN203681882U (en) | 2013-12-20 | 2013-12-20 | Remote control aeroplane trailer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320846413.2U CN203681882U (en) | 2013-12-20 | 2013-12-20 | Remote control aeroplane trailer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203681882U true CN203681882U (en) | 2014-07-02 |
Family
ID=51003824
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320846413.2U Expired - Lifetime CN203681882U (en) | 2013-12-20 | 2013-12-20 | Remote control aeroplane trailer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203681882U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112061416A (en) * | 2020-09-21 | 2020-12-11 | 航大联合航空设备有限公司 | Aviation is system of marcing with pulling |
-
2013
- 2013-12-20 CN CN201320846413.2U patent/CN203681882U/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112061416A (en) * | 2020-09-21 | 2020-12-11 | 航大联合航空设备有限公司 | Aviation is system of marcing with pulling |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: LIU CHANGMING Effective date: 20150722 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20150722 Address after: 650000 9-4-301, 47 North Gate Street, Wuhua District, Yunnan, Kunming Patentee after: Li Lei Patentee after: Liu Changming Address before: 650000 9-4-301, 47 North Gate Street, Wuhua District, Yunnan, Kunming Patentee before: Li Lei |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20180706 Address after: 650000 102-13, first building, A building, biological incubator building, 1389 Changyuan North Road, Kunming new high tech Zone, Yunnan Patentee after: YUNNAN XIANG'AO AVIATION TECHNOLOGY CO.,LTD. Address before: 650000 9-4-301, 47 North Gate Street, Wuhua District, Kunming, Yunnan. Co-patentee before: Liu Changming Patentee before: Li Lei |
|
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20140702 |