CN202541843U - Telescopic airplane traction device - Google Patents
Telescopic airplane traction device Download PDFInfo
- Publication number
- CN202541843U CN202541843U CN201220003872XU CN201220003872U CN202541843U CN 202541843 U CN202541843 U CN 202541843U CN 201220003872X U CN201220003872X U CN 201220003872XU CN 201220003872 U CN201220003872 U CN 201220003872U CN 202541843 U CN202541843 U CN 202541843U
- Authority
- CN
- China
- Prior art keywords
- main body
- pipe
- telescopic
- body pipe
- wheel
- 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
Links
Images
Landscapes
- Clamps And Clips (AREA)
Abstract
The utility model provides a telescopic airplane traction device. The telescopic airplane traction device comprises a main body pipe, a front telescopic pipe and a rear telescopic pipe. The front telescopic pipe and the rear telescopic pipe are respectively disposed at the front end and the rear end of the main body pipe, and one ends of the front telescopic pipe and the rear telescopic pipe respectively extend into the main body pipe, are stretched out and drawn back relatively to the main body pipe, and are fixedly connected with the main body pipe through a hinged clamping plate. The front end of the front telescopic pipe is provided with a traction head with a steel wire rope supporting frame which is capable of rotating and being fixed. A steel wire rope directional pulley is installed on the main body pipe. Two ends of a steel wire rope which winds the steel wire rope directional pulley wind a guiding portion on the steel wire rope supporting frame and are connected with an airplane rear main machine wheel. The main body pipe is provided with a main wheel supporting frame with a main wheel. One end of a hydro-cylinder body which is controlled by a manual pump is connected with the main body pipe in a hinged mode. One end of a piston rod extends out the hydro-cylinder body and is connected with the upper end of the main wheel supporting frame in a hinged mode. The rear telescopic pipe is provided with a rear wheel supporting frame with a rear wheel. The telescopic airplane traction device is light in weight, small in size, convenient to store, place, carry, transship and transport, and capable of meeting requirements of users.
Description
Technical field:
The utility model relates to the draw gear that aircraft roll shifts, particularly be a kind of telescopic aircraft draw gear.
Background technology:
Old structure aircraft draw gear has enough intensity, rigidity, and durable in use, its oad is: 9600 mm * 1250 mm * 800 mm, own wt: 300 kg.The subject matter that it exists:
(1) integral structure, the oversize and difficult fractionation of length, volume is big, and heaviness needs 5～6 people and whipline during carrying, and transportation is inconvenient;
(2) loading and unloading are complicated, and transhipment takes up room big, and the waste of loading transportation time space is bigger.
The utility model content:
The purpose of the utility model is in order to overcome above deficiency, to provide a kind of in light weight, not long-pending little, being convenient to store and parking and carry transhipment, transportation, the telescopic aircraft draw gear of meeting consumers' demand.
The purpose of the utility model realizes like this:
The telescopic aircraft draw gear of the utility model; Comprise the main body pipe; Be arranged in main body pipe front and back ends and an end stretch into main body the pipe flexible and draw that protracts that can captive joint with the main body pipe through hinged clamping plate of main body pipe, back telescopic pipe relatively respectively; The draw front end that protracts is equipped with the drawing head of the steel rope support that contains rotation and can fix; The steel wire rope orientation pulley is contained on the main body pipe, is through the guide part that passes on the steel rope support at the steel rope two ends on the steel wire rope orientation pulley and is connected with aircraft aft engine wheel, and the main wheel support of main wheel is housed on the main body pipe; Be hinged on the main body pipe by cylinder block one end of manual pump control; It is hinged that piston rod stretches out an end and the main wheel support upper end of cylinder body, and the rear wheel support of band trailing wheel is being housed on the telescopic pipe of back, and forward and backward telescopic pipe can be realized length variations to the intermediate host pipe is flexible in 480mm～9600mm scope; Rotatable 90 ° of steel rope support; Can in 480mm～9600mm scope, realize wide variety, shake fuel priming pump, the main wheel support produces rotation under the effect of oil cylinder piston bar; Can in 560mm～1100mm scope, realize height change; Adopt hinge clamping plate (also cry and hold clip tightly) when the aircraft draw gear is worked, make the telescopic pipe at two ends and middle main body pipe become a rigid body, prevent that string is moving each other.
Above-mentioned steel rope support base plate is hinged on the indexing head center shaft and can be fixed on the drawing head center shaft through connecting element.
One end is arranged through hinge pivotally attached train wheel bridge, lower plate in the above-mentioned hinged clamping plate; Be hinged with movable bolt on the other end of lower plate; The position of relative movable bolt has movable bolt to cross groove on the other end of train wheel bridge; Movable bolt one end passes movable bolt and crosses groove and nut and cooperate the upper and lower clamping plate other end is connected, and when train wheel bridge unclamped, the two ends expansion link shrank along draw gear main body bar; This moment, draw gear was lacked ≯ 5 m most, can avoid the expansion link slight deformation and the situation that can't stretch.
Above-mentioned forward and backward telescopic pipe stretches on the other end in the main body pipe has safety screen, safety.
During the utility model work; Make forward and backward telescopic pipe and intermediate host pipe become a rigid body with the quick elongation of forward and backward telescopic pipe and with the hinge clamping plate; The rotatable wire rope support shakes manual pump to control position, makes the main wheel support rotate to desired height; Drawing head is installed on the undercarriage, and the steel rope two ends are fixed on the aircraft aft engine wheel just can.
The utility model is in light weight, and volume is little, and is fast flexible, easy to operate, and do not have loose pieces, and integral body is convenient to store and carry transhipment, practices thrift transhipment floor area ≮ 40%, safety.
Description of drawings:
Fig. 1 is the utility model structural representation.
Fig. 2 is the birds-eye view of Fig. 1.
Fig. 3 is a hinge clip plate structure scheme drawing.
Fig. 4 is telescopic pipe and main body pipe assembly drowing.
Fig. 5 is a drawing head knot portion working state figure.
Fig. 6 is traction head steel rope support slew mode figure.
The specific embodiment:
Referring to Fig. 1～Fig. 6; The telescopic aircraft draw gear of present embodiment; Comprise main body pipe 1, be arranged in main body pipe front and back ends and an end stretch into main body pipe the main body pipe draw 3 that protracts flexible and that captive joint with the main body pipe through hinged clamping plate 2, back telescopic pipe 4 relatively respectively.The draw front end that protracts is equipped with the drawing head 6 of the steel rope support 5 that contains rotation and can fix.Steel wire rope orientation pulley 7 is contained on the main body pipe.Being through the guide part 9 that passes on the steel rope support at steel rope 8 two ends on the steel wire rope orientation pulley is connected with aircraft aft engine wheel.The main wheel support 11 of main wheel 10 is housed on the main body pipe.Be hinged on the main body pipe by cylinder block 13 1 ends of manual pump 12 control, hinged on the end that piston rod 14 stretches out cylinder body and the main wheel support.The rear wheel support 16 of band trailing wheel 15 is housed on the telescopic pipe of back.Back telescopic pipe afterbody is equipped with eye hitch 27.
Referring to Fig. 5, Fig. 6, steel rope support base plate 17 is hinged on the indexing head center shaft 19 through hinge 18.Steel rope support base plate and drawing head center shaft opposite position have pin hole 20, and latch 28 1 ends pass the two corresponding pin hole steel rope support base plate is fixed on the drawing head center shaft.Take off latch steel rope support and just can rotate around hinge, as shown in Figure 6.
Referring to Fig. 3, an end is arranged in the hinged clamping plate through hinge pivotally attached train wheel bridge 21, lower plate 22.Be hinged with movable bolt 23 on the other end of lower plate.On the other end of train wheel bridge relatively the position of movable bolt have movable bolt to cross groove 24, movable bolt one end passes movable bolt and crosses groove and with nut 25 cooperations the upper and lower clamping plate other end is connected.
Referring to Fig. 4, forward and backward telescopic pipe stretches into has safety screen 26 on the other end on the main body pipe.
Claims (4)
1. telescopic aircraft draw gear; It is characterized in that comprising the main body pipe; Be arranged in main body pipe front and back ends and an end stretch into main body the pipe flexible and draw that protracts that can captive joint with the main body pipe through hinged clamping plate of main body pipe, back telescopic pipe relatively respectively; The draw front end that protracts is equipped with the drawing head of the steel rope support that contains rotation and can fix, and the steel wire rope orientation pulley is contained on the main body pipe, is through the guide part that passes on the steel rope support at the steel rope two ends on the steel wire rope orientation pulley and is connected with aircraft aft engine wheel; The main wheel support of main wheel is housed on the main body pipe; Be hinged on the main body pipe by cylinder block one end of manual pump control, it is hinged with main wheel support upper end that piston rod stretches out an end of cylinder body, on the telescopic pipe of back, the rear wheel support of being with trailing wheel is being housed.
2. telescopic aircraft draw gear as claimed in claim 1 is characterized in that base plate hinged in the steel rope support is on the drawing head center shaft and can be fixed on the drawing head center shaft through connecting element.
3. according to claim 1 or claim 2 telescopic aircraft draw gear; It is characterized in that having in the hinged clamping plate end through hinge pivotally attached train wheel bridge, lower plate; Be hinged with movable bolt on the other end of lower plate; On the other end of train wheel bridge relatively on the lower plate position of movable bolt have movable bolt to cross groove, movable bolt one end passes movable bolt and crosses groove and with the nut cooperation the upper and lower clamping plate other end is connected.
4. according to claim 1 or claim 2 telescopic aircraft draw gear is characterized in that forward and backward telescopic pipe stretches on the end in the main body pipe safety screen is arranged.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201220003872XU CN202541843U (en) | 2012-01-06 | 2012-01-06 | Telescopic airplane traction device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201220003872XU CN202541843U (en) | 2012-01-06 | 2012-01-06 | Telescopic airplane traction device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202541843U true CN202541843U (en) | 2012-11-21 |
Family
ID=47162514
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201220003872XU Expired - Lifetime CN202541843U (en) | 2012-01-06 | 2012-01-06 | Telescopic airplane traction device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202541843U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105059561A (en) * | 2015-07-17 | 2015-11-18 | 成都航利航空科技有限责任公司 | Three-section crawler telescoping airplane traction device |
| CN106275486A (en) * | 2015-05-21 | 2017-01-04 | 比亚迪股份有限公司 | Draw bar draw off gear and there is its tractor |
| CN107521715A (en) * | 2017-07-26 | 2017-12-29 | 彩虹无人机科技有限公司 | A kind of linkage for unmanned machine travel |
| CN113232883A (en) * | 2021-06-24 | 2021-08-10 | 中国舰船研究设计中心 | Omnidirectional transfer intelligent traction robot and traction method |
-
2012
- 2012-01-06 CN CN201220003872XU patent/CN202541843U/en not_active Expired - Lifetime
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275486A (en) * | 2015-05-21 | 2017-01-04 | 比亚迪股份有限公司 | Draw bar draw off gear and there is its tractor |
| CN106275486B (en) * | 2015-05-21 | 2019-02-26 | 比亚迪股份有限公司 | Draw bar draw off gear and tractor with it |
| CN105059561A (en) * | 2015-07-17 | 2015-11-18 | 成都航利航空科技有限责任公司 | Three-section crawler telescoping airplane traction device |
| CN105059561B (en) * | 2015-07-17 | 2016-09-28 | 成都航利航空科技有限责任公司 | A kind of three sections of crawler belt telescopic aircraft traction apparatuss |
| CN107521715A (en) * | 2017-07-26 | 2017-12-29 | 彩虹无人机科技有限公司 | A kind of linkage for unmanned machine travel |
| CN113232883A (en) * | 2021-06-24 | 2021-08-10 | 中国舰船研究设计中心 | Omnidirectional transfer intelligent traction robot and traction method |
| CN113232883B (en) * | 2021-06-24 | 2023-12-26 | 中国舰船研究设计中心 | Omnidirectional transportation intelligent traction robot and traction method |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN202541843U (en) | Telescopic airplane traction device | |
| CN103832410B (en) | Support foot device and walking machine | |
| CN210592481U (en) | Multi-degree-of-freedom aircraft missile hanging trailer | |
| CN204238851U (en) | One can slide Universal rotary rig | |
| CN204265034U (en) | Boats and ships modified form hydraulic foldable conveying arm structure | |
| CN202098991U (en) | Movable type folding crane | |
| CN102815628A (en) | Gantry hydraulic folding-arm crane | |
| CN202296907U (en) | Suspension arm balanced movable arm tower crane capable of luffing based on steel rope traction | |
| CN102303821A (en) | Luffing tower crane with balanced type suspension arm based on traction luffing of steel rope | |
| CN205346689U (en) | Four sections suspension arm device of single flexible hydro -cylinder and built -in wire rope linkage drive | |
| CN102734640A (en) | Outdoor engineering lighting device | |
| CN2863755Y (en) | Levelling device for overhead working truck platform draw-in rod | |
| CN201113297Y (en) | Multifunctional electric power construction vehicle | |
| CN201826761U (en) | Derrick | |
| CN105584405B (en) | One kind traction truck with loading crane | |
| CN208544417U (en) | A kind of unmanned plane main landing gear | |
| CN201040586Y (en) | Self-propelled passenger ladder | |
| CN203623922U (en) | Swinging guide rod type gangplank lifting and turning-over mechanism for ships | |
| CN103592143A (en) | Marine elevator test platform | |
| CN203460963U (en) | Cab capable of ascending and descending | |
| CN202766142U (en) | Gantry type hydraulic folding crane | |
| CN206203698U (en) | Scalable isolated pillar crane | |
| CN202322242U (en) | Rotary type derrick operating vehicle | |
| CN203959691U (en) | A kind of hatchcover seat crane | |
| CN201395087Y (en) | Adjustable military carriage shed |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20201125 Address after: Floor 1, building 3, No. 10, Gaopeng Avenue, high tech Zone, Chengdu, Sichuan 610000 Patentee after: Chengdu Hangli Equipment Technology Co., Ltd Address before: 10 No. 610041 Sichuan province Chengdu Gaopeng Road Patentee before: CHENGDU HOLY AVIATION SCIENCE & TECHNOLOGY Co.,Ltd. |
|
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20121121 |