CN2546336Y - Towing platform car for emergency handling aircraft - Google Patents
Towing platform car for emergency handling aircraft Download PDFInfo
- Publication number
- CN2546336Y CN2546336Y CN 01247894 CN01247894U CN2546336Y CN 2546336 Y CN2546336 Y CN 2546336Y CN 01247894 CN01247894 CN 01247894 CN 01247894 U CN01247894 U CN 01247894U CN 2546336 Y CN2546336 Y CN 2546336Y
- Authority
- CN
- China
- Prior art keywords
- platform
- truck
- aircraft
- traction
- undercarriage
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- 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 - Fee Related
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Abstract
Disclosed is an aircraft emergency transfer platform truck which is used when the undercarriage is damaged and can not work in the process of taking off, landing, sliding and other situation. At the moment, the truck will walk on the ground instead of the undercarriage and quickly remove the aircraft to clear away the obstacle on the airport runway and ensure flight safety, so that the flights can resume normal operation. The truck is provided with a platform which is connected with the four wheels under the platform through a lifting structure; the wheels are of universal structure; a traction hitch head is arranged before the platform and is connected with a traction rod additionally arranged in emergency transfer; a hitch ear hole can be arranged behind the platform. A clip hoop is arranged on the platform to fasten the damaged undercarriage tires. During transfer, the truck is dragged by a tractor and a traction rod to carry the aircraft. The truck is convenient and suitable for all aviation aircraft models.
Description
(1) technical field: airplane emergency shifts the traction platform truck, belongs to other class vehicle not to be covered (B60R).
(2) background technology: airplane emergency shifts the traction platform truck be aircraft take off, land, slide or other in particular cases, alighting gear occurring damages, is out of shape, fractures or other mechanical breakdown, use in the time of can not working on, this moment, aircraft was if rest in the middle of the machine level ground inner track and when influencing the unfavorable position of aircraft safety, certainly will have a strong impact on the normal operation of flight.For avoiding the generation of safety misadventure, whole airport certainly will will be closed, cause the economic loss that can't estimate thus, airport, airline company, passenger will be the most direct victims, and consequent negative effect also can not be ignored, therefore, the aircraft that how will lack one or one above alighting gear shifts, draws to perch, recovers the normal operation of flight rapidly, ensures aircraft safety, the further deterioration of minimizing accident drops to bottom line to loss.Aircraft and during self alighting gear cisco unity malfunction, is the operation that ensures flight under emergency, and the question of substance that urgent traction is shifted has just been put on agenda.
(3) summary of the invention: when the utility model proposes a kind of aircraft and can not work on because of the alighting gear fault on the ground, can replace alighting gear to make the urgent traction platform truck that moves.The breakdown plane that uses this car need can be moved draws rapidly to perch or aircraft maintenance factory.The instant potential safety hazard of removing, the normal operation that recovers flight.Its technical scheme is as follows:
Airplane emergency shifts the traction platform truck, it is characterized in that establishing a platform 5, is connected with wheel 6 below it, and its front is provided with traction hanging head 8 or hangers hole 9; The plane is provided with the clip that is connected with alighting gear 10 on the platform 5; Platform is connected employing lifting structure 7 with wheel; Wheel 6 adopts can be according to the universal structure of the automatic correction of movement track of tractive force.Be provided with fixing hoop 11 and movable clip 2 in the clip, and movable clip is provided with screw rod 4 and the nut 3 that matches that the realization that rotates tightens up alighting gear 10.4 of wheel 6 general employings.The platform front has traction hanging head 8 also can set up hangers hole 9 simultaneously in the back.
The utility model beneficial effect:
1, is provided with movable clip 2, fixing hoop 11 can hold the undercarriage tire, traction platform truck and alighting gear are held together, thereby replace alighting gear to make walking movement on ground, clip 2 rotates by nut 3 screw rods 4 and realizes fixing alighting gear 10.2, platform 5 is connected employing lifting structure 7 with wheel 6, can do the random adjustment of height up and down, guarantees aircraft is horizontal, and is convenient to the safe transfer traction.3, the crawler body of each platform truck is made of 4 wheels, and motion is steady, and load-carrying capacity is strong.4, wheel structure all is designed to universal structure, and himself can be according to the automatic correction of movement track of tractive force.5, traction hanging head 8 is established in the platform front, and it can directly be connected with the aircraft draw bar, as the stressed main position of traction.6, the platform back is established the hangers hole and is done to adopt hangers hole 9 convenient and swift when traction connects the traction of suitable longer distance with steel cable.Also can be used as simultaneously the connection of Other related equipment facility.7, this platform truck is convenient and practical, and can be fit to all aviation types and use, be the emergency serving unit of airport, various places ground service service guarantee department practicality.
(4) description of drawings
Fig. 1 the utility model front elevation
Fig. 2 the utility model birds-eye view
Fig. 3 the utility model running condition diagrammatic sketch (being connected diagram with tractor truck) with aircraft
(5) specific embodiment
See Fig. 1, Fig. 2, establish four wheels 6 below the platform 1, both adopt lifting structure 7 to connect, and wheel 6 adopts can be according to the universal structure of the automatic correction of movement track of tractive force.Establish traction hanging head 8 before the platform, hangers hole 9 is established in the back.Establish fixing hoop 11 and movable clip 2 on the platform.On the movable clip 2 screw rod 4 and nut 3 are housed.
Use: certain aircraft 12 causes left side main landing gear 10 breakking away on 13 on the primary runway
aFracture, can not continue, and do traction and move,, recover runway safety and use normally, guarantee the normal operation of flight, must aircraft be drawn to safety zone with utmost dispatch for rapidly this breakdown plane being transferred to safety zone at ground run.The concrete operations step is as follows, with mechanical jack or gas edge aircraft is held up built on stilts, and its terrain clearance is advisable for the traction platform truck can push in, with three (look alighting gear what and different, generally use three) draw platform truck and place nose-gear 10 respectively
bLeft and right sides main landing gear 10
aBelow, rotary screw 4 is held alighting gear 10 tightly by nut 3 and clip 2.Owing to after alighting gear is impaired, change highly to some extent, adjust lifting structure 7, aircraft is horizontal, be convenient to the safe transfer traction.Take off jack or gas edge this moment, platform truck finishes with regard to being connected with alighting gear.Connecting platform trucks traction hanging heads 8 with tractor truck 15 by draw bar 14 can draw aircraft, is transferred to safety zone rapidly or directly draws to aircraft maintenance factory and keep in repair.So far, airplane emergency moves the traction end-of-job, and flight promptly recovers normal operation.
Claims (4)
1, airplane emergency shifts the traction platform truck, it is characterized in that establishing a platform (5), is connected with wheel (6) below it, and traction hanging head (8) or hangers hole (9) are established in its front; Platform (5) is gone up the plane and is provided with the clip that is connected with alighting gear (10); Platform is connected employing lifting structure (7) with wheel; Wheel (6) adopts can be according to the universal structure of the automatic calibration path of motion of traction.
2,, it is characterized in that being provided with in the clip fixing hoop (11) and movable clip (2), and movable clip is provided with the realization that rotates and tightens up the screw rod (4) of alighting gear (10) and the nut (3) that matches by the described platform truck of claim 1.
3,, it is characterized in that wheel (6) adopts 4 by the described platform truck of claim 1.
4,, it is characterized in that the front is provided with traction hanging head (8) and is provided with hangers hole (9) in the back by the described platform truck of claim 1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 01247894 CN2546336Y (en) | 2001-10-16 | 2001-10-16 | Towing platform car for emergency handling aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 01247894 CN2546336Y (en) | 2001-10-16 | 2001-10-16 | Towing platform car for emergency handling aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2546336Y true CN2546336Y (en) | 2003-04-23 |
Family
ID=33658658
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 01247894 Expired - Fee Related CN2546336Y (en) | 2001-10-16 | 2001-10-16 | Towing platform car for emergency handling aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2546336Y (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103057723A (en) * | 2011-10-21 | 2013-04-24 | 成都思茂科技有限公司 | Damping type aircraft rescue pavement transfer platform |
| CN103538731A (en) * | 2008-11-25 | 2014-01-29 | 以色列宇航工业有限公司 | Towbarless airplane tug |
| CN103625632A (en) * | 2013-11-29 | 2014-03-12 | 陈科学 | Manned aircraft |
| CN103946112A (en) * | 2011-11-08 | 2014-07-23 | 斯瓦沃米尔·马利茨基 | A carriage assembly for an airplane transporting system on an airport apron |
| CN104773302A (en) * | 2015-04-28 | 2015-07-15 | 北京新胜福瑞机械设备有限公司 | Emergency rescue device for airplane |
| CN104986351A (en) * | 2015-07-10 | 2015-10-21 | 常州市科宏电子电器有限公司 | Aircraft tow bar and method for towing aircraft through constant tension |
| CN108001703A (en) * | 2017-11-30 | 2018-05-08 | 江西洪都航空工业集团有限责任公司 | A kind of linkage of towing aircraft |
| CN108557109A (en) * | 2018-03-26 | 2018-09-21 | 中国人民解放军第五七零工厂 | Emergency escape runway device and application method |
| RU2714337C2 (en) * | 2017-12-28 | 2020-02-14 | Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации | Aircraft evacuation device |
| CN114084367A (en) * | 2021-12-22 | 2022-02-25 | 中国民航大学 | Emergency rescue equipment for tire burst of airplane wheel, use method and application |
-
2001
- 2001-10-16 CN CN 01247894 patent/CN2546336Y/en not_active Expired - Fee Related
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103538731A (en) * | 2008-11-25 | 2014-01-29 | 以色列宇航工业有限公司 | Towbarless airplane tug |
| CN103538731B (en) * | 2008-11-25 | 2016-05-04 | 以色列宇航工业有限公司 | Without draw bar aircraft trailer |
| CN103057723A (en) * | 2011-10-21 | 2013-04-24 | 成都思茂科技有限公司 | Damping type aircraft rescue pavement transfer platform |
| CN103946112B (en) * | 2011-11-08 | 2016-02-03 | 斯瓦沃米尔·马利茨基 | The trailer assembly of the aerocraft movement system on airport hardstand |
| CN103946112A (en) * | 2011-11-08 | 2014-07-23 | 斯瓦沃米尔·马利茨基 | A carriage assembly for an airplane transporting system on an airport apron |
| CN103625632A (en) * | 2013-11-29 | 2014-03-12 | 陈科学 | Manned aircraft |
| CN104773302A (en) * | 2015-04-28 | 2015-07-15 | 北京新胜福瑞机械设备有限公司 | Emergency rescue device for airplane |
| CN104986351A (en) * | 2015-07-10 | 2015-10-21 | 常州市科宏电子电器有限公司 | Aircraft tow bar and method for towing aircraft through constant tension |
| CN108001703A (en) * | 2017-11-30 | 2018-05-08 | 江西洪都航空工业集团有限责任公司 | A kind of linkage of towing aircraft |
| RU2714337C2 (en) * | 2017-12-28 | 2020-02-14 | Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации | Aircraft evacuation device |
| CN108557109A (en) * | 2018-03-26 | 2018-09-21 | 中国人民解放军第五七零工厂 | Emergency escape runway device and application method |
| CN108557109B (en) * | 2018-03-26 | 2024-03-29 | 凌云(宜昌)航空装备工程有限公司 | Emergency off-runway device and use method thereof |
| CN114084367A (en) * | 2021-12-22 | 2022-02-25 | 中国民航大学 | Emergency rescue equipment for tire burst of airplane wheel, use method and application |
| CN114084367B (en) * | 2021-12-22 | 2023-03-24 | 中国民航大学 | Emergency rescue equipment for tire burst of airplane wheel, use method and application |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |