CN2707619Y - Carrying and transporting equipment of airplane emergency rescue - Google Patents
Carrying and transporting equipment of airplane emergency rescue Download PDFInfo
- Publication number
- CN2707619Y CN2707619Y CN 200420003995 CN200420003995U CN2707619Y CN 2707619 Y CN2707619 Y CN 2707619Y CN 200420003995 CN200420003995 CN 200420003995 CN 200420003995 U CN200420003995 U CN 200420003995U CN 2707619 Y CN2707619 Y CN 2707619Y
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- Prior art keywords
- trailer
- towed
- tie
- towed vehicles
- airplane
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- 229910000831 Steel Inorganic materials 0.000 claims description 6
- 239000010959 steel Substances 0.000 claims description 6
- 239000012530 fluid Substances 0.000 claims description 4
- 238000012423 maintenance Methods 0.000 abstract description 4
- 238000000034 method Methods 0.000 abstract description 4
- 125000006850 spacer group Chemical group 0.000 abstract 1
- 230000001360 synchronised effect Effects 0.000 abstract 1
- 238000012857 repacking Methods 0.000 description 2
- 206010000369 Accident Diseases 0.000 description 1
- 210000001015 abdomen Anatomy 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 239000006260 foam Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229920002635 polyurethane Polymers 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
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Abstract
The utility model relates to a carrying and transporting apparatus of airplane emergency rescue comprising a three-axle trailer and a rotary support table arranged on the three-axle trailer. The rotary support table comprises a socket flange fixed on the three-axle trailer and a support platform connected with the socket flange through a steering mechanism. The platform is provided with a slide rail and two wedge-shaped support blocks fixed on the slide rail of the support platform through a spacer pin. The carrying and transporting apparatus of the airplane emergency rescue is also provided with one or two five-axle trailers connected with the three-axle trailer through a connecting beam and a wire cable. The two trailers are provided with hydraulic inclined platforms, and the hydraulic inclined platforms are connected through the connecting beam and the wire cable. The traction work is conducted by using a common airplane tractor by the utility model and minimum stress can be produced to the airplane in the rescue process to avoid producing a second damage to the airplane; various combining methods are suitable for the various rescue conditions of the airplanes; the apparatus has the maximal flexibility as a result of adopting the synchronous steering system and is convenient to be disassembled to conduct the tractor-trailer transportation on highways; the carrying and transporting apparatus of the airplane emergency rescue has the advantages of short preparing time for apparatus, high service efficiency and easy storage, and a little maintenance is needed.
Description
Technical field
The utility model relates to a kind of transportation device, specifically, relates to a kind of aircraft emergency management and rescue and moves transportation device.
Background technology
At present, if aircraft has an accident when causing alighting gear to damage, because wrecking equipment fast and effectively not, the airport just has only and closes the accident taxiway for a long time, treat the good undercarriage of on site maintenance after, could haul out aircraft.Close for a long time and will cause very big economic loss owing to runway like this.Perhaps use common trailers that accident aircraft is hauled out the accident area, this common trailers is easy to cause the passive safety of body owing to there is not excellent adaptability.Damage for serious full alighting gear, usually just can only the scene disassemble and transporting out of the scene of the accident.
The utility model content
The purpose of this utility model provides and a kind ofly is applicable to that the emergency management and rescue of all kinds aircraft move equipment.
Equipment is moved in aircraft emergency management and rescue described in the utility model, comprise that three holoaxials of a fluid pressure type turn to platform towed vehicle and rotation brace table mounted thereto, described rotation brace table comprises the base flange that is fixed on the towed vehicle, by steering hardware and base flange bonded assembly support platform, have slide rail on the platform and be fixedly mounted on two wedge shape back-up blocks on the support platform slideway by locating dowel pin.
The side of described three towed vehicles is equipped with the steel draw ring, and its front portion is equipped with the tie-beam that is connected with aircraft towing, and its rear portion is equipped with draws button or draw ring.
Also have five holoaxials of a hydraulic pressure and turn to the drag slab trailer, this towed vehicle is positioned at the rear of three towed vehicles, both by tie-beam be connected that wirerope is buckled with drawing of the rear portion that is arranged on three towed vehicles or draw ring is connected, hydraulically powered inclination brace table is installed on it.
Comprise that also five holoaxials of two hydraulic pressure turn to the drag slab trailer, two five towed vehicles lay respectively at the left back and the right abaft of three towed vehicles, both by tie-beam be connected wirerope and be arranged on drawing of three towed vehicle rear portions and link and connect, two three towed vehicles are connected with two wireropes by two tie-beams, are separately installed with hydraulically powered sloping platform on two five towed vehicles.
The side of described five towed vehicles is equipped with several steel draw rings, and its front portion is equipped with the three axle trailer bonded assembly and draws button or draw ring, and installed inside has drawing of being connected with front truck or another trailer to detain or draw ring between two trailers.
Described inclination brace table comprises cushion block and inclination stay bearing plate hinged with it, and cushion block is installed on five towed vehicles by bolt, and the inclination stay bearing plate rotates in 0～20 degree scope around its S. A., and rotation is by three hydraulic column jackings that are positioned at the outside.
Described inclination brace table comprises cushion block and a side and cushion block hinge, opposite side and three hydraulic column bonded assembly inclination stay bearing plates, and the inclination stay bearing plate rotates in 0～20 degree scope around its hinge axis, and cushion block is installed on five towed vehicles by bolt.
Described tie-beam is telescopic component, fixes with locating dowel pin between the extensible member; Described tie-beam all is connected with towed vehicle by latch.
Described tie-beam is telescopic component, fixes with locating dowel pin between the extensible member; Described tie-beam all is connected with towed vehicle by latch.
It is special in rescuing the wrecked aircraft design-calculated that alighting gear damages that equipment is moved in aircraft emergency management and rescue described in the utility model.It has the following advantages and good effect:
1, use the conventional airplane tractor truck can carry out traction work;
2, guarantee in the rescue process, aircraft to be produced minimum stress, avoid that aircraft is produced secondary and destroy;
3, be applicable to the rescue of various types of aircrafts, and have multiple array mode and can be fit to various aircrafts rescue situations;
4, adopt the fluid pressure type holoaxial to turn to the connecting rod Hydraulic Synchronizing steering swivel system of platform towed vehicle, when trailer turns to, each deflection angle of its three trailers remains on the same center of circle, thereby avoid the relative sideslip between the trailer, avoid that aircraft is produced secondary and destroy, make this equipment have maximum alerting ability;
5, can conveniently take tractor-trailer transportation on highway apart;
6, equipment setup time weak point, the service efficiency height;
7, be easy to deposit, only need a little maintenance.
Description of drawings
Fig. 1 is the structural representation that equipment is moved in aircraft emergency management and rescue described in the utility model;
Fig. 2 is the structural representation of rotation brace table;
Fig. 3 is the left side view of Fig. 2;
Fig. 4 is the birds-eye view of Fig. 2;
Fig. 5 is the enlarged drawing of A part among Fig. 1, is illustrated in the draw ring that is provided with on the trailer;
Fig. 6 is a structural representation of moving another embodiment of equipment described in the utility model;
Fig. 7 is the structural representation of sloping platform;
Fig. 8 is the birds-eye view of Fig. 7.
The specific embodiment
Referring to Fig. 1, equipment is moved in aircraft emergency management and rescue described in the utility model, comprises that three holoaxials of a fluid pressure type turn to platform towed vehicle 1 (three towed vehicles of hereinafter referred) and rotation brace table 2 mounted thereto.Rotation brace table 2 comprises the base flange 9 that is fixed on the towed vehicle, by steering hardware 8 and base flange 9 bonded assembly support platforms 7, has slide rail 12 on the platform and is fixedly mounted on two wedge shape back-up blocks 6 on the support platform slideway by locating dowel pin 10.
Referring to Fig. 2, Fig. 3 and Fig. 4, described support platform 7 is installed on the base flange by steering hardware 8, can guarantee that support platform 7 can rotate freely on base flange 9, can freely rotate with respect to three towed vehicles 1.Wedge shape back-up block 6 can move freely on flat-bed slide rail 12, and to satisfy the profile needs of various aircraft ventral, support platform 7 both sides are provided with spacing hole 11, by the position of locating dowel pin 10 stationary wedge back-up blocks.
When aircraft has an accident, when its nose-gear damages, aeroplane nose can be positioned over above-mentioned going up in the dress parts, utilize aircraft towing, whole aircraft traction can be left emergency area, until maintenance ground.
Referring to Fig. 6, the equipment of moving described in the utility model also has five holoaxials of a hydraulic pressure and turns to drag slab trailer 16 (five towed vehicles of hereinafter referred), this towed vehicle 16 is positioned at the rear of three towed vehicles, both by tie-beam 14 be connected drawing of the rear portion of wirerope 15 by being arranged on three towed vehicles buckle 5 or draw ring connect, hydraulically powered inclination brace table 17 is installed on it.
Further improvement of the utility model is also to have two five towed vehicles 16, two five towed vehicles 16 lay respectively at the left back and the right abaft of three towed vehicles 1, both by tie-beam 14 be connected wirerope 15 and be arranged on drawing of three towed vehicle rear portions and buckle 5 and be connected, the both sides of two five towed vehicles 4 are respectively arranged with several and draw button 5 or draw ring, be fixed on the draw ring with two wireropes 18 by two tie-beams 19 between the two and be connected, be separately installed with hydraulically powered sloping platform 17 on two five towed vehicles.
It is to turn to the drag slab trailer through following repacking to existing three holoaxials that described three holoaxials turn to drag slab trailer 1, the one, several steel draw rings 3 are installed in its side, be generally 8, be distributed in two sides, 4 of one sides, use when being used for fixing trailer and rotation brace table orientation, draw ring nominal load is 10 tons; The 2nd, improve the pipe link of trailer front portion, make it to adapt, to guarantee that having the smooth of tractor truck now with the airport is connected with the type of attachment of the tractor truck of aircraft; The 3rd, the trailer rear portion be equipped be connected with back car (five trailers) draw button 5 or draw ring.Be equipped with aircraft towing and be connected
Described three towed vehicle Maximum Loading Capacitys are 90 tons, and trailer vertical lift height is ± 50cm.
It is to turn to the drag slab trailer through following repacking to existing five holoaxials that described five holoaxials turn to drag slab trailer 16, the one, several steel draw rings 3 are installed in its two sides, generally can be 12, be distributed in two sides, 6 of one sides, use when being used for fixing the relative azimuth between the trailer, draw ring nominal load is 10 tons; The 2nd, be equipped with in the trailer front portion with the three axle trailer bonded assembly and draw button 5 or draw ring; The 3rd, between two trailers an inner side be equipped be connected with front truck (three axle trailer) or another trailer (five trailers) draw the button or draw ring.
150 tons of five towed vehicle Maximum Loading Capacity positions, trailer vertical lift height is ± 50cm.
Referring to Fig. 7 and Fig. 8, described inclination brace table 17 comprises cushion block 21 and inclination stay bearing plate 20 hinged with it, and cushion block is fixedly mounted on five towed vehicles 16 by bolt 23.Cushion block is used to regulate the height of inclination stay bearing plate, and for adapting to the needs of various aircraft, its cushion block has some groups, highly has nothing in common with each other, and can be used singly or in combination bolt together between each group.The inclination stay bearing plate can rotate in 0～20 degree scope around its S. A., and to adapt to all kinds aircraft, rotation is finished by three hydraulic column jackings that are positioned at the outside.
Preceding towed vehicle is connected with afterwards using tie-beam between the towed vehicle, and its tie-beam mainly works to bear tractive force.The connection wirerope that is provided with between each towed vehicle can guarantee between the trailer to keep flexibly connecting to a certain degree, and the relative position when mobile between them can have certain relative displacement, to reduce the passive safety that when aircraft is moved aircraft is caused.
Described tie-beam is formed by extensible member, fixes with locating dowel pin between the extensible member, to satisfy the actual needs of various aircraft.Connecting wirerope between the trailer in addition connects.Can guarantee that like this three hinges between the trailer can regulate, to adapt to the needs of different aircraft types.Described tie-beam all is connected with towed vehicle by latch, and is very convenient during work.
The equipment of moving described in the utility model can use or unite use separately, and the alighting gear damaged condition determined after its occupation mode was looked aircraft accident.When having only nose-gear to damage, only use a three axle trailer; When a side main landing gear damages, only use five trailers; When nose-gear and side main landing gear damage, use a three axle trailer and five trailers; When the both sides main landing gear damages, use two five trailers; When whole alighting gears damage more, use three trailers.
Aircraft has an accident when causing alighting gear to damage, and the using method of moving equipment described in the utility model is as follows:
1, utilize other aircraft wrecking equipments (do not belong to and originally move system) that the aircraft damaged location is held up so that trailer can enter the airframe bottom by ground earlier;
When if 2 accident states of ground do not allow breakdown lorry to enter, also need to lay interim road face, to improve the ground loading ability, satisfy the needs that vehicle moves;
3, trailer is moved to the aircraft bottom.Three axle trailer places the position of head bottom near nose-gear; Five trailers place the position of aircraft belly near the wing wing root;
4, regulate trailer height to the distance apart from body 0.2～0.3m, remaining space supports with other materials (polyurethane or air cushion, foam) that are fit to.For five trailers, can under brace table, add cushion block if desired to increase trailer height;
5, install between each trailer tie-beam be connected wirerope, the fixing relative position of trailer;
6, utilize hawser, clamping band that aircraft is fixed on the trailer;
7, utilize aircraft towing to drag aircraft away from the scene of the accident, site clearing etc.
Claims (9)
1, equipment is moved in the aircraft emergency management and rescue, it is characterized in that comprising that three holoaxials of a fluid pressure type turn to platform towed vehicle (1) and rotation brace table (2) mounted thereto, described rotation brace table (2) comprises the base flange (9) that is fixed on the towed vehicle, by steering hardware (8) and base flange bonded assembly support platform (7), have slide rail (12) on the platform and be fixedly mounted on two wedge shape back-up blocks (6) on the support platform slideway by locating dowel pin (10).
2, the equipment of moving according to claim 1 is characterized in that the side of described three towed vehicles (1) is equipped with steel draw ring (13), and its front portion is equipped with the tie-beam that is connected with aircraft towing, and its rear portion is equipped with draws button (5) or draw ring.
3, the equipment of moving according to claim 2, it is characterized in that also having five holoaxials of a hydraulic pressure and turn to drag slab trailer (16), this towed vehicle is positioned at the rear of three towed vehicles, both by tie-beam (14) be connected that wirerope (15) is buckled (5) with drawing of the rear portion that is arranged on three towed vehicles or draw ring is connected, hydraulically powered inclination brace table (17) is installed on it.
4, according to claim 2ly move setting, it is characterized in that also comprising that five holoaxials of two hydraulic pressure turn to drag slab trailer (16), two five towed vehicles (4) lay respectively at the left back and the right abaft of three towed vehicles (1), both by tie-beam be connected wirerope and be arranged on drawing of three towed vehicle rear portions and link and connect, two three towed vehicles (16) are connected with two wireropes (18) by two tie-beams (19), are separately installed with hydraulically powered sloping platform (17) on two five towed vehicles.
5, describedly move setting according to claim 3 or 4, the side that it is characterized in that described five towed vehicles (16) is equipped with several steel draw rings, its front portion is equipped with the three axle trailer bonded assembly and draws button (5) or draw ring, between two trailers installed inside have be connected with front truck or another trailer draw button (13) or draw ring.
6 describedly move setting according to claim 3 or 4, it is characterized in that described inclination brace table (17) comprises cushion block (21) and inclination stay bearing plate hinged with it (20), cushion block is installed on five towed vehicles (16) by bolt, the inclination stay bearing plate rotates in 0～20 degree scope around its S. A., and rotation is by three hydraulic columns (22) jacking that is positioned at the outside.
7, according to claim 5ly move setting, it is characterized in that described inclination brace table (17) comprises cushion block (21) and a side and cushion block (21) hinge, opposite side and three hydraulic columns (22) bonded assembly inclination stay bearing plates (20), the inclination stay bearing plate rotates in 0～20 degree scope around its hinge axis, and cushion block is installed on five towed vehicles (4) by bolt.
8, according to claim 6ly move setting, it is characterized in that described tie-beam is telescopic component, fixes with locating dowel pin between the extensible member; Described tie-beam all is connected with towed vehicle by latch.
9, according to claim 7ly move setting, it is characterized in that described tie-beam is telescopic component, fixes with locating dowel pin between the extensible member; Described tie-beam all is connected with towed vehicle by latch.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420003995 CN2707619Y (en) | 2004-04-26 | 2004-04-26 | Carrying and transporting equipment of airplane emergency rescue |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420003995 CN2707619Y (en) | 2004-04-26 | 2004-04-26 | Carrying and transporting equipment of airplane emergency rescue |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2707619Y true CN2707619Y (en) | 2005-07-06 |
Family
ID=34848319
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200420003995 Expired - Fee Related CN2707619Y (en) | 2004-04-26 | 2004-04-26 | Carrying and transporting equipment of airplane emergency rescue |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2707619Y (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103189275A (en) * | 2010-11-04 | 2013-07-03 | 梅西耶-道提有限公司 | Landing gear bogie beam with jacking dome |
| CN104071345A (en) * | 2014-07-04 | 2014-10-01 | 中国民航大学 | Front undercarriage carrying trailer for damaged aircraft |
| CN106043733A (en) * | 2016-06-15 | 2016-10-26 | 沈阳飞机工业（集团）有限公司 | Traction system used for traction of aircraft |
| CN107416192A (en) * | 2017-05-15 | 2017-12-01 | 河北天启通宇航空器材科技发展有限公司 | The axle connection mechanism of gyroplane wheel hub |
| CN108583927A (en) * | 2018-03-28 | 2018-09-28 | 中安（天津）航空设备有限公司 | A kind of trailer of achievable multiple combinations |
| CN116573152A (en) * | 2023-07-13 | 2023-08-11 | 中国人民解放军空军工程大学 | Omnidirectional driving aircraft rescue carrier with dynamic self-adjusting platform |
-
2004
- 2004-04-26 CN CN 200420003995 patent/CN2707619Y/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103189275A (en) * | 2010-11-04 | 2013-07-03 | 梅西耶-道提有限公司 | Landing gear bogie beam with jacking dome |
| CN103189275B (en) * | 2010-11-04 | 2016-04-06 | 梅西耶-道提有限公司 | A kind of airplane landing gear assemblies |
| CN104071345A (en) * | 2014-07-04 | 2014-10-01 | 中国民航大学 | Front undercarriage carrying trailer for damaged aircraft |
| CN106043733A (en) * | 2016-06-15 | 2016-10-26 | 沈阳飞机工业（集团）有限公司 | Traction system used for traction of aircraft |
| CN106043733B (en) * | 2016-06-15 | 2018-07-10 | 沈阳飞机工业（集团）有限公司 | A kind of trailer system for towing aircraft |
| CN107416192A (en) * | 2017-05-15 | 2017-12-01 | 河北天启通宇航空器材科技发展有限公司 | The axle connection mechanism of gyroplane wheel hub |
| CN108583927A (en) * | 2018-03-28 | 2018-09-28 | 中安（天津）航空设备有限公司 | A kind of trailer of achievable multiple combinations |
| CN116573152A (en) * | 2023-07-13 | 2023-08-11 | 中国人民解放军空军工程大学 | Omnidirectional driving aircraft rescue carrier with dynamic self-adjusting platform |
| CN116573152B (en) * | 2023-07-13 | 2023-09-19 | 中国人民解放军空军工程大学 | Omnidirectional driving aircraft rescue carrier with dynamic self-adjusting platform |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee |
Owner name: ROOM 201, HOUSE 36, DAXIONGYUJINXIANGSHE, YIZHUANG Free format text: FORMER NAME OR ADDRESS: NAN YA GAS PRODUCTS CO.,LTD., NANXINXING INDUSTRIAL PARK, RUYI EAST RD., YIZHUANG INDUSTRIAL PARK, BEIJING |
|
| CP03 | Change of name, title or address |
Patentee address after: Room 36, building 201, big Tulip House, Yizhuang Development Zone, Beijing Patentee address before: Yizhuang Beijing Industrial Park Ruyi East Road, South Xin Xing Industrial Park South Asia gas products Co., Ltd. |
|
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20050706 Termination date: 20110426 |