CN104015935A - Airframe supporting platform - Google Patents
Airframe supporting platform Download PDFInfo
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- CN104015935A CN104015935A CN201410245915.9A CN201410245915A CN104015935A CN 104015935 A CN104015935 A CN 104015935A CN 201410245915 A CN201410245915 A CN 201410245915A CN 104015935 A CN104015935 A CN 104015935A
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- sliding block
- plate
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- hinged
- airframe
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Abstract
An airframe supporting platform comprises a base, two side face hydraulic cylinders, two baffles, two sliding block plates and two middle hydraulic cylinders, wherein the base is horizontally arranged; each sliding block plate is formed by a right-angle triangular prism body and a flat plate in an integrated mode, the two sliding block plates are arranged on the two sides of the surface of the base through moving pairs, and the two ends of the two middle hydraulic cylinders are hinged between the two sides of the bottoms of the opposite inclined planes on the two sliding block plates respectively; the lower end of each baffle is hinged to the upper end of the right-angle triangular prism body on the corresponding sliding block plate; the two ends of each side face hydraulic cylinder are respectively hinged between the back face of one baffle and the outer end of the flat plate on the corresponding sliding block plate. The sliding block plates and the baffles can respectively move individually, so that adjusting space of an airplane contact face is large, and the airframe supporting platform is suitable for various airplane types; five faces, making contact with the airplane, on the airframe supporting platform are respectively provided with a pressure sensor to make pressures on the five faces be equal, and therefore the supporting effect for an airplane nose is better. The platform has the advantages of being simple and reasonable in structural design, small in size, easy to operate and the like, and the fit degree of the platform and the cambered surface of the airplane nose is high.
Description
Technical field
The invention belongs to civilian boat equipment technology field, particularly relate to a kind of airframe support platform.
Background technology
At present aeroplane rescure car by increasing airport in the world as standard equipment.For the impaired or inoperable aircraft of nose-gear, it is fixing that aeroplane rescure car is often used airframe support platform to support plane nose, thereby make aeroplane rescure car can carry reposefully impaired aircraft.But the clamping body at present conventional airframe support platform is to place two to have the fixedly wedge shaped baffle of the gradient on base, so can not fit with the cambered surface of plane nose well, can only be applicable to a small amount of type.And the movement of baffle plate needs manual operation, so the moving velocity of baffle plate is slow, therefore do not meet the requirement of Quick rescue aircraft, and itself and the discontinuity of aircraft contact surface, so easily aircraft is caused to secondary damage.
Summary of the invention
In order to address the above problem, the object of the present invention is to provide a kind of airframe support platform, this mechanism has small volume, high with plane nose cambered surface laminating degree, Fit Models is many, five surface pressures contacting with plane nose equate and simple operation and other advantages.
In order to achieve the above object, airframe support platform provided by the invention comprises base, two side hydraulic actuating cylinders, two baffle plates, two slider plate and two middle part hydraulic actuating cylinders; Wherein base is horizontally disposed with, and bottom surface is connected with the vehicle frame of aeroplane rescure car; Slider plate by right-angle prismatic cylinder be connected to the vertical basifacial dull and stereotyped one of right-angle prismatic cylinder and form, two slider plate are arranged on position, susceptor surface both sides in the relative mode of right-angle prismatic cylinder ramp by moving sets; The two ends of two middle part hydraulic actuating cylinders are hinged on respectively between inclined-plane two bottom sides relative in two slider plate; The lower end of every baffle plate is hinged on the upper end of right-angle prismatic cylinder in a slider plate, and two baffle-panels opposites arrange; The two ends of each side hydraulic actuating cylinder are hinged on respectively between the baffle plate back side of the same side and the outer end of slider plate upper flat plate.
The middle part, surface of the middle part surface of described base, middle part, two right-angle prismatic cylinder ramp surfaces and two baffle plates is respectively equipped with a pressure sensor, and pressure sensor is electrically connected to the read out instrument on aeroplane rescure car.
Slider plate in airframe support platform provided by the invention and baffle plate self-movement separately, so the adjustment space of itself and aircraft contact surface is large, so applicable to different types of machines; By being all provided with pressure sensor on five faces that contact with aircraft thereon, thus can make the pressure of these five faces equate, therefore better to the support effect of plane nose.In addition, it is simple, rationally that this airframe support platform also has structure design, small volume,, lighter weight high with plane nose cambered surface laminating degree, simple operation and other advantages.
Accompanying drawing explanation
Fig. 1 is airframe support platform structure front elevation provided by the invention.
Fig. 2 is airframe support platform structural perspective provided by the invention.
The specific embodiment
Below in conjunction with the drawings and specific embodiments, airframe support platform provided by the invention is described in detail.
As shown in Figure 1 and Figure 2, airframe support platform provided by the invention comprises base 1, two side hydraulic actuating cylinders 2, two baffle plates 3, two slider plate 4 and two middle part hydraulic actuating cylinders 5; Wherein base 1 is horizontally disposed with, and bottom surface is connected with the vehicle frame of aeroplane rescure car; Slider plate 4 by right-angle prismatic cylinder 6 be connected to vertical basifacial dull and stereotyped 7 one of right-angle prismatic cylinder 6 and form, two slider plate 4 are arranged on position, the surperficial both sides of base 1 in the relative mode of right-angle prismatic cylinder 6 ramps by moving sets; The two ends of two middle part hydraulic actuating cylinders 5 are hinged on respectively between inclined-plane two bottom sides relative in two slider plate 4; The lower end of every baffle plate 3 is hinged on the upper end of right-angle prismatic cylinder 6 in a slider plate 4, and two baffle plates 3 arrange face-to-face; The two ends of each side hydraulic actuating cylinder 2 are hinged on respectively between baffle plate 3 back sides of the same side and the outer end of slider plate 4 upper flat plates 7.
The middle part, surface of the middle part surface of described base 1, two right-angle prismatic cylinder 6 middle parts, ramp surface and two baffle plates 3 is respectively equipped with a pressure sensor, and pressure sensor is electrically connected to the read out instrument on aeroplane rescure car.
Now airframe support platform using method provided by the invention is described below: in the time need to carrying impaired aircraft, first utilize crane by airframe lifting, then make aeroplane rescure car move to airframe below, and make the lucky alignment machine centriciput in middle part of the airframe support platform upper bed-plate 1 on it, utilize afterwards crane to make airframe slow decreasing, until bottom surface, head middle part contacts with base 1 middle part, surface, then start two middle part hydraulic actuating cylinders 5, its piston rod is inwardly shunk, under the effect of this piston rod, two slider plate 4 will be along base 1 relative to moving to centre, final and head Surface Contact, start afterwards two side hydraulic actuating cylinders 2, make its piston rod protruding, under the effect of this piston rod, will inwardly overturn in the top of two baffle plates 3, thereby contact with head surface.On the read out instrument of staff at aeroplane rescure car, observe in the middle part of base 1 middle part surface, two right-angle prismatic cylinder 6 ramp surfaces and when the force value of the pressure sensor at two baffle plates 3 middle parts, surface is identical, stop the action of side hydraulic actuating cylinder 2 and middle part hydraulic actuating cylinder 5, thus head is firmly supported and fixed, at this moment just can utilize aeroplane rescure car to carry impaired aircraft.
Claims (2)
1. an airframe support platform, is characterized in that: it comprises base (1), two side hydraulic actuating cylinders (2), two baffle plates (3), two slider plate (4) and two middle part hydraulic actuating cylinders (5); Wherein base (1) is horizontally disposed with, and bottom surface is connected with the vehicle frame of aeroplane rescure car; Slider plate (4) by right-angle prismatic cylinder (6) be connected to the vertical basifacial flat board of right-angle prismatic cylinder (6) (7) one and form, two slider plate (4) are arranged on position, the surperficial both sides of base (1) in the relative mode of right-angle prismatic cylinder (6) ramp by moving sets; The two ends of two middle part hydraulic actuating cylinders (5) are hinged on respectively between the upper relative inclined-plane two bottom sides of two slider plate (4); The lower end of every baffle plate (3) is hinged on the upper end of the upper right-angle prismatic cylinder (6) of a slider plate (4), and two baffle plates (3) arrange face-to-face; The two ends of each side hydraulic actuating cylinder (2) are hinged on respectively and are positioned between baffle plate (3) back side of the same side and the outer end of slider plate (4) upper flat plate (7).
2. airframe support platform according to claim 1, it is characterized in that: the middle part, surface of the middle part surface of described base (1), middle part, two right-angle prismatic cylinders (6) ramp surface and two baffle plates (3) is respectively equipped with a pressure sensor, and pressure sensor is electrically connected to the read out instrument on aeroplane rescure car.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410245915.9A CN104015935B (en) | 2014-06-04 | 2014-06-04 | A kind of airframe support platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410245915.9A CN104015935B (en) | 2014-06-04 | 2014-06-04 | A kind of airframe support platform |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104015935A true CN104015935A (en) | 2014-09-03 |
| CN104015935B CN104015935B (en) | 2016-04-27 |
Family
ID=51433014
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410245915.9A Active CN104015935B (en) | 2014-06-04 | 2014-06-04 | A kind of airframe support platform |
Country Status (1)
| Country | Link |
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| CN (1) | CN104015935B (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106976025A (en) * | 2017-04-18 | 2017-07-25 | 大明重工有限公司 | A kind of interchangeable heat treatment support |
| CN112623216A (en) * | 2020-12-28 | 2021-04-09 | 大连大学 | Rescue aircraft for passenger plane in distress in air |
| CN112660379A (en) * | 2020-12-28 | 2021-04-16 | 大连大学 | Method for rescuing passenger plane in distress by using aircraft |
| CN112796237A (en) * | 2019-11-14 | 2021-05-14 | 北京三快在线科技有限公司 | Unmanned aerial vehicle parking device and system |
| CN113247292A (en) * | 2021-06-28 | 2021-08-13 | 中国船舶重工集团公司第七一三研究所 | Multifunctional aircraft rescue platform |
| GB2598973A (en) * | 2020-09-17 | 2022-03-23 | Coughlin Daniel | Shoring system for aircraft and the like |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3671013A (en) * | 1970-05-25 | 1972-06-20 | Kirke B Everson Jr | Aircraft hangaring support |
| US4596506A (en) * | 1983-02-16 | 1986-06-24 | Mcdonnell Douglas Corporation | Air bearing wheel lift |
| US5709520A (en) * | 1996-01-26 | 1998-01-20 | Pish; Paul J. | Portable wheel dolly |
| CN201253802Y (en) * | 2008-09-23 | 2009-06-10 | 湖南城市学院 | Grinding disc lifting apparatus of grinding machine |
| CN201432186Y (en) * | 2009-06-08 | 2010-03-31 | 上海泰胜(东台)电力工程机械有限公司 | Wheel stand for welding circumferential weld of assembled wind-power tower drums |
| CN202046441U (en) * | 2010-12-03 | 2011-11-23 | 李荣田 | Aircraft rescuing and moving trailer |
-
2014
- 2014-06-04 CN CN201410245915.9A patent/CN104015935B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3671013A (en) * | 1970-05-25 | 1972-06-20 | Kirke B Everson Jr | Aircraft hangaring support |
| US4596506A (en) * | 1983-02-16 | 1986-06-24 | Mcdonnell Douglas Corporation | Air bearing wheel lift |
| US5709520A (en) * | 1996-01-26 | 1998-01-20 | Pish; Paul J. | Portable wheel dolly |
| CN201253802Y (en) * | 2008-09-23 | 2009-06-10 | 湖南城市学院 | Grinding disc lifting apparatus of grinding machine |
| CN201432186Y (en) * | 2009-06-08 | 2010-03-31 | 上海泰胜(东台)电力工程机械有限公司 | Wheel stand for welding circumferential weld of assembled wind-power tower drums |
| CN202046441U (en) * | 2010-12-03 | 2011-11-23 | 李荣田 | Aircraft rescuing and moving trailer |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106976025A (en) * | 2017-04-18 | 2017-07-25 | 大明重工有限公司 | A kind of interchangeable heat treatment support |
| CN112796237A (en) * | 2019-11-14 | 2021-05-14 | 北京三快在线科技有限公司 | Unmanned aerial vehicle parking device and system |
| GB2598973A (en) * | 2020-09-17 | 2022-03-23 | Coughlin Daniel | Shoring system for aircraft and the like |
| GB2598973B (en) * | 2020-09-17 | 2022-11-02 | Coughlin Daniel | Shoring system for aircraft and the like |
| CN112623216A (en) * | 2020-12-28 | 2021-04-09 | 大连大学 | Rescue aircraft for passenger plane in distress in air |
| CN112660379A (en) * | 2020-12-28 | 2021-04-16 | 大连大学 | Method for rescuing passenger plane in distress by using aircraft |
| CN112660379B (en) * | 2020-12-28 | 2023-04-07 | 大连大学 | Method for rescuing passenger plane in distress by using aircraft |
| CN112623216B (en) * | 2020-12-28 | 2023-04-07 | 大连大学 | Rescue aircraft for passenger plane in distress in air |
| CN113247292A (en) * | 2021-06-28 | 2021-08-13 | 中国船舶重工集团公司第七一三研究所 | Multifunctional aircraft rescue platform |
Also Published As
| Publication number | Publication date |
|---|---|
| CN104015935B (en) | 2016-04-27 |
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