CN104015935B - A kind of airframe support platform - Google Patents
A kind of airframe support platform Download PDFInfo
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- CN104015935B CN104015935B CN201410245915.9A CN201410245915A CN104015935B CN 104015935 B CN104015935 B CN 104015935B CN 201410245915 A CN201410245915 A CN 201410245915A CN 104015935 B CN104015935 B CN 104015935B
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- slider plate
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- hydraulic actuating
- cylinder
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Abstract
A kind of airframe support platform.It comprises base, two side hydraulic actuating cylinders, two pieces of baffle plates, two slider plate and two middle part hydraulic actuating cylinders; Base is horizontally disposed with; Slider plate is integrally made up of right-angle prismatic cylinder and flat board, and two slider plate are located at position, susceptor surface both sides by moving sets; Hydraulic actuating cylinder two ends, two middle parts are hinged between inclined-plane two bottom sides relative in two slider plate respectively; Every block baffle plate lower end is hinged on the upper end of right-angle prismatic cylinder in a slider plate; Hydraulic actuating cylinder two ends, each side are hinged between the baffle plate back side and slider plate upper flat plate outer end respectively.Slider plate in the present invention and baffle plate can self-movements separately, and therefore the adjustment space of aircraft contact surface is large, is applicable to different types of machines; Five faces that it contacts with aircraft are all provided with pressure sensor, so the pressure in these five faces can be made equal, to handpiece support better effects if.This platform has structure design advantages of simple, and volume is little, with high, the simple to operate advantage of plane nose cambered surface laminating degree.
Description
Technical field
The invention belongs to civilian boat equipment technology field, particularly relate to a kind of airframe support platform.
Background technology
Current aeroplane rescure car by increasing airport in the world as standard equipment.Impaired or the inoperable aircraft for nose-gear, aeroplane rescure car often uses airframe support platform to carry out support to plane nose and fixes, thus makes aeroplane rescure car can carry impaired aircraft reposefully.But the clamping body in airframe support platform conventional at present places the wedge shaped baffle that two have the fixing 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 the discontinuity of itself and aircraft contact surface, therefore easy secondary damage is caused to aircraft.
Summary of the invention
In order to solve the 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 are equal 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 pieces of 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 is by right-angle prismatic cylinder and be connected to the basifacial flat board of right-angle prismatic column vertical and integrally form, and two slider plate are arranged on position, susceptor surface both sides in the mode that right-angle prismatic cylinder ramp is relative by moving sets; The two ends of two middle part hydraulic actuating cylinders are hinged between inclined-plane two bottom sides relative in two slider plate respectively; The lower end of every block baffle plate is hinged on the upper end of right-angle prismatic cylinder in a slider plate, and two pieces of baffle-panels opposites are arranged; The two ends of each side hydraulic actuating cylinder are hinged on respectively between the baffle plate back side and the outer end of slider plate upper flat plate of the same side.
The surface middle part of the middle part surface of described base, two right-angle prismatic cylinder ramp surface middle part and two pieces of baffle plates is respectively equipped with a pressure sensor, and pressure sensor is electrically connected with the read out instrument on aeroplane rescure car.
Slider plate in airframe support platform provided by the invention and baffle plate can self-movements separately, and therefore the adjustment space of itself and aircraft contact surface is large, so be applicable to different types of machines; All pressure sensor is provided with by five faces contacted with aircraft thereon, so the pressure in these five faces can be made equal, therefore better to the support effect of plane nose.In addition, it is simple, reasonable that this airframe support platform also has structure design, small volume, lighter weight, simple operation and other advantages high with plane nose cambered surface laminating degree.
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.
Detailed description of the invention
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 pieces of 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 is integrally made up of right-angle prismatic cylinder 6 vertical with being connected to right-angle prismatic cylinder 6 basifacial dull and stereotyped 7, and two slider plate 4 are arranged on position, base 1 surperficial both sides in the mode that right-angle prismatic cylinder 6 ramp is relative by moving sets; The two ends of two middle part hydraulic actuating cylinders 5 are hinged between inclined-plane two bottom sides relative in two slider plate 4 respectively; The lower end of every block baffle plate 3 is hinged on the upper end of right-angle prismatic cylinder 6 in a slider plate 4, and two pieces of baffle plates 3 are arranged face-to-face; The two ends of each side hydraulic actuating cylinder 2 are hinged on respectively between baffle plate 3 back side and the outer end of slider plate 4 upper flat plate 7 of the same side.
The surface middle part of the middle part surface of described base 1, two right-angle prismatic cylinder 6 ramp surface middle part and two pieces of baffle plates 3 is respectively equipped with a pressure sensor, and pressure sensor is electrically connected with the read out instrument on aeroplane rescure car.
Now airframe support platform using method provided by the invention is described below: when needing to carry impaired aircraft, first utilize crane by airframe lifting, then aeroplane rescure car is made to move to below airframe, and make the lucky alignment machine centriciput in middle part of the airframe support platform upper bed-plate 1 on it, utilize crane that airframe is slowly declined afterwards, until bottom surface contacts with base 1 surface middle part in the middle part of head, then two middle part hydraulic actuating cylinders 5 are started, its piston rod is inwardly shunk, under the effect of this piston rod, two slider plate 4 will be relative middle mobile along base 1, final and head surface contact, start two side hydraulic actuating cylinders 2 afterwards, make its piston rod protruding, under the effect of this piston rod, the top of two pieces of baffle plates 3 will inwardly overturn, thus contact with head surface.When the force value that staff observes the pressure sensor of base 1 middle part surface, two right-angle prismatic cylinder 6 ramp surface middle part and two pieces of baffle plate 3 surface middle part on the read out instrument of aeroplane rescure car is identical, stop the action of side hydraulic actuating cylinder 2 and middle part hydraulic actuating cylinder 5, thus head is firmly supported and fix, aeroplane rescure car at this moment just can be utilized to have carried impaired aircraft.
Claims (2)
1. an airframe support platform, is characterized in that: it comprises base (1), two side hydraulic actuating cylinders (2), two pieces of baffle plates (3), two slider plate (4) and two middle parts hydraulic actuating cylinder (5); Wherein base (1) is horizontally disposed with, and bottom surface is connected with the vehicle frame of aeroplane rescure car; Slider plate (4) is made up of right-angle prismatic cylinder (6) basifacial flat board (7) one vertical with being connected to right-angle prismatic cylinder (6), and two slider plate (4) are arranged on position, base (1) surperficial both sides in the mode that right-angle prismatic cylinder (6) ramp is relative by moving sets; The two ends of two middle parts hydraulic actuating cylinder (5) are hinged between the upper relative inclined-plane two bottom sides of two slider plate (4) respectively; The lower end of every block baffle plate (3) is hinged on the upper end of the upper right-angle prismatic cylinder (6) of a slider plate (4), and two pieces of baffle plates (3) are arranged face-to-face; The two ends of each side hydraulic actuating cylinder (2) be hinged on respectively be positioned at the same side between baffle plate (3) back 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 surface middle part of the middle part surface of described base (1), two right-angle prismatic cylinder (6) ramp surface middle part and two pieces of baffle plates (3) is respectively equipped with a pressure sensor, and pressure sensor is electrically connected with 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 CN104015935A (en) | 2014-09-03 |
| CN104015935B true CN104015935B (en) | 2016-04-27 |
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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) |
Families Citing this family (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 |
| CN112796237B (en) * | 2019-11-14 | 2022-05-10 | 北京三快在线科技有限公司 | Unmanned aerial vehicle parking device and system |
| GB202014672D0 (en) * | 2020-09-17 | 2020-11-04 | Support Air Ltd | Multi aircraft type - shoring system - MATSS |
| CN112623216B (en) * | 2020-12-28 | 2023-04-07 | 大连大学 | Rescue aircraft for passenger plane in distress in air |
| CN112660379B (en) * | 2020-12-28 | 2023-04-07 | 大连大学 | Method for rescuing passenger plane in distress by using aircraft |
| CN113247292B (en) * | 2021-06-28 | 2022-11-29 | 中国船舶重工集团公司第七一三研究所 | Multifunctional aircraft rescue platform |
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 |
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| Publication number | Publication date |
|---|---|
| CN104015935A (en) | 2014-09-03 |
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