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Disassembling vehicle for front landing gear of airplane

A front landing gear and aircraft technology, applied in metal processing, metal processing equipment, manufacturing tools, etc., can solve the problems of low work efficiency, time-consuming disassembly and assembly, inconvenient operation, etc., to reduce work intensity and ease level adjustment. , the effect of low cost

Active Publication Date: 2014-12-17
成都东科信航空自控设备有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, due to the design of the aircraft, the space of the "landing gear storage compartment" of the aircraft is narrow, and the disassembly and assembly of the tooling is time-consuming and laborious.
When dismantling and installing the landing gear, the operator needs to take out the connecting pin, rotate the landing gear 90 degrees, and then move down to take out the landing gear. This operation is not only inconvenient, but the labor intensity of the operator is relatively large, and the work efficiency is also low, and there are security risks

Method used

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  • Disassembling vehicle for front landing gear of airplane
  • Disassembling vehicle for front landing gear of airplane
  • Disassembling vehicle for front landing gear of airplane

Examples

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Embodiment

[0042] Such as Figure 1-7 As shown, the aircraft front landing gear disassembly vehicle mainly includes a lifting mechanism, an adjusting and aligning mechanism arranged on the lifting mechanism and a working platform 9 arranged on the adjusting and aligning mechanism.

[0043] Described elevating mechanism comprises the rectangular underframe 1 that has sliding groove on both sides, the sliding bar 7 that two ends are arranged in the sliding groove of rectangular underframe 1, and two groups are passed by outer scissor bar 25 and inner scissor bar 24. The center pin 22 is a height adjustment frame that is flexibly connected in a cross shape, and a center pin washer 23 is also provided between the center pin 22 and the inner scissor rod 24; in the two groups of height adjustment frames, two outer scissors The lower ends of the rod 25 are respectively arranged on the two ends of the sliding rod 7, and the lower ends of the two inner scissor rods 24 are respectively arranged on...

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Abstract

The invention discloses a disassembling vehicle for a front landing gear of an airplane and a control method of the disassembling vehicle. The disassembling vehicle is characterized by mainly comprising a lifting mechanism, an adjusting alignment mechanism and a working platform (9), wherein the adjusting alignment mechanism is arranged on the lifting mechanism, and the working platform (9) is disposed on the adjusting alignment mechanism. The disassembling vehicle and the control method aim to overcome shortcomings that in the prior art, disassembly operation of a front landing gear of an airplane is time-wasting and labor-wasting, and causes potential safety hazards. The disassembling vehicle is simple in structure and convenient in use, work intensity of operators during disassembly operation of the front landing gear of the airplane is greatly reduced, and accordingly the disassembling vehicle and the control method are worthy of being popularized and applied.

Description

technical field [0001] The invention relates to a disassembly and assembly device of an aircraft landing gear, in particular to a vehicle for disassembling and assembling the nose landing gear of an aircraft. Background technique [0002] At present, due to the design of the aircraft, the space of the "landing gear storage compartment" of the aircraft is narrow, and the disassembly and assembly of the tooling is time-consuming and laborious. When dismantling and installing the landing gear, the operator needs to take out the connecting pin, rotate the landing gear 90 degrees, and then move down to take out the landing gear. This operation is not only inconvenient, but the labor intensity of the operator is relatively large, and the work efficiency It is also low, and there are security risks. Contents of the invention [0003] The object of the present invention is to overcome above-mentioned defect, provide a kind of not only safe and convenient to use, but also cheap ai...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23P19/00
Inventor 刘建武戴建平
Owner 成都东科信航空自控设备有限公司