A new type of assembly frame for aircraft

A new type of aircraft technology, applied in the field of assembly jigs for new aircraft, can solve the problems of inconvenient equipment control and affecting combined processing, etc., and achieve the effect of simple structure, easy assembly and strong stability

Active Publication Date: 2021-09-21
GUANGDONG KNOWLEDGE CITY OPERATION SERVICES CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] The number of assembly frames used in aircraft manufacturing is large, so whether the structure design of the assembly frame is reasonable and correct not only has a direct impact on the workload, cycle length, cost and assembly working conditions of the frame itself, but also It determines whether the docking and mating dimensions of each workpiece can be coordinated, whether the frame can maintain its dimensional stability in long-term use, and has a great impact on the interchange coordination, manufacturing quality and progress of aircraft assembly. Assembling often needs to be lifted and erected, the existing equipment is inconvenient to control, and at the same time affects the combined processing

Method used

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  • A new type of assembly frame for aircraft
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Embodiment Construction

[0013] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0014] see Figure 1-2 , the present invention provides a kind of technical scheme: a kind of new-style assembly frame for aircraft, comprises base 1, and control switch 2 is installed on the front side of base 1, and the input end of control switch 2 is electrically connected with the output end of external power supply, and base 1 Walking wheels 3 are installed on the four corners of the lower surface, and the left and right ends of the upper surface of the ...

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Abstract

The invention discloses a novel assembly frame for aircraft, which includes a base, a control switch is installed on the front side of the base, the input end of the control switch is electrically connected with the output end of an external power supply, and the four corners of the lower surface of the base Walking wheels are installed on the wheel frame. This new type of assembly frame for aircraft has simple structure and is easy to use. It is equipped with walking wheels to facilitate the overall movement. The overturning and docking of the two worktables facilitates the assembly of parts. The support plate, the left end seat and the right end seat can be moved as a whole, which can realize the turning of the parts and finally reach the vertical state. The right end seat is supported by the supporting studs. The left end seat is clamped by the inserting plate and locking stud, which has strong stability and is not easy to slide. At the same time, the supporting stud, inserting plate and locking stud can be disassembled without affecting the assembly of the two matching parts.

Description

technical field [0001] The invention relates to the technical field of aircraft production auxiliary equipment, in particular to a novel assembly frame for aircraft. Background technique [0002] The number of assembly frames used in aircraft manufacturing is large, so whether the structure design of the assembly frame is reasonable and correct not only has a direct impact on the workload, cycle length, cost and assembly working conditions of the frame itself, but also It determines whether the docking and mating dimensions of each workpiece can be coordinated, whether the frame can maintain its dimensional stability in long-term use, and has a great impact on the interchange coordination, manufacturing quality and progress of aircraft assembly. Assembling often needs to be lifted and erected, the existing equipment is inconvenient to control, and at the same time affects the combined processing. Contents of the invention [0003] The technical problem to be solved by the...

Claims

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Application Information

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Patent Type & AuthorityPatents(China)
IPC IPC(8): B64F5/10
CPCB64F5/10
Inventor项磊
OwnerGUANGDONG KNOWLEDGE CITY OPERATION SERVICES CO LTD