Device and method for positioning overall frame of airplane

A technology of positioning device and integral frame, applied in aircraft assembly and other directions, can solve the problems of inability to meet the needs of production line assembly, inaccurate positioning of the frame body, and reduce production efficiency, and achieve the effect of improving assembly quality, simplifying structure, and improving assembly efficiency.

Inactive Publication Date: 2021-07-13
SHAANXI AIRCRAFT CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Due to the large number of parts and scattered positions, the assembly period occupied by them in the rack is long, which reduces the production efficiency; the scattered positioning of each frame also leads to inaccurate positioning of the entire frame, and the product is not easy to remove from the shelf after assembly
With the increasing demand for aircraft production batches, this method has become less and less able to meet the needs of production line assembly

Method used

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  • Device and method for positioning overall frame of airplane
  • Device and method for positioning overall frame of airplane
  • Device and method for positioning overall frame of airplane

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Experimental program
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Effect test

Embodiment Construction

[0021] DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0022] Such as figure 1 As shown; the proposed aircraft integral frame positioning device, the device includes a slide 2, a refining bolt 3, a nut 5, a compression nut 7, a flange 8, a slide pin 1; wherein the slide 2 is purified by The bolt 3 and the nut 5 are connected to the mounting base 4, and then the slide 1 passes through the slide 2, and then the flange 8 is threaded over and the slip pin 1 is connected, and finally the special pressing nut 7 is pressed into the overall frame 6, Make the overall box to close the flange 8, in order to achieve self-locking between the slide 2 and the slide pin, the slider 2 end is provided with a circular arc-shaped boss, and a card slot is opened on the boss; There is a ring boss on the pin 1. There is a slit on the annular boss, and the cutting shape is approximately an outer shape, and the slide pin is rotated. When the annular boss is screwed into the card slot of the slide 1, t...

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PUM

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Abstract

The invention belongs to the technical field of aircraft assembly, and particularly relates to a device and method for positioning an overall frame of an airplane. The positioning device comprises a sliding sleeve, a refined bolt, a nut, a compression nut, a flange plate and a sliding pin; the sliding sleeve is of a lug-shaped structure, mounting holes are formed in the two ends of a lug, and the sliding sleeve is fixed to the mounting base body in cooperation with refined bolts and nuts. The axis of the sliding sleeve is of a sleeve type structure, a semi-arc boss is arranged at the end of the axis, and a clamping groove is formed in the boss. The sliding pin is a step shaft, and shaft sections with the smallest diameter and the second smallest diameter are provided with threads and are matched with the compression nut and the flange plate respectively. An annular boss is arranged on the shaft section, with the maximum diameter, of the pin shaft, and a notch is formed in the annular boss. The sliding pin is rotated, so that the annular boss is matched with the clamping groove in the sliding sleeve, and locking and disengaging of the sliding pin are achieved. The device can be used for effectively positioning and assembling the whole frame of the airplane, and the purposes of simple manufacturing, convenient use and accurate positioning are achieved. And meanwhile, the in-rack occupation time is reduced, and the assembly efficiency is improved.

Description

Technical field [0001] The present invention belongs to the field of aircraft assembly, and more particularly to devices and methods for the overall frame positioning of aircraft. Background technique [0002] For a long time, the plane is assembled in the form of a displacement. The method is: First, in the frame (or web) in the frame (or web), follow the box on the box and the frame (or web) and the aircraft's space geometric dimension, order to complete the assembly . Since the number of dispersions is large, the position is dispersed, resulting in a long time to take advantage of the assembly period, which reduces production efficiency; the dispersion positioning of each frame also leads to inaccurate the positioning of the entire frame, and the product is not easy to remove after assembly. With the increase in bulk demand for airplane production, this method has become more and more unable to meet the production line demand. [0003] In view of such a situation, it is necess...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/10
CPCB64F5/10
Inventor 贾世川韩波陈珂邹秋芽韩志斌王波汤建军关红左铁强张伟庆
Owner SHAANXI AIRCRAFT CORPORATION
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