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A method of manufacturing an aircraft spherical frame Y-shaped connector

A connector and frame technology, which is applied in the field of manufacturing aircraft spherical frame Y-shaped connectors, can solve problems such as the inability to break through localization, the difficulty of manufacturing Y-shaped connectors, and the high cost of Y-shaped connectors.

Active Publication Date: 2021-09-14
西安兴航航空科技股份有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Due to the larger size and thinner wall thickness of the Y-shaped connector, the rigidity of the Y-shaped connector is poor, making it easy to deform during the processing of the Y-shaped connector, which makes the manufacture of the Y-shaped connector more difficult.
[0003] Due to the difficulty in manufacturing the Y-shaped connectors, it has been unable to break through localization, and has been imported from abroad, which makes the cost of the Y-shaped connectors higher.

Method used

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  • A method of manufacturing an aircraft spherical frame Y-shaped connector
  • A method of manufacturing an aircraft spherical frame Y-shaped connector
  • A method of manufacturing an aircraft spherical frame Y-shaped connector

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Embodiment Construction

[0034] The technical solutions in the embodiments of the present invention will be described below with reference to the drawings in the embodiments of the present invention.

[0035] In order to realize the localization of the Y-shaped connector and thereby reduce the cost of the Y-shaped connector, an embodiment of the present invention provides a method for manufacturing the Y-shaped connector of an aircraft spherical frame.

[0036] It should be noted that the method for manufacturing the Y-shaped connector of the aircraft spherical frame provided by the embodiment of the present invention can be applied to the aircraft manufacturing industry.

[0037] Such as figure 1 As shown, the manufacturing method of the aircraft spherical frame Y-shaped connector provided by the embodiment of the present invention includes the following steps:

[0038] S101: Obtain a bar-shaped blank.

[0039] The above-mentioned rod-shaped blank can be, for example, a cylindrical blank with a dia...

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Abstract

An embodiment of the present invention provides a method for manufacturing an aircraft spherical frame Y-shaped connector. The method includes: obtaining a rod-shaped blank; The arc-shaped structure of the radian is used to obtain a blank; the blank is forged using a preset forging die to obtain a forged piece, wherein the forged piece can be divided into two identical pieces to be processed; The above-mentioned forgings are obtained to obtain two identical workpieces to be processed; the workpieces to be processed are machined to obtain Y-shaped connectors. Using the technical method provided by the embodiment of the present invention can realize the localization of the Y-shaped connector when manufacturing the connector, thereby reducing the cost of the Y-shaped connector.

Description

technical field [0001] The invention relates to the technical field of aircraft manufacturing, in particular to a method for manufacturing an aircraft spherical frame Y-shaped connector. Background technique [0002] The Y-shaped connector of the aircraft spherical frame is usually in the shape of a semi-circular arc with a large outer diameter. For example, the Y-shaped connector of the spherical frame of the C919 aircraft is a one-third arc of the outer diameter of Φ2852mm. Because the size of the Y-shaped connector is large and the wall thickness is thin, the rigidity of the Y-shaped connector is poor, which makes the Y-shaped connector easily deformed during processing, thus making it difficult to manufacture the Y-shaped connector. [0003] Due to the difficulty of manufacturing the Y-shaped connectors, it has been unable to break through localization, and has been imported from abroad, which makes the cost of the Y-shaped connectors relatively high. Contents of the i...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23P15/00
CPCB23P15/00
Inventor 范建校徐科王海忠
Owner 西安兴航航空科技股份有限公司