Electron beam welding and superplastic forming process for wing and rudder parts

A technology of electron beam welding and superplastic forming, which is applied in the direction of electron beam welding equipment, welding equipment, non-electric welding equipment, etc., can solve the problem that the quality of the diffusion connection of the core layer is difficult to guarantee, the air flow of the middle core layer is not smooth, and the surface of the part is affected Quality and other issues, to achieve the effect of avoiding solder resist coating work, high cell size accuracy, and reducing the risk of air leakage

Active Publication Date: 2018-06-15
BEIJING XINGHANG MECHANICAL ELECTRICAL EQUIP
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  • Abstract
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Problems solved by technology

[0003] As the size of the parts increases, the number of forming air paths increases, and the intake and exhaust increase, and the superplastic forming / diffusion connection process also exposes deficiencies: (1) There are many air paths that are prone to blockage, air leakage, and cross-gas. The middle core layer The airway is easy to be poorly ventilated
(2) The quality of the diffusion connection of the core layer is difficult to guarantee, and the core layer is also prone to offset
(3) Superplastic forming / diffusion connection is easy to produce grooves on the surface of parts, which affects the surface quality of parts
(4) The entire forming cycle is relatively long, the time is about 6-8 hours, and the performance of the board is easy to decline

Method used

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  • Electron beam welding and superplastic forming process for wing and rudder parts
  • Electron beam welding and superplastic forming process for wing and rudder parts
  • Electron beam welding and superplastic forming process for wing and rudder parts

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Embodiment Construction

[0033] In order to make the purpose, content, and advantages of the present invention clearer, the specific implementation manners of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

[0034] refer to figure 1 , the wing and rudder parts proposed by the present invention adopt electron beam welding superplastic forming process as follows:

[0035] (1) Cutting the upper core layer 2, the lower core layer 3, the upper skin 1, and the lower skin 4 according to the drawings;

[0036] (2) Add ventilation grooves to the upper core layer 2 and lower core layer 3, and carry out pickling, and carry out electron beam penetration welding on the plates of the upper core layer 2 and lower core layer 3 according to the size distribution of the internal core cells of the wing and rudder parts ;

[0037] (3) manual argon arc welding on the periphery of the upper core layer 2 and the lower core layer 3 (that is, th...

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Abstract

The invention relates to the technical field of superplastic forming, in particular to an electron beam welding and superplastic forming process for wing and rudder parts. The electron beam welding and superplastic forming process for the wing and rudder parts can achieve electron beam welding and superplastic compound integrated formation of hollow intensive core grid wind and rudder parts, corelayers are subjected to electron beam keyhole-mode welding instead of diffusion bonding, and accordingly the quality problem of diffusion bonding of the core layers is solved; the number of gas circuits is decreased, and the risk that the gas circuits are blocked or leak air is reduced; the complicated work of solder mask coating is avoided, the core grid dimension precision is higher, and the part forming quality is improved; and compared with superplastic forming and diffusion bonding, the forming time is shortened, the forming efficiency is improved, and the forming qualified rate is increased.

Description

technical field [0001] The invention relates to the technical field of time-frequency measurement, in particular to an electron beam welding superplastic forming process for wing and rudder parts. Background technique [0002] Aircraft wing and rudder parts are often manufactured using superplastic forming / diffusion connection technology, which can manufacture hollow dense core parts and realize lightweight and integrated wing and rudder parts. The process flow is: rationally design the size of the blank skin and core plate according to the parts, and carry out precise blanking, and pickling treatment after the core plate is milled with ventilation grooves. Apply solder resist according to the internal structure of the part, seal and weld the prepared four-layer sheet (core board / skin), put it into the mold and heat it up. After the temperature reaches the set forming temperature, run the program according to the set process parameters, and load the air pressure through the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23K15/00B23K20/00B23K20/02B23K28/02
CPCB23K15/0046B23K20/002B23K20/023B23K28/02
Inventor 赵红凯刘太盈朱冬妹沈华胡晓勇
Owner BEIJING XINGHANG MECHANICAL ELECTRICAL EQUIP
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