A processing method of a welded structure fuel manifold with a nozzle

A fuel oil main pipe and welding structure technology, which is applied in welding equipment, metal processing equipment, manufacturing tools, etc., can solve problems such as fracture failure, large residual stress, and out-of-tolerance nozzle housing position, and achieve improved welding deformation and stable quality , Dimensional accuracy qualified effect

Active Publication Date: 2016-01-13
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Application Information

AI Technical Summary

Problems solved by technology

Due to the small diameter D caused by welding deformation, the position of the nozzle housing is out of tolerance and the large residual stress, there have been fracture failures during the engine test run

Method used

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  • A processing method of a welded structure fuel manifold with a nozzle
  • A processing method of a welded structure fuel manifold with a nozzle
  • A processing method of a welded structure fuel manifold with a nozzle

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Embodiment Construction

[0023] The present invention is specifically described below in conjunction with accompanying drawing, as Figure 1-1 to Figure 6 As shown, the part consists of 15 nozzle housings 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15 (6 of which have mounting pins, respectively It is 2, 5, 8, 9, 12, 15) and Φ8 and Φ15 pipes are welded by argon arc welding, and there are also main and auxiliary oil inlet pipes welded at the same time, with as many as 65 welds. The drawing of the main pipe requires that the position degree of 15 nozzle shells and 6 mounting pins is not greater than 0.5. The process route in the early stage of development adopts the nozzle shell and the pipe to be assembled and welded into the main pipe ring at one time, and six installation pins are bored after heat treatment and correction. Due to the small diameter D caused by welding deformation, the position of the nozzle housing is out of tolerance and the large residual stress, fracture failures occurred duri...

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Abstract

The invention discloses a method for machining a fuel manifold with nozzles and of a welding structure. The method includes the welding step, the thermal treatment step and the boring step. Assembly and positioned welding are conducted on each nozzle shell and each pipe at the position, located on the middle arc increasing position, of a small-section welding clamp, and 15 sets of welded nozzle assemblies are formed and corrected at the position; assembly and positioned welding are conducted on every two sets of nozzle assemblies at the middle arc increasing position of the welding clamp according to the general drawing position, and the welded nozzle assemblies are corrected on the original welding clamp; in the process of forming half rings of the manifold, assembly and positioned welding are conducted on each welding seam at the middle arc increasing position of the welding clamp, and the welded welding seams are corrected on the original welding clamp; eventually positioned welding is conducted on the two half rings on the original welding clamp, and the two welded half rings are corrected. The method has the advantages that the welding deformation phenomenon is obviously improved, size accuracy is qualified, the method smoothly passes long test evaluation, the quality is stable, and no fracture failure in the engine test process occurs.

Description

technical field [0001] The invention relates to the field of welding, in particular to a method for processing a welded structure fuel main pipe with a nozzle. Background technique [0002] The working fuel main pipe of an aero-engine is mainly an annular welded structure composed of a nozzle shell and a pipe, as shown in Figure 1. The part consists of 15 nozzle housings 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15 (6 of which have mounting pins, respectively 2, 5, 8, 9, 12, 15) and Φ8 and Φ15 pipes are welded by argon arc welding, and the main and auxiliary oil inlet pipes are welded at the same time, with as many as 65 welds. The drawing of the main pipe requires that the position degree of 15 nozzle shells and 6 mounting pins is not greater than 0.5. The process route in the early stage of development adopts the nozzle shell and the pipe to be assembled and welded into the main pipe ring at one time, and six installation pins are bored after heat treatment and corr...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23P15/00B23K9/167
CPCB23P15/00B25B11/00
Inventor 周勇杨踊杨涧石张炳海刘晓娟
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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