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an intake box

An air intake casing, integrated technology, applied in the air inlet of the turbine/propulsion unit, engine components, combustion air/combustion-air treatment, etc., can solve the sharp edge cracks of anti-icing holes, welding deformation and large residual stress , blade staggered deflection and other problems, to achieve the effect of eliminating the problem of weld cracks

Active Publication Date: 2021-11-19
AECC SHENYANG ENGINE RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] First of all, the hollow rectifying blade assembly processed by superplastic forming / diffusion bonding process using four-layer titanium alloy plate has welding problems such as poor welding rate and triangular area between layers due to the limitation of forming process. Some non-destructive testing methods cannot effectively check for welding defects, resulting in problems such as bulges and cracks in the triangular area and the rear end surface of the blade.
[0007] Secondly, at present, the anti-icing holes on the rectifier blades are electro-machined. Due to the limitation of the structure and molding process, manual polishing is required to remove the re-melted layer on the electro-machined surface. Due to the limitation of the operator's technical level and stability, the re-melted layer will appear thick Uneven phenomenon, and the excessive thickness of the remelted layer will bring about hidden dangers of cracks
At the same time, due to the limitation of the molding process, it is impossible to round the edge of the anti-icing hole in the inner cavity of the support plate, and there is a phenomenon of stress concentration at the edge of the hole
Under the influence of the above two factors, the fixed support plate is prone to cracks at the sharp edge of the anti-icing hole under various loads
[0008] Thirdly, the front part of the inner ring of the air intake case and the support head of the outer ring are all made of castings. Due to the current domestic casting level, the geometric dimensions and geometric tolerance accuracy of the castings often cannot meet the assembly and welding requirements of the components.
Airfoil misalignment and deflection, airfoil thickness out of tolerance, and wall thickness out of tolerance will lead to serious misalignment after welding, poor welding consistency, large welding deformation and residual stress, and subsequent defect repair welding further increases welding deformation and residual stress Level
At the same time, defects such as loose structure and trachoma of the casting reduce the load-carrying capacity of the entire casing. Crack

Method used

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Embodiment Construction

[0029] In order to make the purpose, technical solution and advantages of the application more clear, the technical solution in the embodiment of the application will be described in more detail below in conjunction with the drawings in the embodiment of the application. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the application. The embodiments described below by referring to the figures are exemplary, and are intended to explain the present application, and should not be construed as limiting the present application. Based on the embodiments in this application, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of this application. Embodiments of the present application will be described in detail below in conjunction with th...

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Abstract

The present application discloses an air intake casing, comprising: a fixed strut plate welded by a first fixed strut plate and a second fixed strut plate, the structure of the first fixed strut plate and the second fixed strut plate is formed by rectifying blades The plane of the center line in the length direction is symmetrical to the left and right. The first fixed support plate and the second fixed support plate both include rectifying blades and support plate heads formed in one piece; The surface of the rectifying blade; the front section of the inner ring, which is welded on the end of the fixed support plate away from the support plate head; the case shell, which is welded to the support plate head. The air intake casing of this application can eliminate the problems of superplastic forming fixed support plate surface bulge, anti-icing hole crack, and welding triangle area; in addition, due to the integrated design of the fixed support plate and support plate head, the gap between The argon arc welding seam, thus fundamentally eliminating the weld crack problem here.

Description

technical field [0001] The application belongs to the field of aero-engine structural design, in particular to an air intake case. Background technique [0002] The intake casing of the small bypass ratio aero-engine is located at the front end of the engine, and is composed of a fairing assembly, an intake casing assembly assembly, etc. The casing is equipped with bearings to withstand the front fulcrum load and vibration load of the low-pressure rotor, etc. It is one of the main bearing frames of the engine. In order to prevent the front end parts of the engine from freezing in low temperature environment, the air intake case also needs to have anti-icing function. [0003] Commonly used structures for air intake casings include assembly structures and welded structures. Among them, welded air intake casings have a simple structure, do not need to be connected by fasteners, reduce assembly difficulty, have a smaller overall weight, and have higher processing efficiency. ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F02C7/04
CPCF02C7/04
Inventor 邵珠蕾杨治中段文龙王继业刘公博
Owner AECC SHENYANG ENGINE RES INST
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