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Deep repairing method for turboprop airplane propeller hub sealing face

A sealing surface and propeller technology, applied in the aerospace field, can solve the problems of long repair cycle, high cost, inconvenience to domestic customers, etc., and achieve the effect of reducing maintenance cost, easy operation, and restoring mechanical properties and material properties.

Active Publication Date: 2018-04-03
WUHAN HANGDA AERO SCI & TECH DEV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The CMM (Component Maintenance Manual) manual stipulates that the repair should be returned to the foreign original equipment manufacturer (OEM for short). The above-mentioned existing repair method has a long repair cycle and high cost, which has caused great inconvenience to domestic customers.

Method used

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  • Deep repairing method for turboprop airplane propeller hub sealing face
  • Deep repairing method for turboprop airplane propeller hub sealing face
  • Deep repairing method for turboprop airplane propeller hub sealing face

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Embodiment Construction

[0020] The implementation of the present invention will be described in detail below in conjunction with the accompanying drawings, but they do not constitute a limitation to the present invention, and are only examples. At the same time, the advantages of the present invention are clearer and easier to understand through the description.

[0021] Referring to the accompanying drawings, it can be seen that the method for repairing the depth of the sealing surface of the turboprop propeller hub is characterized in that it comprises the following process steps:

[0022] Step 1: According to the standard of American Society for Testing and Materials (ASTM E1444), conduct magnetic particle inspection on the damaged area of ​​the propeller hub sealing surface;

[0023] Step 2: According to the standard (BAC) of Boeing Company of the United States, thermal damage inspection is carried out on the damaged area of ​​the hub sealing surface of the propeller, and the thermal damage readi...

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Abstract

The invention discloses a deep repairing method for a turboprop airplane propeller hub sealing face, and relates to a repairing method for an airplane propeller. The method comprises the steps that the damaged area of the propeller hub sealing face of the propeller is subjected to magnetic powder inspection and thermal damage examination to be removed, the damage removed area on the propeller hubsealing face is subjected to hypersonic flame spraying, a high-precision five-axis coordinate grinding machine is used for grinding the thermal spraying area, and a self-made special clamp is adoptedfor completing accurate positioning of a propeller hub before grinding machining; the propeller hub face machined by the grinding machine is subjected to magnetic powder inspection to be ensured of being free of cracks, the propeller hub face machined by the grinding machine is subjected to Barkhausen thermal damage examination to ensure that no grinding thermal damage is produced in the thermal spraying area, and a reassembled hub assembly is subjected to temperature tolerance testing and leakage testing. The technical monopoly of OEM (original equipment manufacturer) is broken through, the technical barrier is broken through, and the core technology is grasped.

Description

technical field [0001] The invention belongs to the technical field of aerospace and relates to a method for repairing an aircraft propeller, more specifically, a method for repairing the depth of the hub sealing surface of a propeller of a turboprop aircraft. Background technique [0002] The propeller used by the Xinzhou 60 aircraft (English: Modern Ark 60, English abbreviation MA60) manufactured by Xi'an Aircraft Industry (Group) Co., Ltd. is a four-blade variable-pitch propeller made by the American Hamilton company (see figure 1 ). Among them, the propeller hub is forged from high-strength alloy steel, and there is a variable pitch actuator driven by lubricating oil inside the propeller hub. [0003] Under the action of the control system, the variable pitch actuator can adjust the pitch angle of the blades within a certain range, so that the propeller and the engine can be kept running at high efficiency. At the same time, when the aircraft is in the landing braking ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): C23C4/129C23C4/02C23C4/06C23C4/08
Inventor 宋彦军刘剑辉
Owner WUHAN HANGDA AERO SCI & TECH DEV
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