Method for repairing micro-arc oxide film oil leakage at seal groove of cylinder body of actuator cylinder of airplane

A technology of micro-arc oxidation and sealing groove, which is applied to aircraft parts, ground devices, grinding machines, etc., can solve the problems of frequent oil leakage failures on the joint surface of the cylinder and the piston, and the aging of the micro-arc oxidation layer is particularly serious, and achieves a solution to the cylinder Oil leakage at the body seal groove, saving money, and great application prospects

Active Publication Date: 2016-08-17
SHENYANG LIMING AERO PARTS MFG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, with the prolongation of the service time of the aircraft, the micro-arc oxidation layer of the actuating cylinder components is gradually aging, especially the aging of the micro-arc oxidation layer at the seal groove of the actuating cylinder cylinder is particularly serious, which makes the leakage of the joint surface between the cylinder body and the piston Oil faults occur frequently, and serious safety problems will occur if they are not dealt with in time. In most cases, the only remedy is to replace the actuator assembly. There is no more convenient and economical method at present

Method used

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  • Method for repairing micro-arc oxide film oil leakage at seal groove of cylinder body of actuator cylinder of airplane
  • Method for repairing micro-arc oxide film oil leakage at seal groove of cylinder body of actuator cylinder of airplane
  • Method for repairing micro-arc oxide film oil leakage at seal groove of cylinder body of actuator cylinder of airplane

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Experimental program
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Effect test

Embodiment 1

[0025] The method of repairing the oil leakage of the micro-arc oxidation film layer at the bottom of the sealing groove of the cylinder body of the aircraft actuator is carried out according to the following steps:

[0026] (1) Disassemble the cylinder body of the aircraft cylinder assembly that has oil leakage failure at the bottom of the seal groove of the cylinder cylinder body, and clean it with gasoline;

[0027] (2) Measure the surface roughness of the micro-arc oxidation film layer at the bottom of the cylinder sealing groove to be 2.83;

[0028] (3) Using an electron microscope to observe the microscopic cross-sectional morphology of the micro-arc oxidation film layer at the bottom of the sealing groove of the cylinder body, it is found that the micro-arc oxidation film layer produces a loose layer, and the cross-sectional morphology of the micro-arc oxidation film layer is as follows figure 1 As shown, the thickness of the oxide film is 74.92 μm, the thickness of the...

Embodiment 2

[0042] The method of repairing the oil leakage of the micro-arc oxidation film layer on the side of the sealing groove of the cylinder body of the aircraft actuator is carried out according to the following steps:

[0043] (1) Disassemble the cylinder body of the aircraft cylinder assembly that has oil leakage failure at the side of the seal groove of the cylinder cylinder body, and clean it with gasoline;

[0044] (2) Measure the surface roughness of the micro-arc oxidation film layer on the side of the sealing groove of the cylinder to be 2.47;

[0045] (3) Using an electron microscope and an energy spectrometer to measure whether a loose layer is produced on the micro-arc oxidation film layer on the side of the cylinder sealing groove, the result is a loose layer, in which the thickness of the oxide film is 75.34 μm, the thickness of the loose layer is 30.89 μm, and the thickness of the dense layer is 44.45 μm, the loose layer accounts for 41.00% of the total thickness; Tab...

Embodiment 3

[0059] The method of repairing the oil leakage of the micro-arc oxidation film layer on the side of the sealing groove of the cylinder body of the aircraft actuator is carried out according to the following steps:

[0060] (1) Disassemble the cylinder body of the aircraft cylinder assembly that has oil leakage failure at the side of the seal groove of the cylinder cylinder body, and clean it with gasoline;

[0061] (2) Measure the surface roughness of the micro-arc oxidation film layer on the side of the sealing groove of the cylinder to be 2.53;

[0062] (3) Using an electron microscope and an energy spectrometer to measure whether a loose layer is produced on the micro-arc oxidation film layer on the side of the cylinder sealing groove, the result is a loose layer, in which the thickness of the oxide film is 73.77 μm, the thickness of the loose layer is 28.89 μm, and the thickness of the dense layer is 44.88 μm, the loose layer accounts for 39.16% of the total thickness; Tab...

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Abstract

The invention discloses a method for repairing micro-arc oxide film oil leakage at a seal groove of a cylinder body of an actuator cylinder of an airplane. The method comprises the followings steps: disassembling the cylinder body of the actuator cylinder assembly of the airplane; measuring the surface roughness of the micro-arc oxide film at the seal groove of the cylinder body, if the surface roughness reaches Ra 1.6 or above, detecting whether a loose layer is generated on the micro-arc oxide film at the seal groove of the cylinder body or not, and if the loose layer is generated, conducting reparation: (1) wrapping the cylinder body with a layer of soft cloth, and clamping the cylinder body on a three jaw chuck of an electric polishing machine; (2) adsorbing a gauge head and a gauge stand of a dial indicator on the other side of the electric polishing machine, rotating the cylinder body, and keeping the jerk value of the seal groove of the cylinder body to be not more than 0.05; (3) enabling a felt wheel to extend into the seal groove of the cylinder body, adjusting the rotating speed of the felt wheel, and polishing the micro-arc oxide film at the seal groove; (4) measuring the size and the roughness of the polished seal groove of the cylinder body; (5) assembling the polished qualified cylinder body on the actuator cylinder assembly, and conducting seal test detection according to the product design requirements.

Description

technical field [0001] The invention belongs to the technical field of aero-engine manufacturing, and in particular relates to a method for repairing oil seepage in a micro-arc oxidation film layer at a seal groove of an aircraft actuator cylinder. Background technique [0002] The aircraft actuator assembly is a driving device that controls the movement of various control surfaces or other components on the aircraft. For example, the flap actuator is the driving actuator for the flap action. Flying direction; the aileron action cylinder is to operate the aileron to move up and down. These cylinder components themselves have a certain pressure, and the driving process is similar to the spring principle. They are generally made of aluminum alloy and are mainly composed of cylinders, pistons, rear covers and other components. In order to meet the performance of the aircraft actuator assembly in the marine air environment, the inner and outer surfaces of all components of the ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/00B24B27/033
CPCB24B27/033
Inventor 张向东郭红杨景伟纪成龙薛庆增陈玲玲王继业
Owner SHENYANG LIMING AERO PARTS MFG
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