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Repairing method for loosening of bearing of tail transmission shaft of helicopter

A tail drive shaft and repair method technology, applied to aircraft parts, transportation and packaging, etc., can solve the problems of no repair method, large vibration of the tail shaft, waste, etc., achieve good working conditions and ensure the effect of environmental adaptability

Active Publication Date: 2018-11-23
HARBIN DONGAN ENGINE GRP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

At the same time, the tail shaft is composed of multiple sections of aluminum tubes, and the aluminum tubes are connected by riveting, so the bearings on the tail shaft cannot be disassembled
Due to the influence of working conditions, when the tail shaft starts to work, the bearings often loosen
After the bearing is loose, if it is not repaired in time, it will cause a large vibration of the tail shaft and accelerate the wear of the tail shaft, which will affect the safety of the whole machine in severe cases
Since the bearing on the tail shaft cannot be disassembled, and there is no feasible repair method in the early stage, when the tail shaft bearing becomes loose, the entire tail shaft is forced to be scrapped, causing a lot of waste

Method used

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Examples

Experimental program
Comparison scheme
Effect test

Embodiment

[0032] The bearing in the middle section of the tail shaft of a certain type of helicopter is loose, and the repair steps are as follows:

[0033] (1) Confirm the type of bearing looseness, and the bearing cannot move axially;

[0034] (2) Use a paint remover to remove the paint layer on the end of the bearing on the tail shaft, remove the bearing, and carefully clean the position where the bearing is installed;

[0035] (3) Measure the shaft diameter of the fitting part of the inner ring of the bearing, the shaft diameter is greater than the wear limit size;

[0036] (4) Clean the bearing installation position and the inner ring of the bearing with acetone, and there will be no impurities after cleaning;

[0037] (5) Apply loctite638 glue to the bearing installation position on the tail shaft, and the glue is evenly distributed;

[0038] (6) Adjust the bearing to the original machine position, and apply loctite638 glue on one end of the bearing, the glue has soaked into t...

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PUM

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Abstract

The invention relates to a repairing method for loosening of a bearing of a tail transmission shaft of a helicopter. A bearing loosening and wear repairing standard is offered, curing methods such asa normal temperature method are adopted, damaged paint layers in the bearing repairing process are repaired, and the repaired tail shaft can continue to be put into use. The repairing method is put into use for many years in removing loosening faults of bearings of tail shafts of helicopters with a certain model, the repaired bearings of the tail shaft has a good working state in an external field, and bearing loosening problems are not fed back anymore.

Description

technical field [0001] The invention relates to a repair method for a loose bearing, in particular to a repair method for a loose bearing of a tail drive shaft of a helicopter. Background technique [0002] A bearing is installed on the tail shaft of the helicopter, the inner ring of the bearing cooperates with the tail shaft tube, and the outer ring of the bearing cooperates with the damping rubber bushing to eliminate the vibration of the tail shaft during operation. The two ends of the tail shaft are flange structures, and the maximum outer diameter of the flange is larger than the inner ring of the bearing. Therefore, when installing the tail shaft, the bearing must be installed first, and then the flange. At the same time, the tail shaft is composed of multiple sections of aluminum tubes, and the aluminum tubes are connected by riveting, so the bearings on the tail shaft cannot be disassembled. Due to the influence of working conditions, when the tail shaft starts to w...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B23P6/00
CPCB23P6/00B23P2700/01
Inventor 欧阳可平王银凤冯磊李远那国雨许鹏
Owner HARBIN DONGAN ENGINE GRP
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