A method for controlling grinding deformation of helicopter center pull rod
A central tie rod and helicopter technology, which is applied to the parts of grinding machine tools, machine tools designed for grinding the rotating surface of workpieces, grinding drive devices, etc., can solve the problems of low processing efficiency, product processing out-of-tolerance, and increased preparation time , to achieve the effect of improving machining accuracy and controlling deformation problems
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Publication Date
- 2022-07-08
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Figure 1
Abstract
Description
technical field
[0001] The invention relates to a method for grinding the outer diameter of slender shaft parts, in particular to a method for grinding the outer diameter of a central tie rod of a helicopter. Background technique
[0002] The central tie rod is an important part of the hot end part of the helicopter engine. It belongs to the type of slender shaft, which will be bent and deformed by the influence of processing resistance and self-excited vibration during the processing process. For the components on the helicopter, its technological requirements will be higher. In the past, for the processing of slender shafts, one or more center brackets were used to add auxiliary supports to the parts to reduce the processing deformation of the parts and ensure the technical requirements. There are certain drawbacks in using the center bracket to process products: 1. When using the center bracket to process the slender shaft, every time 0.03mm of allowance is removed from ...
Examples
Embodiment Construction
[0020] specific implementation
[0021] The invention provides a method for controlling the grinding deformation of a central tie rod of a helicopter. The parts are subjected to solid solution aging after blanking to improve the cutting performance of the material, then the parts are roughed and ultrasonically inspected to check whether the parts have machining defects, and finally the parts are semi-finished. When turning the shape, leave a margin of 0.15mm for each outer shaft diameter and enter the grinding process.
[0022] The first step in the grinding process is to configure a small taper mandrel for part grinding, and the taper of the mandrel is 1:2000. In order to ensure that the pressure is not too concentrated at one point when the mandrel is assembled with the inner hole of the part, the assembly deformation of the part occurs. When assembling the mandrel and the part, ensure that the mandrel is manually rotated and pushed into the inner hole of the part, and the ...