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Grinding tool and grinding method for guide pipe orifice angle

A technology for grinding tools and nozzles, which is applied in the manufacturing field of aircraft catheters. It can solve the problems of low efficiency of catheter nozzle angle grinding, unstable grinding angle size, and non-durability, so as to achieve stable and reliable grinding quality, shorten the grinding cycle, The effect of easy operation

Pending Publication Date: 2018-05-25
XIAN AIRCRAFT IND GROUP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In order to solve the defects of low grinding efficiency, non-durability, low precision, unstable grinding angle size, and deflection of the existing catheter nozzle angle, the purpose of this application is to provide a catheter nozzle with reliable grinding, high precision and high finish Angle Grinding Tools and Grinding Methods

Method used

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  • Grinding tool and grinding method for guide pipe orifice angle
  • Grinding tool and grinding method for guide pipe orifice angle
  • Grinding tool and grinding method for guide pipe orifice angle

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Embodiment Construction

[0014] see figure 1 , a conduit nozzle angle grinding tool, the grinding tool includes a grinding head 1, a guide rod 6, a compression spring 2 and a threaded guide sleeve 4, the grinding head 1 is located at the front end of the guide rod 6, and the grinding head 1 is a tapered The rigid structure of the grinding surface 9, the tapered grinding surface 9 matches the nozzle angle surface 8 of the conduit, the threaded guide sleeve 4 is a rotating body, the center of which has a guide hole and is embedded with a bearing 3, and its outer side is provided with External thread, the guide rod 6 is inserted into the guide hole, and the compression spring 2 is located between the grinding head 1, the guide rod 6 and the bearing 3.

[0015] The above-mentioned grinding head 1 is divided into a rough grinding head and a fine grinding head. In the rough grinding head, several grinding grooves are evenly distributed on the conical grinding surface 9. The rough grinding head is only used ...

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PUM

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Abstract

Provided are a grinding tool and a grinding method for a guide pipe orifice angle. The grinding tool comprises a grinding head, a guide rod, a compaction spring and a thread guide sleeve. The grindinghead is located at the front end of the guide rod, the grinding head is of a rigid structure with a tapered grinding surface, the angle of the tapered grinding surface is matched with the angle surface of an orifice of a guide pipe, the thread guide sleeve is a revolution body, a guide hole is formed in the center of the thread guide sleeve, a bearing is inlaid in the center of the thread guide sleeve, external threads are arranged on the outer side of the thread guide sleeve, the guide rod is inserted into the guide hole, and the compaction spring is located among the grinding head, the guide rod and the bearing. The thread guide sleeve of the grinding tool is connected with a cap nut of the orifice of a guide pipe part, the grinding head is pressed in the orifice of the guide pipe underthe action of the compaction spring, the grinding head is rotated through a handle at the tail of the guide rod to realize the purpose of rough grinding of the angle of the orifice of the grinded guide pipe.

Description

Technical field: [0001] The invention relates to the production and manufacturing technology of aircraft conduits, in particular to the processing and manufacturing of the nozzle angle of the conduit, especially the grinding of the nozzle angle which requires airtightness and high surface roughness when the nozzle is installed. Background technique [0002] There are thousands of conduits in aircraft parts, such as air pipes, oil pipes, etc., all over the aircraft. At present, angles are commonly used in the assembly of aircraft pipelines at home and abroad, such as 74°, 45°, etc. The advantages of this process are that the process of processing and installation is simple, and the cost is relatively low. The disadvantage is that the installation stress of the conduit Larger, prone to leakage. When assembling on the aircraft, the angle open end of the pipe is matched with the standard part joint, and the two ends of the standard part joint are opposite angles with the same a...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B24B37/04B24B37/11B24B41/047
CPCB24B37/04B24B37/11B24B41/047
Inventor 刘艳芳王伟高飞
Owner XIAN AIRCRAFT IND GROUP
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