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A rapid clamping and installation mechanism for aero-engine blades

An aero-engine and installation mechanism technology, applied in the field of workpiece processing, can solve problems such as affecting the efficiency of blade processing, and achieve the effect of improving work efficiency

Active Publication Date: 2022-02-01
BEIJING PROSPER PRECISION MACHINE TOOL CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In view of the above-mentioned related technologies, the inventor believes that each time the blade is installed on the workbench, it needs to be repeatedly calibrated, fixed and then processed, which has the disadvantage of affecting the efficiency of blade processing

Method used

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  • A rapid clamping and installation mechanism for aero-engine blades
  • A rapid clamping and installation mechanism for aero-engine blades
  • A rapid clamping and installation mechanism for aero-engine blades

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Embodiment Construction

[0037] The following is attached Figure 1-5 The application is described in further detail.

[0038] The embodiment of the present application discloses a fast clamping installation mechanism for an aeroengine blade.

[0039] refer to figure 1 and figure 2 , a fast clamping installation mechanism for an aeroengine blade includes two clamping parts 1 for fixing both ends of the blade and a mounting seat 2 for installing the clamping parts 1. The mounting seat 2 is located on a workbench, and the mounting seat 2 is provided with Two, the two installation bases 2 can move away from each other or approach each other, and can be fixed with the workbench by pressing. When the blade is processed on the workbench, the staff can calibrate and fix the two ends of the blade to be processed through the clamping part 1, and then drive the screw to rotate through the drive motor, so that one of the mounting seats 2 faces away from the other mounting seat 2 Move the blade and the two c...

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PUM

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Abstract

The application relates to a fast clamping and installation mechanism for aeroengine blades, which belongs to the field of workpiece processing, and includes clamping parts for clamping and fixing the two ends of the blades. The mounting seat of the holder, the side of the mounting seat away from the clamping part is provided with a motor, and one end of the output shaft of the motor is fixedly connected with the transmission shaft in the mounting seat, and a connection between the transmission shaft and the clamping part is provided. The connection shaft, the end of the connection shaft close to the motor is fixedly connected with the connection sleeve, the connection sleeve is set on the transmission shaft and is slidably connected with the transmission shaft, and the end of the connection shaft close to the clamp is provided with a clamping assembly for clamping with the clamp . The application can improve the working efficiency of blade production and processing.

Description

technical field [0001] The present application relates to the field of workpiece processing, in particular to an aeroengine blade quick clamping installation mechanism. Background technique [0002] At present, the blanks of aviation blades are all alloy castings, and the processing procedures are relatively complicated. From the drawing to the finished product, it generally takes 40-60 processes. At present, the processing of aviation blades is mostly processed by milling. [0003] The existing technology requires the staff to install the blade on the workbench when processing the blade of the aeroengine, and then perform repeated calibration and positioning, and then use the machine tool for processing, and then remove the blade after completion, install another blade and repeat the process. operate. [0004] With regard to the related technologies mentioned above, the inventor believes that each time the blade is installed on the workbench, it needs to be repeatedly cal...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B23Q3/06
CPCB23Q3/063
Inventor 吴行飞吕桂芳邓崛华邓光亚
Owner BEIJING PROSPER PRECISION MACHINE TOOL CO LTD