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Fixture mechanism for creep feed grinding of tenon teeth of turbine blade

A turbine blade and slow-feed grinding technology, which is applied to gear teeth, gear cutting machines, and components with teeth, etc., can solve the problems of weak compression, inaccurate positioning, and difficult positioning and clamping of fixtures, etc., and achieve a reasonable overall structure Reliable, increased rigidity, and convenient clamping effect

Pending Publication Date: 2021-03-16
SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Due to the difficulty in positioning and clamping the fixture during the slow-feed grinding tenon teeth processing, it is very difficult to realize the structure. However, the traditional structure has the problems of inaccurate positioning, weak compression, and difficult installation and alignment.

Method used

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  • Fixture mechanism for creep feed grinding of tenon teeth of turbine blade
  • Fixture mechanism for creep feed grinding of tenon teeth of turbine blade
  • Fixture mechanism for creep feed grinding of tenon teeth of turbine blade

Examples

Experimental program
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Embodiment Construction

[0034] Such as Figure 1-4 Shown is a fixture mechanism for slowly grinding tenons of turbine blades, including a main body 1, a support block 2, a cover plate 3, a pressure rod 4, a front pressure head 5, a rear pressure head 6, a side positioning seat 7, and a blade body positioning block 8. Tail positioning seat 9, craft ball pin 10, pressure rod body 11, front pressure rod 12, rear pressure rod 13, side pressure head 14, tail pressure head 15, tail block 16, pin shaft 17, right deflector 18, Left deflector 19, side positioning block 20, shaft positioning pin 21, compression spring 29, compression screw 37;

[0035] The support block 2, the blade body positioning block 8, the side positioning block 20, and the shaft positioning pin 21 are all positioning points, which are fixed on the main body 1, and are used to realize the position positioning of the bottom surface, the side surface and the axial direction of the blade;

[0036] The main body 1 is provided with two bosse...

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Abstract

The invention discloses a fixture mechanism for creep feed grinding of tenon teeth of a turbine blade. According to the fixture mechanism, a supporting block, a blade body locating block, a side locating block and an axial locating pin are all locating points, are fixed to a main body and are used for locating the bottom face, the side face and the axial direction of the blade; a pressing rod is connected to a cover plate through a pin shaft; a front pressing head and a rear pressing head are connected to the two ends of the pressing rod through pin shafts; the cover plate, the pressing rod, the front pressing head and the rear pressing head form a whole and are arranged on the main body; a front pressing rod and a rear pressing rod are connected with a pressing rod body through pin shafts; a side pressing head is connected with the front pressing rod, a tail pressing head is connected with the rear pressing rod, and a side pressing plate assembly of a lever structure is formed; a leftguide plate and a right guide plate are fixed into grooves in the front ends of two bosses of the main body respectively; and a rapid locating clamping groove is formed in the bottom end of the mainbody and is used for being connected with a machining tool. The tool achieves a very good effect through on-site application. The fixture structure has the advantages of clamping convenience, accuracyand stability, thereby having important significance in optimizing and improving a process route.

Description

technical field [0001] The invention relates to the technical field of disassembly of disc parts, in particular to a fixture mechanism for slow-feeding grinding teeth of turbine blades. Background technique [0002] In the manufacturing process of aero-engine turbine blades, due to the complex profile, small shape and low processing pass rate, it has always been a difficult problem in engine manufacturing technology. As the first manufacturing process, tenon tooth processing is particularly important and difficult. It must be processed by a stable and reliable special fixture. The quality of the fixture structure directly affects the subsequent manufacturing process and pass rate of the entire blade. Due to the difficulty in positioning and clamping the fixture during the slow-feed grinding tenon teeth processing, it is very difficult to realize the structure. However, the traditional structure has the problems of inaccurate positioning, weak compression, and difficult insta...

Claims

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Application Information

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IPC IPC(8): B23F23/06B24B41/06
CPCB23F23/06B24B41/06
Inventor 赵西松姚红梅李硕赵海翔阚敏
Owner SHENYANG LIMING AERO-ENGINE GROUP CORPORATION
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