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Tenon connection structure design method for turbine rotor of long-service-life small turbofan engine

A technology of turbofan engine and connecting structure, applied in geometric CAD and other directions, can solve the problems of uneven stress distribution on the side and back of the blade basin, high risk of engine damage, low cycle fatigue damage, etc., to reduce the stress level and improve the bearing capacity. capacity, the effect of improving the bearing capacity of the structure

Pending Publication Date: 2020-02-04
BEIJING POWER MACHINERY INST
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AI Technical Summary

Problems solved by technology

[0004] The fillet at the root of the third pair of teeth and the fillet at the root of the tenon and groove ( image 3 ) under the superposition of the radial stress at the root of the wheel rim lug, the bending stress of the mortise teeth, and the circumferential stress of the rim, the stress level is relatively high, and low-cycle fatigue damage is prone to occur after long-term repeated use
[0005] Through analysis, it is concluded that the current turbine rotor adopts a three-pair tooth fir tree-shaped tenon connection structure, which has a high stress level at the key strength position, and the stress distribution on the side of the blade pot and the back side is uneven, and the risk of damage during the engine's working process is high.

Method used

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  • Tenon connection structure design method for turbine rotor of long-service-life small turbofan engine
  • Tenon connection structure design method for turbine rotor of long-service-life small turbofan engine
  • Tenon connection structure design method for turbine rotor of long-service-life small turbofan engine

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Embodiment Construction

[0024] In order to make the purpose, content, and advantages of the present invention clearer, the specific implementation manners of the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments.

[0025] A method for designing a tenon connection structure for a long-life small turbofan engine turbine rotor according to the present invention, the method includes the following steps:

[0026] The first step is to design the tenon connection structure as a four-tooth fir tree-shaped tenon connection structure, in which the bottom of the tenon and groove is a rounded transition, and the characteristic dimensions of the tenon head include neck width, tooth height, tooth root fillet, and tenon tooth fillet , tooth pitch, wedge angle, tooth profile angle, pressure angle, tooth bottom width, tooth bottom thickness, such as Figure 4 As shown; the characteristic dimensions of the tenon and groove include tooth height, te...

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Abstract

The invention relates to a tenon connection structure design method for a turbine rotor of a long-service-life small turbofan engine, and relates to the technical field of turbofan engines. Accordingto the tenon connection structure design method for a turbine rotor of a long-service-life small turbofan engine, in order to reduce the average load of tenon teeth, a four-pair-tooth structure is adopted, the area of a tenon and mortise working face bearing face is increased, the bottom of a mortise is changed into large fillet transition, mortise stress concentration is reduced, the stress levelof a key position is effectively reduced, and the bearing capacity of the tenon and mortise is effectively improved. And through the optimal design of the characteristic size of the tenon connectionstructure, the stress concentration of the key positions of the tenon and mortise strength is reduced, the stress level of the key positions is further reduced, and the bearing capacity of the structure is improved.

Description

technical field [0001] The invention relates to the technical field of turbofan engines, in particular to a tenon connection structure design method for long-life small turbofan engine turbine rotors. Background technique [0002] The turbine disk and turbine rotor blades of a turbine engine generally adopt a fir tree-shaped tenon connection structure, which has a great impact on the strength, life and failure of the turbine disk and turbine blades. In the existing tenon connection structure, the tenon is installed in the tenon groove through three pairs of tenon teeth to realize the connection between the blade and the wheel ( figure 1 ). When the engine is working, the centrifugal force of the blade is transmitted to the wheel disk through three pairs of mortise teeth working surfaces. [0003] During the working process of the engine, the turbine blades mainly bear centrifugal loads caused by high-speed rotation, temperature loads caused by high-temperature environments...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/17
Inventor 杜永恩王雨龙徐乐党永杰杨凯
Owner BEIJING POWER MACHINERY INST
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