Turbine blade forming material long-time service condition simulation test device

A technology for simulating turbine blades and operating conditions, which is applied to measuring devices, analyzing materials, and using stable tension/pressure to test the strength of materials, etc., can solve the problem of long time-consuming, high testing costs, and inability to truly reflect the service work of formed turbine blades. low cost, high simulation test efficiency, and simple structure

Pending Publication Date: 2022-04-15
DONGFANG TURBINE CO LTD
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] The performance test of method 1 cannot simulate the multi-parameter environment at the same time and in the same space for real service conditions, so it cannot truly reflect the service conditions of the formed turbine blades in the gas turbine
[0006] Although the performance test of the second method can truly reflect the service conditions of the formed turbine blades in the gas turbine, the test cost is huge and time-consuming

Method used

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  • Turbine blade forming material long-time service condition simulation test device
  • Turbine blade forming material long-time service condition simulation test device
  • Turbine blade forming material long-time service condition simulation test device

Examples

Experimental program
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Effect test

Embodiment 1

[0041] see figure 1 , figure 2 and image 3 As shown, the present invention includes a creep testing machine 1 , a sample assembly 4 , a cooling atmosphere simulation system 2 and a working atmosphere simulation system 3 .

[0042] The creep testing machine 1 is mainly composed of a main engine, a test frame, a measuring and controlling device 15, a heater 16, and the like. Wherein, the test frame is mainly composed of two sets of upright columns 11 and a beam 12 between the two sets of upright columns 11 , the beam 12 is connected with an upper joint 13 . The main engine is used to output the pull-out force for the creep performance test on the sample assembly 4 clamped by the test frame, and the output end of the main engine is connected with a lower joint 14 . The measuring and controlling device 15 integrates various temperature sensors and various strain sensors, and is mainly used for controlling and collecting temperature signals and deformation detection signals of...

Embodiment 2

[0067] The other contents of this embodiment are the same as those of Embodiment 1, except that: the sample body of the sample assembly has no coating structure, that is, only the performance of the superalloy material is simulated and the coating is not involved.

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PUM

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Abstract

The invention discloses a long-time service condition simulation test device for a material for forming a turbine blade. The long-time service condition simulation test device comprises a creep testing machine, a sample assembly, a cooling atmosphere simulation system and an acting atmosphere simulation system, the sample assembly is clamped on the creep testing machine and mainly comprises a sample body, an outer pipe, an upper clamp and a lower clamp, an alloy base material of the sample body is made of a high-temperature alloy material to be tested, an inner hole of the sample body forms a cooling atmosphere simulation cavity, and a working atmosphere simulation cavity is formed between the sample body and the outer pipe; the cooling atmosphere simulation system is used for conveying cooling gas with required pressure, flow and temperature to the cooling atmosphere simulation cavity; the acting atmosphere simulation system is used for conveying fuel gas with required pressure, flow and temperature to the acting atmosphere simulation cavity. According to the invention, the long-time creep property of the material for forming the turbine blade can be tested under the coupling action of factors such as heat, force and chemical factors in the long-time service process, and the service condition of the formed turbine blade in a gas turbine can be truly reflected.

Description

technical field [0001] The invention relates to material service performance testing equipment, in particular to a material used for forming gas turbine blades (turbine blades), and a simulation test device for long-term service working conditions. Background technique [0002] As an important component of the turbine section of a gas turbine, the turbine blade has long served in the extreme working conditions of high temperature and high pressure, and is a typical hot end part of the gas turbine. Since the turbine blade has been in the part with the highest temperature, the most complex stress and the harshest environment for a long time, it is one of the parts with the worst working environment and the most complex structure of the gas turbine, and it is also one of the parts with frequent fracture failures of the gas turbine. [0003] In order to meet the technical requirements of operation, the turbine blades of the gas turbine are provided with flow channels for cooli...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N3/00G01N3/18G01N3/02G01N3/04
Inventor 陈艺文孙友贝裴玉冰巩秀芳隆彬王天剑李定骏龙老虎江雷张波郭维华高振桓李金祺李翠芹娄霞王伟
Owner DONGFANG TURBINE CO LTD
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