Temperature distribution and thermal stress analysis for turbojet engine turbine guide blade

Yang Sun; Jian Lu; Yan Zheng; Jie Hong; Hang Cao; Rui Hu Zhang

Temperature distribution and thermal stress analysis for turbojet engine turbine guide blade

Yang Sun^*
, Jian Lu
, Yan Zheng
, Jie Hong
, Hang Cao
, Rui Hu Zhang

^*此作品的通讯作者

能源与动力工程学院

Nanjing University of Aeronautics and Astronautics
Airforce Deputy Dept. of Jingfeng
The Electrical and Mechanical Engineering Institute of Beijing
Beihang University

科研成果: 期刊稿件 › 文章 › 同行评审

1 引用（Scopus）

摘要

An FEA model for turbojet engine turbine was established and the turbine guide blade temperature distribution was computed. The turbine guide blade thermal stress was studied. The results are helpful for the turbine guide blade design of the turbojet engine.

源语言	英语
页（从-至）	357-359
页数	3
期刊	Tuijin Jishu/Journal of Propulsion Technology
卷	25
期	4
出版状态	已出版 - 8月 2004

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引用此

@article{3f3dbe81af54446a861c896b15780098,

title = "Temperature distribution and thermal stress analysis for turbojet engine turbine guide blade",

abstract = "An FEA model for turbojet engine turbine was established and the turbine guide blade temperature distribution was computed. The turbine guide blade thermal stress was studied. The results are helpful for the turbine guide blade design of the turbojet engine.",

keywords = "Temperature distribution, Thermal stress, Turbojet engine, Turborotor",

author = "Yang Sun and Jian Lu and Yan Zheng and Jie Hong and Hang Cao and Zhang, \{Rui Hu\}",

year = "2004",

month = aug,

language = "英语",

volume = "25",

pages = "357--359",

journal = "Tuijin Jishu/Journal of Propulsion Technology",

issn = "1001-4055",

publisher = "China Aerospace Science and Industry Corp",

number = "4",

}

TY - JOUR

T1 - Temperature distribution and thermal stress analysis for turbojet engine turbine guide blade

AU - Sun, Yang

AU - Lu, Jian

AU - Zheng, Yan

AU - Hong, Jie

AU - Cao, Hang

AU - Zhang, Rui Hu

PY - 2004/8

Y1 - 2004/8

N2 - An FEA model for turbojet engine turbine was established and the turbine guide blade temperature distribution was computed. The turbine guide blade thermal stress was studied. The results are helpful for the turbine guide blade design of the turbojet engine.

AB - An FEA model for turbojet engine turbine was established and the turbine guide blade temperature distribution was computed. The turbine guide blade thermal stress was studied. The results are helpful for the turbine guide blade design of the turbojet engine.

KW - Temperature distribution

KW - Thermal stress

KW - Turbojet engine

KW - Turborotor

UR - https://www.scopus.com/pages/publications/7244251744

M3 - 文章

AN - SCOPUS:7244251744

SN - 1001-4055

VL - 25

SP - 357

EP - 359

JO - Tuijin Jishu/Journal of Propulsion Technology

JF - Tuijin Jishu/Journal of Propulsion Technology

IS - 4

ER -

Temperature distribution and thermal stress analysis for turbojet engine turbine guide blade

摘要

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引用此