Equivalent Heat Load Test on Hot Aircraft Engine Components

被引：0

作者：

Mroz, M. ^{[1
]}

Orlowicz, A. W. ^{[1
]}

Tupaj, M. ^{[1
]}

Lenik, M. ^{[1
]}

机构：

[1] Rzeszow Univ Technol, Al Powstancow Warszawy 12, PL-35959 Rzeszow, Poland

来源：

ARCHIVES OF FOUNDRY ENGINEERING | 2023年 / 23卷 / 01期

关键词：

Heat load; Heat barrier; Aircraft engines;

D O I：

10.24425/afe.2023.144277

中图分类号：

TF [冶金工业];

学科分类号：

0806 ;

摘要：

The paper presents the assumptions and methodology for investigating equivalent heat load testing of hot aircraft engine components. The basic heat loads occurring in an aircraft engine during aircraft flight are characterised. Diagrams of the proposed heat loads are presented, together with the number of cycles, and a test bench is characterised and shown to enable equivalent heat load testing of aircraft engine components.

引用

页码：34 / 36

页数：3

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