Development of Design Principles for a Creep-Limited Alloy for Turbine Blades

Z. Huda

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Development of Design Principles for a Creep-Limited Alloy for Turbine Blades

机译：涡轮叶片蠕变有限合金设计原理的发展

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摘要

Recent advancements in turbine-blade materials engineering are reviewed in light of general superalloy research and the author's work on a new powder metallurgy IN-792 creep-limited alloy for application in blades of gas-turbine engines. The developed set of principles presented in this paper incorporates all the factors that must be taken into consideration in selecting and designing an alloy for turbine blades.

机译：根据一般的超合金研究以及作者在用于燃气涡轮发动机叶片的新型粉末冶金IN-792蠕变极限合金中的工作，对涡轮叶片材料工程的最新进展进行了综述。本文提出的一套已开发的原理综合了在选择和设计涡轮叶片合金时必须考虑的所有因素。

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来源
《Journal of Materials Engineering and Performance》 |1995年第1期|p.48-53|共6页
作者
Z. Huda;
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作者单位

Metallurgical Engineering Department, Dawood College of Engineering & Technology, Karachi 74800, Pakistan;

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原文格式 PDF
正文语种 eng
中图分类金属学与金属工艺;
关键词
alloy design; creep; IN-792; powder metallurgy; turbine blades;

机译：合金设计;蠕变;IN-792;粉末冶金;涡轮叶片;

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1. Development of Design Principles for a Creep-Limited Alloy for Turbine Blades [J] . Z. Huda Journal of Materials Engineering and Performance . 1995,第1期

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7. Design for Recycling Principles Applicable to Selected Clean Energy Technologies: Crystalline-Silicon Photovoltaic Modules, Electric Vehicle Batteries, and Wind Turbine Blades [O] . Alex Norgren, Alberta Carpenter, Garvin Heath 2020

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Development of Design Principles for a Creep-Limited Alloy for Turbine Blades

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