首页> 外国专利> DEVELOPMENT OF 2 TYPES OF MARTENSITIC GRADE STAINLESS STEEL (AE-961Ш) COMPRESSOR BLADE FORGINGS WITH AXIAL ENTRY ROOT FOR OF 1ST AND 10TH STAGE FOR TURBO SHAFT ENGINE.

DEVELOPMENT OF 2 TYPES OF MARTENSITIC GRADE STAINLESS STEEL (AE-961Ш) COMPRESSOR BLADE FORGINGS WITH AXIAL ENTRY ROOT FOR OF 1ST AND 10TH STAGE FOR TURBO SHAFT ENGINE.

机译：涡轮轴发动机第一级和第十级两种带轴向入口的马氏体不锈钢（AE-961Ш）压气机锻件的研制。

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摘要

This method is developed to supply 2 types of AE-961? steel alloy compressor blades for 1st and 10th stage with axial entry root as per the technical requirements stipulated in the test schedule for turbo shaft TV-2 engine of MI-8 Helicopter.

机译：开发此方法可提供2种类型的AE-961？根据MI-8直升机的涡轮轴TV-2发动机测试计划中规定的技术要求，带有轴向入口根部的第一级和第十级钢合金压缩机叶片。

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公开/公告号IN2015KO00035A

专利类型
公开/公告日2016-07-08

原文格式PDF
申请/专利权人
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申请/专利号IN35/KOL/2015
发明设计人 SHRI C VE NKATACHALAPATHI;SMT SUMANA MISHRA;SHRI PADALA KRISHNA;
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申请日2015-01-07
分类号C22C19/05;
国家 IN
入库时间 2022-08-21 14:24:51

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