首页> 外国专利> PROCESS FOR PRODUCING ABRADABLE METAL/CERAMIC SEAL STRUCTURES, PARTICULARLY FOR APPLICATION ON TURBINE ENGINE SURFACES, AND SEAL STRUCTURES PRODUCED ACCORDING TO THE PROCESS

PROCESS FOR PRODUCING ABRADABLE METAL/CERAMIC SEAL STRUCTURES, PARTICULARLY FOR APPLICATION ON TURBINE ENGINE SURFACES, AND SEAL STRUCTURES PRODUCED ACCORDING TO THE PROCESS

机译:生产可变形的金属/陶瓷密封结构的方法,特别是在涡轮发动机表面上的应用,以及根据该方法生产的密封结构

摘要

A metal/ceramic abradable seal structure (10,18) of the type used in aircraft turbine engines is improved by using a metal substrate (10) which is able to deform during cooling from the brazing temperature and is then rendered rigid after the cool down by applying reinforcements (20,22) to the substrate (10). By this method internal stress in the material is relieved which would otherwise occur, if an initially rigid substrate was used.
机译:用于飞机涡轮发动机的金属/陶瓷耐磨密封结构(10,18)通过使用金属基底(10)得以改进,该基底能够在冷却过程中从钎焊温度变形,然后在冷却后变硬通过将增强物(20,22)施加到基底(10)上。通过这种方法,可以减轻材料中的内部应力,如果使用最初的刚性基材,则可能会发生内部应力。

著录项

  • 公开/公告号DE2964875D1

    专利类型

  • 公开/公告日1983-03-24

    原文格式PDF

  • 申请/专利权人 UNION CARBIDE CORPORATION;

    申请/专利号DE19792964875T

  • 发明设计人 SARA RAYMOND VINCENT;

    申请日1979-12-19

  • 分类号C04B37/02;F01D11/08;

  • 国家 DE

  • 入库时间 2022-08-22 10:10:35

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