发明名称 THERMALLY HIGHLY STRESSED COOLED TURBINE BLADE
摘要 A structural component which is coolable for use under high thermal load conditions, such as a turbine blade, has a metallic support core with cooling ducts separated by lands in its surface. The core and its cooling ducts and lands are enclosed by an inner layer of metal felt and an outer layer of heat insulating ceramic material which partially penetrates into the metal felt to form a bonding zone between the felt and the ceramic material. Thus, any heat passing through the ceramic layer is introduced into the large surface area of the metal felt enabling the latter to efficiently introduce the heat into a cooling medium flowing in the ducts, thereby preventing thermal loads from adversely affecting the metal core to any appreciable extent.
申请公布号 EP0132667(B1) 申请公布日期 1987.10.28
申请号 EP19840107962 申请日期 1984.07.07
申请人 MTU MOTOREN- UND TURBINEN-UNION MUNCHEN GMBH 发明人 SCHWEITZER, KLAUS, DR.RER.NAT. DIPL.-CHEM.
分类号 F01D5/18;B23K1/19;B32B15/04;B32B18/00;F01D5/28;F01D11/12;F01D25/00;(IPC1-7):F01D5/28 主分类号 F01D5/18
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