发明名称 TURBINE SHROUD SUPPORT STRUCTURE OF JET ENGINE
摘要 PROBLEM TO BE SOLVED: To miniaturize a whole plate spring, capable of being used for a small engine, etc. SOLUTION: A support structure is constituted to engage a curved plate spring 20 which is installed at a rear end part of a turbine shroud 2, with a recessed part 19 divided by a turbine casing 1 and a stationary blade 13. In this case, the plate spring 20 has a two-division structure, wherein one plate spring 22 supports a turbine shroud 2 in the axial direction, and the other plate spring 21 supports the turbine shroud 2 in the diameter direction.
申请公布号 JPH1162509(A) 申请公布日期 1999.03.05
申请号 JP19970221633 申请日期 1997.08.18
申请人 ISHIKAWAJIMA HARIMA HEAVY IND CO LTD 发明人 FUNADOGAWA OSAMU;MIZUTANI TETSUYA;HAYAKAWA YUKIO;TANAKA TAKASHI
分类号 F01D11/08;F02C7/00;F02C7/28;(IPC1-7):F01D11/08 主分类号 F01D11/08
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