发明名称 GAS SEAL ROTATABLE SUPPORT STRUCTURE
摘要 A toroidal structure which is lenticular in cross section and rotatable in a gas turbine environment is disclosed. The structure is described as a support member for the rotating component of a seal assembly in a high temperature application, such as a turbine rotor.
申请公布号 US3733146(A) 申请公布日期 1973.05.15
申请号 USD3733146 申请日期 1971.04.07
申请人 UNITED AIRCRAFT CORP,US 发明人 SMITH S,US;VOYER P,US
分类号 F01D5/06;F01D11/00;(IPC1-7):F01D11/08;F01D1/04 主分类号 F01D5/06
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