发明名称 Wrapped paired blade rotor
摘要 A new lightweight bladed rotor for gas turbine or turbojet engines combines an inner support ring with blade straps made of fiber reinforced material. The blade straps wrap halfway around the inner support ring so that their ends extend radially outwardly to form blade pairs. A rim connects the blade straps near their ends to provide rigidity and to define a flowpath.
申请公布号 US5273401(A) 申请公布日期 1993.12.28
申请号 US19920907272 申请日期 1992.07.01
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE 发明人 GRIFFIN, JOSEPH T.
分类号 F01D5/28;(IPC1-7):F01D5/02 主分类号 F01D5/28
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