发明名称 Impact absorbing blade mounts for variable pitch blades
摘要 A variable pitch blade and blade mount which is suitable for propellers, fans and the like and which has improved impact resistance. The invention is particularly directed to composite fan blades and blade mounting arrangements wherein the blades are permitted to pivot relative to a turbine hub about an axis generally parallel to the centerline of the engine upon impact of a large foreign object, such as a bird. By thus providing for the pivoting of the blades upon impact, centrifugal force recovery becomes the principal energy absorbing mechanism and a blade having improved impact strength is obtained.
申请公布号 US4047840(A) 申请公布日期 1977.09.13
申请号 US19750581751 申请日期 1975.05.29
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 RAVENHALL, RICHARD;SALEMME, CHARLES T.;ADAMSON, ARTHUR P.
分类号 F04D29/36;B64C11/02;F02C9/22;F04D29/32;(IPC1-7):F04D29/36;F01D5/32 主分类号 F04D29/36
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