Rotor blade internal damper
作者： Joseph M. Baskin
DOI:
关键词: Amplifier 、 Damper 、 Bending moment 、 Engineering 、 Control system 、 Stall (fluid mechanics) 、 Structural engineering
摘要: A load absorbing elastic member or members is incorporated in the design of a rotor blade to assist reducing flapwise and chordwise bending moments, torsional loading, reduce eliminate control system loads induced by moment stall. In all its embodiments, has operatively associated therewith constraining which serves as strain amplifier permitting achieve purpose effectively.
lens.org 参考文章(17)
Charles V Toner, Rotor blade variable modulus trailing edge ,(1969)
Tadeusz Tarcrynski, Composite rotor blade retention ,(1969)
Robert C. Huss, Raymond P. Belko, Rotor blade tipweight assembly ,(1977)
Robert Zincone, Composite tip weight attachment ,(1975)
James A Hinds, Method of manufacturing plastic rotor blades ,(1957)
Thomas S. Scarpati, Robert J. Ford, Method of fabricating a composite aerodynamic rotorblade assembly ,(1976)
Michael J. Salkind, William C. Reinfelder, Composite aerodynamic blade with twin-beam spar ,(1973)
Igor Ivanovich Kovyryalkin, Vladimir Borisovich Golstman, Nikolai Ilich Kamov, Alexandr Georgievich Satarov, Konstantin Nikolaevich Guskov, Mark Alexandrovich Kupfer, Stanislav Ivanovich Stetsenko, Anatoly Filippovich Vakulenko, Iosif Shulimovich Sherman, Anatoly Fedorovich Kovalev, Nikolai Nikolaevich Priorov, Method of manufacture of hollow pieces ,(1974)
Huber John Richard, Aircraft rotor blade construction ,(1954)
Michael E Gluhareff, Rotor blade retention of a bolted and cemented construction ,(1948)