Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Formed with main spar
Patent
1977-08-02
1980-02-12
Powell, Jr., Everette A.
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Formed with main spar
416145, 416229R, 416500, B64C 2746
Patent
active
041881710
ABSTRACT:
A load absorbing elastic member or members is incorporated in the design of a rotor blade to assist in reducing flapwise and chordwise bending moments, torsional loading, and to reduce or eliminate the control system loads induced by rotor blade moment stall. In all its embodiments, the load absorbing elastic member has operatively associated therewith a constraining member which serves as a strain amplifier permitting the load absorbing elastic member to achieve its purpose effectively.
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patent: 3603701 (1971-09-01), Tarczynski
patent: 3645481 (1972-02-01), Purdy
patent: 3782856 (1974-01-01), Salkind et al.
D'Ambrosio Felix J.
Greigg Edwin E.
Powell Jr. Everette A.
Puffer Jack D.
The Boeing Company
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