Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Irregular – flanged or channel forming blade surface
Patent
1980-08-27
1981-10-06
Powell, Jr., Everette A.
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Irregular, flanged or channel forming blade surface
416175, 416236A, B63H 118
Patent
active
042932807
ABSTRACT:
A propeller blade for a multi-bladed propeller comprises a radial inner pion, a radially outer portion and a transition portion extending therebetween. Generally, the leading edge of the blade portions are colinear and the trailing edges of the inner and outer blade portions are offset from each other so that shoulders are defined on the transition portion and the outer blade portion has a higher blade angle of attack than the inner blade portion. The shoulders extend from the leading edge to the trailing edge of the transition for providing flow stability and blade reinforcement.
REFERENCES:
patent: D138866 (1944-09-01), Orsett
patent: 329822 (1885-11-01), De Bruignac
patent: 1688639 (1928-10-01), Larson
patent: 1872749 (1932-08-01), Karageorge
patent: 2327453 (1943-08-01), Presser
patent: 2421798 (1947-06-01), Marshall
patent: 3065723 (1962-11-01), Tulin
patent: 3077173 (1963-02-01), Lang
patent: 3306246 (1967-02-01), Reder
patent: 3572962 (1971-03-01), Embleton et al.
Beers R. F.
Marsh L. A.
Powell Jr. Everette A.
Randolph W. W.
The United States of America as represented by the Secretary of
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