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US4073601A Expired / Lapsed US ⏱️ 0.0 years remaining

Marine propeller

Assignee: Michigan Wheel Corp
•
Filing: 1976-06-14
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Granted: 1978-02-14
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Expires: 1996-06-14
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Abstract

Abstract A marine propeller with unique blade geometry resistant to cavitation and ventilation at high speed operation. The face of the blade has a special convexly curved portion extending from the leading blade edge to a transition zone along the blade chord length toward the blade trailing edge, and a special concavely curved portion from this transition zone to the trailing blade edge, both defined herein.

Inventors

  • 👤 Robert F. Kress

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 16:21
CPC Classifications
B; B63; B63H; B63H1/00; B63H1/02; B63H1/12; B63H1/14; B63H1/26

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 287 words
A marine propeller having specially configurated blades exhibiting resistance to ventilation and cavitation at high speed operation, each blade including a leading edge, a trailing edge, a face constituting a pressure side, and a back constituting a suction side; said face having a contour consisting of a convex surface extending from said leading edge to a transition zone about 20-25% of the blade chord length toward said trailing edge, and a concave surface extending the remainder of the chord length to said trailing edge; said convex and concave surfaces having curvatures defined relative to reference pitch datum lines at particular radial blade sections, said reference line at any particular radial blade section being a straight line outside of said blade, intersecting said blade trailing edge, and at an angle φ to a plane transverse to the propeller axis, the arc tangent of said angle φ being the blade pitch divided by 2πr, where r is the distance of the particular radial blade section from the propeller axis; said blade having its maximum set back from said pitch datum line at said leading edge, said set back being between about 7% of the blade chord length at the inner radii blade sections to about 1% of the blade chord length at the outer blade chord sections; said blade convex surface having minimum offset from said pitch datum line at about 10 to 15% of the blade chord length from said leading edge, said offset being about 1 to 21/2% of the blade chord length; said blade concave surface having a maximum spacing from said pitch datum line at about mid-chord length, said spacing being about 2 to 31/2 of the blade chord length from said pitch datum line.
Claim 2
Dependent Claim 287 words
A marine propeller having specially configurated blades exhibiting resistance to ventilation and cavitation at high speed operation, each blade including a leading edge, a trailing edge, a face constituting a pressure side, and a back constituting a suction side; said face having a contour consisting of a convex surface extending from said leading edge to a transition zone about 20-25% of the blade chord length toward said trailing edge, and a concave surface extending the remainder of the chord length to said trailing edge; said convex and concave surfaces having curvatures defined relative to reference pitch datum lines at particular radial blade sections, said reference line at any particular radial blade section being a straight line outside of said blade, intersecting said blade trailing edge, and at an angle φ to a plane transverse to the propeller axis, the arc tangent of said angle φ being the blade pitch divided by 2πr, where r is the distance of the particular radial blade section from the propeller axis; said blade having its maximum set back from said pitch datum line at said leading edge, said set back being between about 7% of the blade chord length at the inner radii blade sections to about 1% of the blade chord length at the outer blade chord sections; said blade convex surface having minimum offset from said pitch datum line at about 10 to 15% of the blade chord length from said leading edge, said offset being about 1 to 21/2% of the blade chord length; said blade concave surface having a maximum spacing from said pitch datum line at about mid-chord length, said spacing being about 2 to 31/2 of the blade chord length from said pitch datum line.
Claim 3
Dependent Claim 21 words
The marine propeller blade in claim 1 wherein said back is convexly curved from said leading edge toward said trailing edge.

References Cited (Backward Citations)

DE302859C Cited
US2157999A Cited
US2682925A Cited
US3261297A Cited
US3514215A Cited
US3697193A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-02-13 1981-08-15 1982-02-14 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-02-13 1985-08-15 1986-02-14 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-02-13 1989-08-15 1990-02-14 $7700.00 Window Closed / Lapsed

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