US4073601A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Marine propeller
Assignee: Michigan Wheel Corp
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Filing: 1976-06-14
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Granted: 1978-02-14
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Expires: 1996-06-14
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)
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US2682925A
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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 |