US2006211315A1PendingUtilityA1
Bravo drive propeller shaft bearing carrier
Individually held — no corporate assignee on recordPriority: Mar 17, 2005Filed: Mar 17, 2005Published: Sep 21, 2006
Est. expiryMar 17, 2025(expired)· nominal 20-yr term from priority
Inventors:Rolf Papke
B63H 23/34B63H 1/14B63H 2001/185
25
PatentIndex Score
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Cited by
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References
0
Claims
Abstract
A propeller drive system for V-hull and catamaran racing vessels including an offshore racing cleaver propeller run on a long, thick propeller shaft coupled with a Bravo Unit Drive Motor at, and above, the water's surface through a tightly fitted bearing carrier.
Claims
exact text as granted — not AI-modified1 . In a stern-mounted propulsion system for a marine vessel of the type having a Bravo Unit Drive Motor, a bearing carrier at an output end of said motor, a propeller shaft coupled to said motor via said bearing carrier and having a splined first end and a threaded second end, and an offshore racing cleaver propeller on said threaded second end, the improvement comprising a bearing carrier to securely fit and support said propeller shaft when being of a length and girth to ride above the surface of the water through which the vessel is propelled.
2 . The improvement of claim 1 wherein said bearing carrier securely fits and supports said propeller shaft when being of a length and girth to ride to a height of 2-½ inches above the surface of the water through which the marine vessel is propelled.
3 . The improvement of claim 1 wherein said bearing carrier through which said propeller shaft couples includes an apertured front end of a diameter to receive said threaded end of said propeller shaft and an apertured rear end of a diameter to receive said splined end of said shaft.
4 . The improvement of claim 3 wherein the aperture of said apertured front end is of a diameter of substantially 2.900 inches and wherein the aperture of said apertured rear end is of a diameter of substantially 3.865 inches.
5 . The improvement of claim 4 wherein said apertured front end is of a diameter of substantially 4.305 inches and wherein said apertured rear end is of a diameter of substantially 4.283 inches.
6 . The improvement of claim 5 wherein said bearing carrier is of a length between said front and rear apertured ends of substantially 4.900 inches.
7 . The improvement of claim 6 wherein said bearing carrier is composed of hard anodized, billeted aircraft 2024 aluminum.Join the waitlist — get patent alerts
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