IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0444101
(2007-09-25)
|
등록번호 |
US-8491268
(2013-07-23)
|
우선권정보 |
AU-2006905421 (2006-10-02); AU-2006233263 (2006-10-30) |
국제출원번호 |
PCT/AU2007/001448
(2007-09-25)
|
§371/§102 date |
20100119
(20100119)
|
국제공개번호 |
WO2008/040049
(2008-04-10)
|
발명자
/ 주소 |
|
출원인 / 주소 |
|
대리인 / 주소 |
|
인용정보 |
피인용 횟수 :
1 인용 특허 :
7 |
초록
A propeller (10,110) has a hub (20,120) with blades (40,140). A safety member (50,150) is provided along at least a portion of the leading edge (43,143) of each blade (40,140); and the blades (140) may incorporate anti-cavitation slots (160).
대표청구항
▼
1. A safety propeller, preferably for watercraft, of the type having a hub and a plurality of blades, where each blade has a leading edge extending from a proximal end of the blade adjacent the hub to a distal end spaced from the hub; and a respective safety member that extends over more than 50% of
1. A safety propeller, preferably for watercraft, of the type having a hub and a plurality of blades, where each blade has a leading edge extending from a proximal end of the blade adjacent the hub to a distal end spaced from the hub; and a respective safety member that extends over more than 50% of the length of the leading edge of each blade, each safety member being of greater height than the leading edge so that the safety member will strike any obstruction before the balance of the leading edge not provided with the safety member, and at least a portion of the safety member extending from a thrust or driving face of the blade in the forward direction of rotation of the propeller. 2. A propeller as claimed in claim 1, wherein: for a propeller which rotates in a clockwise direction (when viewed from a trailing end of the hub), the safety member on each thrust or driving face of the blade appears to be directed towards the trailing end of the propeller. 3. A propeller as claimed in claim 1, wherein: the safety member is of a constant height over the leading edge, or of relatively increasing height towards the distal end of the blade. 4. A propeller as claimed in claim 1, wherein: the safety member is located with a central axis substantially parallel to, or aligned with, the leading edge, or with the central axis increasingly leading the leading edge of the blade in the direction from the proximal end to the distal end of the blade. 5. A propeller as claimed in claim 4, wherein: the safety member is smoothly contoured into the adjacent portion of the blade. 6. A propeller as claimed in claim 1, wherein: the safety member is mounted on, or formed integrally with, the blade. 7. A propeller as claimed in claim 1, wherein: at least one anti-cavitation slot is provided in each blade. 8. A propeller as claimed in claim 7, wherein: each cavitation slot is circular, square, rectangular or modified rectangular shape in plan view. 9. A propeller as claimed in claim 8, wherein: the or each side wall of the anti-cavitation slot extends through blade substantially parallel to the rotational axis of the propeller. 10. A propeller, preferably for watercraft, of the type having a hub and a plurality of blades, where each blade has a respective leading edge and a trailing edge extending from respective proximal ends of the blade adjacent the hub to a distal end spaced from the hub; wherein: one anti-cavitation slot that extends through each blade, and is located at the mid-point between (i) the respective leading edge and trailing edge of the blade and (ii) at 50% the radial distance from the hub and the distal end of the blade. 11. A propeller as claimed in claim 10, wherein: the anti-cavitation slot is of circular, square, rectangular, modified-rectangular or other shape in plan view. 12. A propeller as claimed in claim 11, wherein: the internal edges of the blade that together define the anti-cavitation slot lie substantially parallel to the rotational axis of the hub. 13. A propeller as claimed in claim 11, wherein: the internal edges of the blade together define at least one of a square and rectangular anti-cavitation slot such that opposed side walls of the anti-cavitation slot extend substantially parallel to a central axis of the slot extending substantially radially from the hub. 14. A propeller, preferably for watercraft, of the type having a hub and a plurality of blades, where each blade has a leading edge extending from a proximal end of the blade adjacent the hub to a distal end spaced from the hub; a respective safety member that extends over more than 50% of the length of the leading edge of each blade, each safety member being of greater height than the leading edge, and at least a portion of the safety member extending from a thrust or driving face of the blade in the forward direction of rotation of the propeller; andone anti-cavitation slot that extends through each blade, and is located at the mid-point between (i) the respective leading edge and trailing edge of the blade and (ii) at 50% the radial distance from the hub to the distal end of the blade. 15. A safety propeller, preferably for watercraft, of the type having a hub and a plurality of blades, where each blade has a leading edge extending from a proximal end of the blade adjacent the hub to a distal end spaced from the hub; and a respective safety member that extends over more than 50% of the length of the leading edge of each blade and is of a greater thickness so that the safety member will strike any obstruction before the balance of the leading edge not provided with the safety member, with at least a portion of the safety member extending from a thrust or driving face of the blade in the forward direction of rotation of the propeller. 16. A propeller, preferably for watercraft, of the type having a hub and a plurality of blades, where each blade has a leading edge extending from a proximal end of the blade adjacent the hub to a distal end spaced from the hub; a respective safety member that extends over more than 50% of the length of the leading edge of each blade, each safety member being of greater thickness than the leading edge, and at least a portion of the safety member extending from a thrust or driving face of the blade in the forward direction of rotation of the propeller; andone anti-cavitation slot defined through each blade, and located at the mid-point between: (i) the respective leading edge and trailing edge of the blade, and (ii) at 50% of the radial distance from the hub to the distal end of the blade.
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