Method and system for improving flow characteristics in marine propellers

Patent metadata

Field	Value
Publication number	US-10633067-B2
Application number	US-201615295303-A
Country	US
Kind code	B2
Filing date	Oct 17, 2016
Priority date	Oct 17, 2016
Publication date	Apr 28, 2020
Grant date	Apr 28, 2020

Abstract

A propeller assembly is provided. The propeller assembly includes a central hub including a forward end, an aft end, and a hub body extending therebetween along an axis of rotation of the central hub. The propeller assembly further includes a first retention member including a first radial interference member, the first retention member coupled to the forward end of the central hub and a second retention member including a second radial interference member, the second retention member coupled to the aft end of the central hub. The propeller assembly also includes a fairing platform extending between the first retention member and the second retention member, wherein the fairing platform is retained by the first radial interference member and by the second radial interference member.

First claim

What is claimed is:

1. A propeller assembly, comprising:
a central hub comprising a forward end, an aft end, and a hub body extending therebetween along an axis of rotation of said central hub; a plurality of blades extending from said central hub, each of said plurality of blades being connected to said central hub with a dovetail joint, said dovetail joint having a curved portion that is curved around the axis of rotation of said central hub;
a first retention member including a first radial interference member having a first complementary feature that defines a first engagement, said first retention member coupled to said forward end of said central hub;
a second retention member including a second radial interference member having a second complementary feature that defines a second engagement, said second retention member coupled to said aft end of said central hub; and
a fairing platform that is separable from the plurality of blades and said central hub, said fairing platform extending between said first retention member and said second retention member, wherein said fairing platform is retained by said first engagement of said first radial interference member and by said second engagement of said second radial interference member.

2. A propeller assembly in accordance with claim 1 , wherein at least one of the first radial interference member and the second radial interference member limit the radial motion of the fairing platform.

3. A propeller assembly in accordance with claim 1 , wherein said fairing platform extends between two adjacent blades of said plurality of blades.

4. A propeller assembly in accordance with claim 3 , wherein said plurality of blades is separable from said central hub.

5. A propeller assembly in accordance with claim 3 , wherein said plurality of blades comprises at least one of a metal material, a composite material, and a combination thereof.

6. A propeller assembly in accordance with claim 1 , wherein said first retention member further comprises an aft face, said first radial interference member circumscribing said aft face, and said second retention member further comprises a forward face, said second radial interference member circumscribing said forward face.

7. A propeller assembly in accordance with claim 1 , wherein said fairing platform is floatingly retained by at least one of said first retention member and said second retention member such that a clearance between said fairing platform and at least one of said first retention member and said second retention member facilitates at least some movement of said fairing platform in at least one direction.

8. A propeller assembly in accordance with claim 1 , wherein said fairing platform further comprises: a forward platform retention member complementary to said first complementary feature of said first radial interference member and configured to be retained by first complementary feature of said first radial interference member; and an aft platform retention member complementary to said second complementary feature of said second radial interference member and configured to be retained by said second complementary feature of second radial interference member.

9. A propeller assembly in accordance with claim 8 , wherein at least one of the first engagement and the second engagement is one of a tongue and groove engagement and a mortise and tenon engagement.

10. A propeller assembly in accordance with claim 1 , wherein said hub comprises a radially outer hub surface having a first flow coefficient, said fairing platform comprises a radially outer platform surface having a second flow coefficient, and said second flow coefficient is greater than said first flow coefficient.

11. A propeller assembly in accordance with claim 10 , wherein said first coefficient and said second coefficient relate to at least one of: (i) an amount of cavitation during operation; (ii) generated thrust; (iii) open water efficiency; (iv) hull efficiency; (v) relative rotative efficiency; (vi) mechanical efficiency; (vii) a quasi-propulsive coefficient; and (viii) acoustic efficiency.

12. A propeller assembly in accordance with claim 1 , wherein said central hub includes a plurality of dovetail grooves, each of said plurality of dovetail grooves being configured to receive a wedge and a dovetail of one of said plurality of blades.

13. A fairing structure supportable by a central hub of a propeller assembly, the central hub including a forward end, an aft end, and a hub body extending therebetween along an axis of rotation of the central hub, said fairing structure comprising:
a first retention member including a first radial interference member having a first complementary feature that defines a first engagement, said first retention member couplable to the forward end of the central hub;
a second retention member including a second radial interference member having a second complementary feature that defines a second engagement, said second retention member couplable to the aft end of the central hub; and
a fairing platform that is separable from a plurality of blades and said central hub, said plurality of blades being connected to said central hub with a dovetail joint, said dovetail joint having a curved portion that is curved around the axis of rotation of said central hub, said fairing platform extending from said hub body, the fairing platform extending between said first retention member and said second retention member, said fairing platform engaging said first engagement of said first radial interference member and said second engagement of said second radial interference member.

14. A fairing structure in accordance with claim 13 , wherein at least one of the first radial interference member and the second radial interference member limit the radial motion of the fairing platform and wherein said fairing platform is configured to be floatingly retained by each of said first retention member and said second retention member.

15. A fairing structure in accordance with claim 13 , wherein said first retention member further comprises an aft face, said first radial interference member circumscribing said aft face, and said second retention member further comprises a forward face, said second radial interference member circumscribing said forward face.

16. A fairing structure in accordance with claim 13 , wherein said fairing platform further comprises: a forward platform retention member complementary to said first radial interference member and configured to be retained by said first radial interference member; and an aft platform retention member complementary to said second radial interference member and configured to be retained by said second radial interference member.

17. A fairing structure in accordance with claim 16 , wherein said first radial interference member and said first retention member comprise first complementary features that define said first engagement, said second radial interference member and said second retention member comprise second complementary features that define said second engagement, and at least one of the first engagement and the second engagement is one of one of a tongue and groove engagement and a mortise and tenon engagement.

18. A fairing structure in accordance with claim 13 , wherein the hub includes a radially outer hub surface having a first flow coefficient, said fairing platform comprises a radially outer platform surface having a second flow coefficient, and said second flow coefficient is greater than the first flow coefficient.

Assignees

• Gen Electric

Inventors

• Kray Nicholas Joseph
• Van Nieuwenhove Stefaan Guido
• Baehmann Peggy Lynn

Classifications

• B63H1/28

  Other means for improving propeller efficiency · CPC title

• F01D11/008

  by spacer elements between the blades, e.g. independent interblade platforms · CPC title

• B63H1/20 Primary

  Hubs; Blade connections · CPC title

• B63H2001/283

  Propeller hub caps with fins having a pitch different from pitch of propeller blades, or a helix hand opposed to the propellers' helix hand · CPC title