Systems and methods for reducing porosity in propellers

Patent metadata

Field	Value
Publication number	US-10875615-B1
Application number	US-201816105372-A
Country	US
Kind code	B1
Filing date	Aug 20, 2018
Priority date	Aug 20, 2018
Publication date	Dec 29, 2020
Grant date	Dec 29, 2020

Abstract

A method of making a propeller includes forming the propeller to have blades coupled to an outer hub, the outer hub coupled to an inner hub via ribs, and the inner hub configured to be coupled to the marine vessel. The ribs each have first and second ends with a midpoint therebetween, an inner end and an outer end that define a width therebetween, and a leading surface and a trailing surface that define a thickness therebetween. The ribs are tapered such that the thickness is greater at the midpoint than at least at one of the first end and the second end, and scalloped such that the width is greater at the midpoint than at least at one of the first end and the second end. Each of the ribs is coupled to the outer hub in radial alignment with one of the blades.

First claim

We claim:

1. A method of making a propeller for a marine vessel, the method comprising:
forming the propeller to have blades coupled to an outer hub;
forming the propeller such that the outer hub is coupled to an inner hub via ribs, wherein the inner hub is configured to be coupled to the marine vessel, wherein the ribs each have a first end and a second end that define a length therebetween, wherein a midpoint is further defined between the first end and the second end, wherein the ribs each have an inner end and an outer end that define a width therebetween, and wherein the ribs each have a leading surface and a trailing surface that define a thickness therebetween;
forming each of the ribs to be tapered such that the thickness is greater at the midpoint than at least at one of the first end and the second end;
forming each of the ribs to be scalloped such that the width is greater at the midpoint than at least at one of the first end and the second end, wherein the length between the first end and the second end varies from a smallest length to a greatest length that differ by a delta, and wherein each of the ribs is also scalloped such that the delta is greater than the width at the midpoint; and
forming the propeller such that each of the ribs is coupled to the outer hub to be radially aligned with one of the blades.

2. The method according to claim 1 , wherein the propeller is configured such that the first end is farther than the second end from the marine vessel when the propeller is coupled thereto, wherein the thickness is greater at the second end than at the first end, and wherein the width is greater at the second end than at the first end.

3. The method according to claim 1 , wherein each of the blades has a thickest region, and wherein each of the ribs is radially aligned with the thickest region of one of the blades.

4. The method according to claim 1 , wherein each of the blades has a blade width divided into even thirds, and wherein each of the ribs is radially aligned with a center third of the even thirds of one of the blades.

5. The method according to claim 1 , wherein the blades are three individual blades, and wherein the ribs are three individual ribs.

6. The method according to claim 1 , further comprising forming each of the ribs to also be tapered between the inner end and the outer end such that the thickness is greater at the outer end than at the inner end.

7. The method according to claim 1 , wherein the propeller is formed of aluminum.

8. The method according to claim 1 , wherein each of the ribs has a center plane that is centrally defined between the leading surface and the trailing surface, and wherein the center plane is perpendicular to both the inner hub and the outer hub.

9. A propeller for a marine vessel, the propeller comprising:
an inner hub configured to be coupled to the marine vessel;
an outer hub and a plurality of ribs that couple the outer hub to the inner hub, wherein the ribs each have a first end and a second end that define a length therebetween, wherein a midpoint is further defined between the first end and the second end, wherein the ribs each have an inner end and an outer end that define a width therebetween, wherein the width is greater at the midpoint than at least at one of the first end and the second end such that the ribs are scalloped, wherein the length between the first end and the second end varies from a smallest length to a greatest length that differ by a delta, and wherein each of the ribs is also scalloped such that the delta is greater than the width at the midpoint, and wherein the ribs each have a leading surface and a trailing surface that define a thickness therebetween, wherein the thickness is greater at the midpoint than
at least at one of the first end and the second end such that the ribs are tapered; and
a plurality of blades that are coupled to the outer hub;
wherein each of the ribs is coupled to the outer hub in radial alignment with one of the blades.

10. The propeller according to claim 9 , wherein the propeller is configured such that the first end is farther than the second end from the marine vessel when the propeller is coupled thereto, wherein the thickness is greater at the second end than at the first end, and wherein the width is greater at the second end than at the first end.

11. The propeller according to claim 9 , wherein each of the blades has a thickest region, and wherein each of the ribs is radially aligned with the thickest region of one of the blades.

12. The propeller according to claim 9 , wherein each of the blades has a blade width divided into even thirds, and wherein each of the ribs is radially aligned with a center third of the even thirds of one of the blades.

13. The propeller according to claim 9 , wherein the blades are three individual blades, and wherein the ribs are three individual ribs.

14. The propeller according to claim 9 , further comprising forming each of the ribs to also be tapered between the inner end and the outer end such that the thickness is greater at the outer end than at the inner end.

15. The propeller according to claim 9 , wherein the propeller is formed of aluminum.

16. The propeller according to claim 9 , wherein each of the ribs has a center plane that is centrally defined between the leading surface and the trailing surface, and wherein the center plane is perpendicular to both the inner hub and the outer hub.

17. A method of making a propeller for a marine vessel, the method comprising:
forming the propeller to have blades coupled to an outer hub;
forming the propeller such that the outer hub is coupled to an inner hub via ribs, wherein the inner hub is configured to be coupled to the marine vessel, wherein the ribs each have a first end and a second end that define a length therebetween, wherein a midpoint is further defined between the first end and the second end, wherein the ribs each have an inner end and an outer end that define a width therebetween, and wherein the ribs each have a leading surface and a trailing surface that define a thickness therebetween;
forming each of the ribs to be tapered such that the thickness is greater at the midpoint than at least at one of the first end and the second end;
forming each of the ribs to be scalloped such that the width is greater at the midpoint than at least at one of the first end and the second end; and
forming the propeller such that each of the ribs is coupled to the outer hub to be radially aligned with one of the blades;
wherein the thickness decreases at a first rate between the second end and the midpoint, and the thickness decreases at a second rate between the midpoint and the first end, wherein the second rate is greater than the first rate.

18. A propeller for a marine vessel, the propeller comprising:
an inner hub configured to be coupled to the marine vessel;
an outer hub and a plurality of ribs that couple the outer hub to the inner hub, wherein the ribs each have a first end and a second end that define a length therebetween, wherein a midpoint is further defined between the first end and the second end, wherein the ribs each have an inner end and an outer end that define a width therebetween, wherein the width is greater at the midpoint than at least one of the first end and the second end such that the ribs are scalloped, and wherein the ribs each have a leading surface and a trailing surface that define a thickness therebetween, wherein the thickness is greater at the midpoint than at least one of the first end and the second end such

Assignees

• Brunswick Corp

Inventors

• Monroe Alexander K
• George Trevor
• Walker Philip R
• Guse Daniel J
• Ericson Justin D
• Worful Jason

Classifications

• B63H1/20 Primary

  Hubs; Blade connections · CPC title

• B63H20/26

  {Exhaust gas outlets} passing through the propeller or its hub · CPC title

• B63H1/14

  Propellers (pitch changing B63H3/00) · CPC title

• B63B71/00

  Designing vessels; Predicting their performance · CPC title

• B63H1/26

  Blades · CPC title