Dual propeller assemblies and methods
12054234 ยท 2024-08-06
Inventors
Cpc classification
B63H5/10
PERFORMING OPERATIONS; TRANSPORTING
B63H2005/106
PERFORMING OPERATIONS; TRANSPORTING
International classification
B63H5/10
PERFORMING OPERATIONS; TRANSPORTING
B63H20/24
PERFORMING OPERATIONS; TRANSPORTING
Abstract
Dual propeller assemblies for driving engagement by a propeller drive shaft may include at least two propellers having a forward propeller and a rear propeller rearwardly of the forward propeller. The forward propeller may include a forward propeller hub with a forward propeller hub wall having a forward propeller hub outer diameter. A forward propeller hub bore may be formed by the forward propeller hub wall and configured to receive the propeller drive shaft for driving engagement of the forward propeller hub thereby. The forward propeller hub bore may form a passageway for flow of exhaust gas configured to traverse the forward propeller between the propeller drive shaft and the forward propeller hub wall. The rear propeller may include a rear propeller hub with a rear propeller hub wall having a rear propeller hub outer diameter less than the forward propeller hub outer diameter of the forward propeller hub wall of the forward propeller hub. A rear propeller hub bore may be formed by the rear propeller hub wall. The rear propeller hub bore may be configured to receive the propeller drive shaft for driving engagement of the rear propeller hub thereby. The passageway for flow of exhaust gas may be configured to traverse the rear propeller hub wall exterior to the rear propeller hub bore of the rear propeller hub.
Claims
1. A propeller assembly for driving engagement by at least one propeller drive shaft, comprising: at least two propellers comprising: a forward propeller comprising: a forward propeller hub with a forward propeller hub wall having a forward propeller hub outer diameter; a forward propeller hub bore formed by the forward propeller hub wall and configured to receive the propeller drive shaft for driving engagement of the forward propeller hub thereby, the forward propeller hub bore forming a passageway for flow of exhaust gas configured to traverse the forward propeller between the propeller drive shaft and the forward propeller hub wall; and a plurality of forward propeller blades extending from the forward propeller hub wall; and a rear propeller disposed rearwardly of the forward propeller, the rear propeller comprising: a rear propeller hub with a rear propeller hub wall having a rear propeller hub outer diameter less than the forward propeller hub outer diameter of the forward propeller hub wall of the forward propeller hub; a rear propeller hub bore formed by the rear propeller hub wall and configured to receive the propeller drive shaft for driving engagement of the rear propeller hub thereby, the passageway for flow of exhaust gas configured to traverse the rear propeller hub wall exterior and to the rear propeller hub bore of the rear propeller hub; and a plurality of rear propeller blades extending from the rear propeller hub wall.
2. The propeller assembly of claim 1 wherein at least one of the forward propeller hub wall of the forward propeller hub and the rear propeller hub wall of the rear propeller hub is tapered.
3. The propeller assembly of claim 2 wherein each of the forward propeller hub wall of the forward propeller hub and the rear propeller hub wall of the rear propeller hub is tapered.
4. The propeller assembly of claim 3 wherein the forward propeller hub wall of the forward propeller hub has a fore hub end with a forward hub fore end diameter and an aft hub end with a forward hub aft end diameter, and difference in diameter between the forward hub fore end diameter and the forward hub aft end diameter is 50%; and wherein the rear propeller hub wall of the rear propeller hub has a fore hub end with a rear hub fore end diameter and an aft hub end with a rear hub aft end diameter, and difference in diameter between the rear hub fore end diameter and the rear hub aft end diameter is 50%.
5. The propeller assembly of claim 1 wherein the rear propeller hub outer diameter of the rear propeller is about 20%-50% less than the forward propeller hub outer diameter of the forward propeller.
6. The propeller assembly of claim 5 wherein the rear propeller hub outer diameter of the rear propeller is about 50% less than the forward propeller hub outer diameter of the forward propeller.
7. The propeller assembly of claim 1 wherein the passageway for flow of the exhaust gas is completely exterior to the rear propeller hub wall of the rear propeller hub.
8. The propeller assembly of claim 1 wherein the passageway for flow of the exhaust gas is split partially over the rear propeller blades of the rear propeller and through the rear propeller hub bore of the rear propeller.
9. A propeller assembly for driving engagement by a propeller drive assembly having a main propeller drive shaft and an outer propeller drive shaft and an inner propeller drive shaft drivingly engaged for rotation by the main propeller drive shaft, the propeller assembly comprising: at least two propellers comprising: a forward propeller configured for driving engagement by the outer propeller drive shaft, the forward propeller comprising: a forward propeller hub with a forward propeller hub wall having a forward propeller hub outer diameter; a forward propeller hub bore formed by the forward propeller hub wall and configured to receive the outer propeller drive shaft for driving engagement of the forward propeller hub thereby, the forward propeller hub bore forming a passageway for flow of exhaust gas configured to traverse the forward propeller between the outer propeller drive shaft and the forward propeller hub wall; and a plurality of forward propeller blades extending from the forward propeller hub wall; and a rear propeller disposed rearwardly of the forward propeller and configured for driving engagement by the inner propeller drive shaft, the rear propeller comprising: a rear propeller hub with a rear propeller hub wall having a rear propeller hub outer diameter about 20%-50% less than the forward propeller hub outer diameter of the forward propeller hub wall of the forward propeller hub; a rear propeller hub bore formed by the rear propeller hub wall and configured to receive the inner propeller drive shaft for driving engagement of the rear propeller hub thereby, the passageway for flow of exhaust gas configured to traverse the rear propeller hub wall exterior and to the rear propeller hub bore of the rear propeller hub; and a plurality of rear propeller blades extending from the rear propeller hub wall.
10. The propeller assembly of claim 9 wherein at least one of the forward propeller hub wall of the forward propeller hub and the rear propeller hub wall of the rear propeller hub is tapered.
11. The propeller assembly of claim 10 wherein each of the forward propeller hub wall of the forward propeller hub and the rear propeller hub wall of the rear propeller hub is tapered.
12. The propeller assembly of claim 11 wherein the forward propeller hub wall of the forward propeller hub has a fore hub end with a forward hub fore end diameter and an aft hub end with a forward hub aft end diameter, and difference in diameter between the forward hub fore end diameter and the forward hub aft end diameter is 50%; and wherein the rear propeller hub wall of the rear propeller hub has a fore hub end with a rear hub fore end diameter and an aft hub end with a rear hub aft end diameter, and difference in diameter between the rear hub fore end diameter and the rear hub al end diameter is 50%.
13. The propeller assembly of claim 9 wherein the rear prop hub outer diameter of the rear propeller is about 50% less than the forward prop hub outer diameter of the forward propeller.
14. The propeller assembly of claim 9 wherein the passageway for flow of the exhaust gas is completely exterior to the rear propeller hub wall of the rear propeller hub.
15. The propeller assembly of claim 9 wherein the passageway for flow of the exhaust gas is split partially over the rear propeller blades of the rear propeller and the rear propeller hub bore of the rear propeller.
16. The propeller assembly of claim 9 further comprising a front prop nut configured for securing the forward propeller on the outer propeller drive shaft and a rear prop nut configured for securing the rear propeller on the inner propeller drive shaft of the propeller drive assembly.
17. A propeller assembly for driving engagement by a propeller drive assembly having a main propeller drive shaft and an outer propeller drive shaft and an inner propeller drive shaft drivingly engaged for rotation by the main propeller drive shaft, the propeller assembly comprising: at least two propellers comprising: a forward propeller configured for driving engagement by the outer propeller drive shaft, the forward propeller comprising: a forward propeller hub with a forward propeller hub wall having a forward propeller hub outer diameter; a forward propeller hub bore formed by the forward propeller hub wall and configured to receive the outer propeller drive shaft for driving engagement of the forward propeller hub thereby, the forward propeller hub bore forming a passageway for flow of exhaust gas configured to traverse the forward propeller between the outer propeller drive shaft and the forward propeller hub wall; and a plurality of forward propeller blades extending from the forward propeller hub wall; and a rear propeller disposed rearwardly of the forward propeller and configured for driving engagement by the inner propeller drive shaft, the rear propeller comprising: a rear propeller hub with a rear propeller hub wall having a rear propeller hub outer diameter about 50% less than the forward propeller hub outer diameter of the forward propeller hub wall of the forward propeller hub; a rear propeller hub bore formed by the rear propeller hub wall and configured to receive the inner propeller drive shaft for driving engagement of the rear propeller hub thereby, the passageway for flow of exhaust gas configured to traverse the rear propeller hub wall exterior and to the rear propeller hub bore of the rear propeller hub; and a plurality of rear propeller blades extending from the rear propeller hub wall.
18. The propeller assembly of claim 17 wherein each of the forward propeller hub wall of the forward propeller hub and the rear propeller hub wall of the rear propeller hub is tapered, the forward propeller hub wall of the forward propeller hub having a fore hub end with a forward hub fore end diameter and an aft hub end with a forward hub aft end diameter, and difference in diameter between the forward hub fore end diameter and the forward hub aft end diameter is 50%; and wherein the rear propeller hub wall of the rear propeller hub has a fore hub end with a rear hub fore end diameter and an aft hub end with a rear hub aft end diameter, and difference in diameter between the rear hub fore end diameter and the rear hub aft end diameter is 50%.
19. The propeller assembly of claim 17 wherein the passageway for flow of the exhaust gas is completely exterior to the rear propeller hub wall of the rear propeller hub.
20. The propeller assembly of claim 17 wherein the passageway for flow of the exhaust gas is split partially over the rear propeller blades of the rear propeller and the rear propeller hub bore of the rear propeller.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) Illustrative embodiments of the disclosure will now be described, by way of example, with reference to the accompanying drawings, in which:
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DETAILED DESCRIPTION
(8) The following detailed description is merely exemplary in nature and is not intended to limit the described embodiments or the application and uses of the described embodiments. As used herein, the word exemplary or illustrative means serving as an example, instance, or illustration. Any implementation described herein as exemplary or illustrative is not necessarily to be construed as preferred or advantageous over other implementations. All of the implementations described below are exemplary implementations provided to enable persons skilled in the art to make or use the embodiments of the disclosure and are not intended to limit the scope of the disclosure, which is defined by the claims. For purposes of description herein, the terms upper, lower, left, rear, right, front, vertical, horizontal, and derivatives thereof shall relate to the invention as oriented in
(9) Referring initially to
(10) As further illustrated in
(11) Multiple forward propeller blades 7 may extend outwardly from the forward propeller hub wall 8 of the forward propeller hub 3. The forward propeller blades 7 may be oriented to propel the forward propeller 2 forwardly in the body of water as it rotates in the clockwise or counterclockwise first rotational direction and rearwardly in the body of water as it rotates in the opposite clockwise or counterclockwise first rotational direction.
(12) As further illustrated in
(13) The rear propeller 32 of the propeller assembly 1 may have a rear propeller hub 33. The rear propeller hub 33 may have a rear propeller hub wall 38 which may be elongated and generally cylindrical. The rear propeller hub wall 38 may have a fore hub end 34 and an aft hub end 35. As illustrated in
(14) As further illustrated in
(15) As illustrated in
(16) An illustrative tapered prop embodiment of the dual prop apertured propeller assemblies 1 is illustrated in
(17) As illustrated in
(18) As further illustrated in
(19) The inner shaft drive gear 73 and the outer shaft drive gear 77 may be housed inside a gearcase 90. A gearcase labyrinth seal 91 may be disposed between the forward propeller 2 and the gearcase 90. The fore hub end 4 of the forward propeller 2 may interface with the gearcase labyrinth seal 91. The forward prop hub diameter 58 (
(20) In typical application, the dual prop propeller assembly 1 may be assembled on the marine vehicle (not illustrated) to propel the marine vehicle on a body of water. Accordingly, the forward propeller 2 and the rear propeller 32 of the propeller assembly 1 may be disposed in driving engagement with the inner propeller drive shaft 72 and the outer propeller drive shaft 76, respectively, typically as was heretofore described. The propeller assembly 1 may be immersed in the body of water as the marine vehicle is placed thereon. Responsive to operation of the motor (not illustrated) of the marine vehicle, the main propeller drive shaft 71 of the propeller drive assembly 70 may simultaneously rotate the outer propeller drive shaft 76 and the inner propeller drive shaft 72 in the respective first and second clockwise and counterclockwise rotational directions. The front propeller 2 and the rear propeller 32 may responsively rotate in the respective corresponding first and second rotational directions as the forward propeller blades 7 on the forward propeller 2 and the rear propeller blades 37 on the rear propeller 32 propel the propeller assembly 1 and the marine vehicle on the water.
(21) As illustrated in
(22) It will be appreciated by those skilled in the art that the dual prop embodiment of the propeller assembly 1 may eliminate or substantially minimize steering torque to the marine vehicle since the rotational forces of the forward propeller 2 and the rear propeller 32 largely offset each other. The propeller assembly 1 may provide several advantages over standard or conventional dual prop designs. For example, in conventional dual props in which the forward propeller and the rear propeller have the same outer hub diameters basically matching the gearcase diameter (commonly known as through hub propeller style with an integral internal exhaust passageway), the extended running surface of the propeller hubs may tend to create a pronounced ski effect, causing the marine vehicle to run stern high. On marine vehicles which require a bow high running attitude, this extended running surface may lead to handling and performance issues. Moreover, the conventional method of routing the motor exhaust over the forward and rear propellers of like hub diameter (known typically as an overhub exhaust type propeller with no internal passageway) tends not to restrain the exhaust, but rather, routes the exhaust onto the blade surfaces, thus tending to produce ventilation, especially in initial planing and high speed cornering maneuvers of the marine vehicle. The dual prop propeller assembly 1 may utilize a through hub exhaust forward propeller 2 having the relatively large forward propeller hub diameter 58 (
(23) While certain illustrative embodiments of the disclosure have been described above, it will be recognized and understood that various modifications can be made to the embodiments and the appended claims are intended to cover all such modifications which may fall within the spirit and scope of the disclosure.