Propeller hub

Information

  • Patent Grant
  • 6609892
  • Patent Number
    6,609,892
  • Date Filed
    Tuesday, November 21, 2000
    23 years ago
  • Date Issued
    Tuesday, August 26, 2003
    21 years ago
Abstract
A propeller assembly that includes a plastic bushing that is secured, e.g., bonded, to an inner hub and is configured to engage an outer hub of a propeller. More specifically, and in an exemplary embodiment, the bushing includes a cylindrical shaped body having a bore therethrough, and a plurality of grooves are in an outer diameter surface of the cylindrical shaped body. The inner hub includes a cylindrical shaped body sized to extend into the bushing bore. A flange is at one end of the inner hub body, and at least one limp home tab extends from the flange. The propeller includes an outer hub having a cylindrical shaped body, and a plurality of blades extend from an outer diameter surface of the outer hub body. An inner diameter surface of the outer hub body has a plurality of protrusions that extend radially inward. Each protrusion is positioned to extend within a respective one of the grooves in the outer diameter surface of the bushing body. At least one limp home tab extends from the outer hub inner diameter surface.
Description




BACKGROUND OF THE INVENTION




The invention relates generally to marine engines, and more particularly, to propeller hubs.




Outboard engines include a drive shaft which extends from the engine power head, through an exhaust case, and into an engine lower unit. The lower unit includes a gear case, and a propeller shaft extends through the gear case. Forward and reverse gears couple the propeller shaft to the drive shaft. The drive shaft, gears, and propeller shaft sometimes are referred to as a drive train.




A propeller is secured to and rotates with the propeller shaft. Torque from the engine is transmitted from the propeller shaft to the propeller. Exemplary propeller hub assemblies include cross bolts, keys, shear pins, plastic hubs, and compressed rubber hubs. Such hub assemblies should have sufficient strength or stiffness so that during normal engine operations, very few losses occur between the propeller shaft and the propeller. Such hub assemblies, however, also should be resilient so that the engine drive train is protected in the event of an impact, e.g., if the propeller hits a log or rock.




A propeller hub assembly also should facilitate “limp home” operation of the engine so that even in the event that an interface between the propeller shaft and the propeller shears due to a large impact, the propeller and propeller shaft still remain sufficiently engaged so that the engine still drives the boat, for example, to return to a dock for repairs.




BRIEF SUMMARY OF THE INVENTION




In an exemplary embodiment, a propeller assembly includes a plastic bushing secured, e.g., bonded, to an inner hub and configured to engage an outer hub of a propeller. More specifically, and in an exemplary embodiment, the bushing includes a cylindrical shaped body having a bore therethrough, and a plurality of grooves are in an outer diameter surface of the cylindrical shaped body. The inner hub includes a cylindrical shaped body sized to extend into the bushing bore. A flange is at one end of the inner hub body, and at least one limp home tab extends from the flange.




The propeller includes an outer hub having a cylindrical shaped body, and a plurality of blades extend from an outer diameter surface of the outer hub body. An inner diameter surface of the outer hub body has a plurality of protrusions that extend radially inward. Each protrusion is positioned to extend within a respective one of the grooves in the outer diameter surface of the bushing body. Also, at least one limp home tab extends from the outer hub inner diameter surface.




Generally, the propeller assembly rotates with the propeller shaft during normal operations. In the event of an impact, e.g., the propeller strikes an object in the water, the propeller may rotate relative to the shaft. Specifically, in the exemplary embodiment, since the torsion bushing is plastic and outer hub is stainless steel, the outer hub may rotate relative to the bushing.




In the event that such relative rotation of the propeller results in shearing the engagement between the propeller and the torsion bushing, a limp home arrangement provides that the propeller may still be rotatable with the propeller shaft so that the operator can at least reach a dock for repairs. The limp home arrangement includes the outer hub tabs and the inner hub tabs. Once the propeller outer hub rotates so that the outer hub tabs engage the inner hub tabs, the outer hub once again rotates with the propeller shaft. Such operational condition is sometimes referred to herein as the limp home operation mode.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a front exploded view of the propeller assembly shown in FIG.


1


.





FIG. 2

is a rear exploded view of the propeller assembly shown in FIG.


3


.





FIG. 3

is a front perspective view of a propeller assembly in accordance with one embodiment of the present invention.





FIG. 4

is a rear perspective view of the propeller assembly shown in FIG.


1


.





FIG. 5

is a front view of the propeller assembly shown in FIG.


1


.





FIG. 6

is a rear view of the propeller assembly shown in FIG.


1


.





FIG. 7

is a cross-sectional view through line


7





7


shown in FIG.


5


.





FIG. 8

is a cross-sectional view through line


8





8


shown in FIG.


7


.











DETAILED DESCRIPTION OF THE INVENTION




The present invention is not limited to practice in connection with a particular engine, nor is the present invention limited to practice with a particular propeller configuration. The present invention can be utilized in connection with many engines and propeller configurations. For example, a propeller having three blades is described herein. The present invention, however, can be used in connection with propellers having any number of blades. Therefore, although the invention is described below in the context of an exemplary outboard engine and propeller configuration, the invention is not limited to practice with such engine and propeller.





FIG. 1

is a front exploded view of a propeller assembly


100


in accordance with one embodiment of the present invention, and

FIG. 2

is a rear exploded view of assembly


100


. Propeller assembly


100


is configured for being secured to a propeller shaft


102


of a marine engine. Propeller assembly


100


includes a thrust bushing


104


and a propeller


106


having an outer hub


108


with a cylindrical shaped body. A plurality of blades


110


extend from an outer diameter hub surface


112


. Assembly


100


further includes a torsion bushing


114


and an inner hub


116


. A washer


118


and a nut


120


secure assembly


100


to propeller shaft


102


.




Torsion bushing


114


includes a plurality of grooves


122


that mate with drive protrusions


124


that extend radially inward from an inner diameter surface


126


of outer hub


108


. More specifically, a bore


128


extends through outer hub


108


. Each protrusion


124


is positioned to extend within a respective one of grooves


122


.




Bushing


114


includes a cylindrical shaped body


130


having a bore


132


therethrough. Grooves


122


are in an outer diameter surface


134


of cylindrical shaped body


130


. Bushing


114


slides into outer hub bore


128


so that protrusions


124


are located within grooves


122


. Outer hub


108


also includes a plurality of tabs


136


that, under certain operating conditions as described below in more detail, engage tabs


138


that extend from a flange


140


of inner hub


116


.




Inner hub


116


slides into bore


132


of bushing


114


and is securely engaged to bushing


114


, e.g., by a bonding process, such as by a vulcanizing process or other bonding process known in the art. Specifically, inner hub cylindrical shaped body


142


extends into bushing bore


132


.




In the exemplary embodiment described above, propeller shaft


102


is fabricated from steel, thrust bushing


104


is stainless steel, propeller


106


is stainless steel, torsion bushing


114


is a plastic, e.g., urethane, and inner hub


116


is stainless steel. Of course, such components can be fabricated from other materials, e.g., brass, aluminum, selected depending upon the desired operating characteristics of assembly


100


.





FIG. 3

is a front perspective view of propeller assembly


100


, and

FIG. 4

is a rear perspective view of assembly


100


. Generally, propeller assembly


100


rotates with propeller shaft


102


during normal operations. In the event of an impact, e.g., propeller


106


strikes an object in the water, propeller


106


may rotate relative to shaft


102


. Specifically, in the exemplary embodiment, since torsion bushing


114


is plastic and outer hub


108


is stainless steel, outer hub


108


may rotate relative to bushing


114


as described below.




In the event that such relative rotation of propeller


106


results in shearing the engagement between propeller


106


and torsion bushing


114


, a limp home arrangement provides that propeller


106


may still be rotatable with propeller shaft


102


so that the operator can at least reach a dock for repairs. The limp home arrangement includes outer hub tabs


136


and inner hub tabs


138


. Once propeller outer hub


108


rotates so that outer hub tabs


136


engage inner hub tabs


138


, outer hub


108


once again rotates with propeller shaft


102


. Such operational condition is sometimes referred to herein as the limp home operation mode.





FIG. 5

is a front view of assembly


100


, and

FIG. 6

is a rear view of assembly


100


. As shown in

FIG. 5

, inner hub


116


includes a central shaft supporting sleeve


144


having a bore


146


therethrough, and support ribs


148


′ extend from sleeve


144


to an inner wall


150


of hub


116


. Propeller shaft


102


extends through bore


146


.




As shown in

FIG. 6

, nut


120


is tightened to shaft


102


and engages shaft


102


to propeller


106


. As a result, propeller


106


rotates with shaft


102


during normal engine operations. Also, in an initial operative position, outer hub tabs


136


are radially spaced from inner hub tabs


138


. In the event propeller


106


rotates relative to inner hub


116


, e.g., upon an impact with an object in the water, then such relative rotation may continue until tabs


136


and


138


are in contact. Once tabs


136


and


138


are in contact, propeller


106


once again rotates with inner hub


116


and propeller shaft


102


, i.e., the limp home operation mode.





FIG. 7

is a cross-sectional view through line


7





7


shown in FIG.


5


. As shown in

FIG. 7

, torsion bushing


114


is tapered which facilitates secure engagement between bushing


114


and outer hub


108


. In addition, and although not shown in

FIG. 7

, propeller shaft


102


has longitudinal splines that extend from an end


152


of shaft


102


. The propeller shaft splines mate with grooves in an inner diameter surface


154


of sleeve


144


and facilitate secure engagement between inner hub


114


and propeller shaft


102


.





FIG. 8

is a cross-sectional view through line


8





8


shown in FIG.


7


. As shown in

FIG. 8

, protrusions


124


extend into grooves


122


in bushing


114


. Angles A, B, C, D, and E, in the exemplary embodiment, are as set forth below subject to manufacturing tolerances.




Angle A as illustrated in

FIG. 8

is an angle between a first side of bushing groove


122


and an edge of an inner hub support rib


148


. In an illustrative embodiment Angle A is about 12.8°.




Angle B as illustrated in

FIG. 8

is an angular difference between a first side of a bushing grove


122


and a first side of one of the outer hub protrusions


124


. In an illustrative embodiment Angle B is approximately 0.0181pi radians (approximately 1.04°).




Angle C as illustrated in

FIG. 8

is an angular difference between a second side of a bushing grove


122


and a second side of one of the outer hub protrusions


124


. In an illustrative embodiment Angle C is approximately 0.0181 pi radians (approximately 1.04°).




Angle D as illustrated in

FIG. 8

is an angular difference between a first side of one of the outer hub protrusions


124


and a second side of the outer hub protrusion


124


. In an illustrative embodiment Angle C is approximately 7.0°.




Angle E as illustrated in

FIG. 8

is an angular difference between a first side of a bushing grove


122


and a second side the bushing groove


122


. In an illustrative embodiment Angle E is approximately 8.5°.




Upon the occurrence of an impact, inner hub


116


continues to rotate with propeller shaft


102


. In the event that sufficient force is present, protrusions


124


shear which results in propeller shaft


102


rotating relative to propeller


106


. If the forces are not sufficient to also shear limp home tabs


136


and


138


, then propeller


106


will resume rotating with propeller shaft


102


.




Different inner hub and torsion bushing combinations can be used with one propeller so that one propeller can be utilized on many different types of marine engines. For example, one particular marine engine may have splines on the propeller shaft of a first length, and another particular marine engine may have splines on a propeller shaft of a second length, or a different number of splines or different size splines. Different inner hubs having sleeves with different length splines can be provided. Although different inner hub and torsion bushings are utilized, a same propeller can be used. That is, by providing interchangeable inner hub and torsion bushing sub-assemblies, one propeller can be used in conjunction with many different type engines.




It is contemplated that inner hub and torsion busing bushing subassemblies could be sold in kit form. For example, different kits containing different sub-assemblies specified for particular engine types could be provided. In one specific embodiment, a kit includes at least one such sub-assembly and a propeller that can be used with sub-assembly included in the kit as well as with other subassemblies.




From the preceding description of various embodiments of the present invention, it is evident that the objectives of the invention are attained. Although the invention has been described and illustrated in detail, it is to be clearly understood that the same is intended by way of illustration and example only and is not to be taken by way of limitation. Accordingly, the spirit and scope of the invention are to be limited only by the terms of the appended claims.



Claims
  • 1. A propeller assembly for being secured to a propeller shaft of a marine engine, said propeller assembly comprising:a bushing comprising a cylindrical shaped body having a bore therethrough; an inner hub comprising a cylindrical shaped body sized to extend into said bushing bore and at least one tab extending therefrom; a propeller comprising an outer hub comprising a cylindrical shaped body, a plurality of blades extending from an outer diameter surface of said outer hub body; and at least one limp home tab radially extending from a side of the outer hub in the axial direction.
  • 2. A propeller assembly in accordance with claim 1 wherein said bushing and said inner hub are secured together.
  • 3. A propeller assembly in accordance with claim 2 wherein said bushing and said inner hub are secured together by a bonding process.
  • 4. A propeller assembly in accordance with claim 1 wherein said bushing is fabricated from plastic.
  • 5. A propeller assembly in accordance with claim 1, said bushing comprising a plurality of grooves in an outer diameter surface of said cylindrical shaped body.
  • 6. A propeller assembly in accordance with claim 5 wherein an inner diameter surface of said outer hub body comprises a plurality of protrusions extending radially inward, each said protrusion positioned to extend within a respective one of said grooves in said outer diameter surface of said bushing body.
  • 7. A propeller assembly in accordance with claim 1, said inner hub comprising a flange at one end of said inner hub body, and at least one tab extending therefrom.
  • 8. An interchangeable bushing and inner hub subassembly for a propeller assembly to secure a propeller to a propeller shaft, said subassembly comprising a bushing comprising a cylindrical shaped body having a bore therethrough, and an inner hub comprising a cylindrical shaped body sized to extend into said bushing bore, wherein the cylindrical shaped body of the inner hub is sized such that upon positioning of the inner hub within the bushing, the body of the inner hub extends at least an entire length of the body of the bushing; andat least one tab extending radially outwardly from an end of said inner hub body.
  • 9. A subassembly in accordance with claim 8 wherein said bushing and said inner hub are secured together.
  • 10. A subassembly in accordance with claim 9 wherein said bushing and said inner hub are secured together by a bonding process.
  • 11. A subassembly in accordance with claim 8 wherein said bushing is fabricated from plastic.
  • 12. A subassembly in accordance with claim 8 wherein said inner hub further comprising a sleeve having a bore therethrough, a plurality of grooves in an inner diameter surface of said sleeve configured to mate with splines extending from an outer diameter surface of the propeller shaft.
  • 13. A subassembly in accordance with claim 12 wherein a longitudinal length of said grooves in said inner diameter surface of said sleeve is selected based on a length of the splines extending from the outer diameter surface of the propeller shaft.
  • 14. An interchangeable bushing and inner hub assembly in accordance with claim 8, said bushing comprising a plurality of grooves in an outer diameter surface of said bushing cylindrical shaped body.
  • 15. An interchangeable bushing and inner hub assembly in accordance with claim 8, said inner hub body comprising a flange at one end thereof, said at least one tab extending from said flange.
  • 16. A kit for securing a propeller to a propeller shaft of a marine engine, said kit comprising:a bushing comprising a cylindrical shaped body having a bore therethrough, and an inner hub comprising a cylindrical shaped body sized to extend into said bushing bore such that the cylindrical body of the inner hub extends past the cylindrical body of the bushing, said inner hub comprising a flange at one end of said inner hub body, and at least one tab radially extending from said flange.
  • 17. A kit in accordance with claim 16 wherein the cylindrical shaped body of the inner hub comprises a plurality of grooves in an outer diameter surface.
  • 18. A kit assembly in accordance with claim 16 wherein said bushing and said inner hub are secured together.
  • 19. A kit in accordance with claim 18 wherein said bushing and said inner hub are secured together by a bonding process.
  • 20. A kit in accordance with claim 16 wherein said bushing is fabricated from plastic.
  • 21. A propeller assembly for being secured to a propeller shaft of a marine engine, said propeller assembly comprising:means for engaging the propeller shaft; a propeller comprising an outer hub comprising a cylindrical shaped body, and a plurality of blades extending from an outer diameter surface of said outer hub body, a bore extending through said propeller, and a plurality of protrusions extending radially inward from an inner diameter surface of said outer hub body; means intermediate said propeller shaft engaging means and said propeller, said intermediate means secured to said engaging means, said intermediate means comprising a plurality of grooves that mate with said plurality of protrusions; and at least one limp home tab extending from a side of the outer hub in the axial direction.
  • 22. A propeller assembly in accordance with claim 21 wherein said engaging means comprises an inner hub comprising a cylindrical shaped body, a flange at one end of said inner hub body, and at least one tab extending from said flange.
  • 23. A propeller assembly in accordance with claim 22 wherein said intermediate means comprises a bushing comprising a cylindrical shaped body have a bore therethrough, said plurality of grooves in an outer diameter surface of said cylindrical shaped body.
  • 24. A propeller assembly in accordance with claim 21 wherein said engaging means and said intermediate means secured together by a bonding process.
  • 25. A propeller assembly in accordance with claim 21 wherein said intermediate means is fabricated from plastic.
  • 26. A propeller assembly for being secured to a propeller shaft of a marine engine, said propeller assembly comprising:an inner hub comprising a cylindrical shaped body, a flange at one end of said inner hub body, and at least one tab extending from said flange; a propeller comprising an outer hub comprising a cylindrical shaped body, a plurality of blades extending from an outer diameter surface of said outer hub body, an inner diameter surface of said outer hub body having a plurality of protrusions extending radially inward and,at least one limp home tab, an engagement member for coupling said propeller to said inner hub and causing said propeller and said hub to rotate together, said limp home tab configured to engage said at least one tab of said flange and rotate said propeller when said engagement member fails.
  • 27. A propeller assembly in accordance with claim 26 said engagement member comprises a torsion bushing.
  • 28. A propeller assembly in accordance with claim 27 wherein said torsion bushing comprises a cylindrical shaped body having a bore therethrough, and a plurality of grooves in an outer diameter surface of said cylindrical shaped body.
  • 29. A propeller assembly in accordance with claim 28, each said outer hub body protrusion positioned to extend within a respective one of said grooves in said outer diameter surface of said bushing body.
  • 30. A propeller assembly in accordance with claim 29 wherein said bushing is bonded to said inner hub.
  • 31. An interchangeable bushing and inner hub subassembly for a propeller assembly to secure a propeller to a propeller shaft, said subassembly comprising a bushing comprising a cylindrical shaped body having a bore therethrough, and an inner hub comprising a cylindrical shaped body sized to extend into said bushing bore and at least one tab extending radially outwardly from an end of said inner hub body; andwherein said inner hub further comprises a sleeve having a bore therethrough, a plurality of grooves in an inner diameter surface of said sleeve configured to mate with splines extending from an outer diameter surface of the propeller shaft.
  • 32. A subassembly in accordance with claim 31 wherein a longitudinal length of said grooves in said inner diameter surface of said sleeve is selected based on a length of the splines extending from the outer diameter surface of the propeller shaft.
US Referenced Citations (20)
Number Name Date Kind
3589833 Lancioni Jun 1971 A
3999887 McGuire Dec 1976 A
4097191 Genuardi Jun 1978 A
4507091 Govan Mar 1985 A
4566855 Costabile et al. Jan 1986 A
4826404 Zwicky May 1989 A
5184945 Chi-Wei Feb 1993 A
5201679 Velte, Jr. et al. Apr 1993 A
5244348 Karls et al. Sep 1993 A
5252028 LoBosco et al. Oct 1993 A
5322416 Karls et al. Jun 1994 A
5476284 DuRocher et al. Dec 1995 A
5484264 Karls et al. Jan 1996 A
5527153 Bernhardt Jun 1996 A
5573372 Badger Nov 1996 A
5630704 Gilgenbach et al. May 1997 A
5647810 Huddleston Jul 1997 A
5967751 Chen Oct 1999 A
6177742 Lauk et al. Jan 2001 B1
6383042 Neisen May 2002 B1