Thrust coupler
AssigneeBrunswick Corporation
InventorsJames M. Horak, Brian D. Simpson
Life of this patent
Estimating the term…
Abstract
A coupling device is provided with two flanges and a resilient annular member disposed between facing surfaces of the flanges. The resilient annular member is provided with a central opening through which a metallic spring is disposed to exert a resistive force against compression of the resilient annular member between the two flanges. The device is particularly well suited for use in a marine propulsion system because of the propulsive force exerted on the shaft system by the propeller. In one particularly preferred arrangement, each of the two flanges is provided with three holes, and the resilient annular member is provided with six holes. The two flanges are offset rotationally to place each of the holes of one flange in alignment with an interstitial space between the holes of the other flange.
Claims19
A coupler device, comprising:
- a first flange attached to a first shaft;
- a second flange attached to a second shaft, said first and second shafts being aligned generally in coaxial relation with each other;
- a resilient annular member disposed between said first and second flanges;
- and
- a metal spring disposed between said first and second flanges, said first and second flanges being fastened together to compress said resilient annular member and said metal spring therebetween said metal spring providing an axial force resisting an axial compressive force on said resilient member by said first and second shafts.
A coupler device, comprising:
- a first flange attached to a first shaft;
- a second flange attached to a second shaft, said first and second shafts being aligned generally in coaxial relation with each other;
- a resilient annular member disposed between said first and second flanges;
- and
- a metal spring disposed between said first and second flanges, said first and second flanges being fastened together to compress said resilient annular member and said metal spring therebetween, said metal spring providing an axial force resisting an axial compressive force on said resilient member by said first and second shafts, said first flange is generally triangular in shape with a first set of three holes formed therethrough, said second flange is generally triangular in shape with a second set of three holes formed therethrough, said resilient annular member has six holes formed therethrough, said first set of three holes being aligned and associated with a preselected three of said six holes to attach said first flange to said resilient annular member and the second set of three holes being aligned and associated with the remaining three of said six holes to attach said second flange to said resilient annular member.
A coupler device, comprising:
- a first flange attached to a first shaft;
- a second flange attached to a second shaft, said first and second shafts being aligned generally in coaxial relation with each other;
- a resilient annular member disposed between said first and second flanges;
- and
- a metal spring disposed between said first and second flanges, said first and second flanges being fastened together to compress said resilient annular member and said metal spring therebetween, said metal spring providing an axial force resisting an axial compressive force on said resilient member by said first and second shafts, said first flange is generally triangular in shape with a first set of three holes formed therethrough, said second flange is generally triangular in shape with a second set of three holes formed therethrough, said resilient annular member has six holes formed therethrough, said first set of three holes being aligned and associated with a preselected three of said six holes to attach said first flange to said resilient annular member and the second set of three holes being aligned and associated with the remaining three of said six holes to attach said second flange to said resilient annular member, said first shaft being an output shaft of an engine and transmission assembly, said second shaft being attached to a propeller.
Dependencies are inferred from the claim text.