Thrust coupler

Rotary shafts – gudgeons – housings – and flexible couplings for ro – Torque transmitted via flexible element – Nonmetallic element

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

464 57, F16D 356

Patent

active

059646624

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.

REFERENCES:
patent: 1034249 (1912-07-01), Kennington
patent: 2907189 (1959-10-01), Flieg
patent: 2936625 (1960-05-01), Heiseler
patent: 3731499 (1973-05-01), Morlon
patent: 3793849 (1974-02-01), Downey
patent: 3798924 (1974-03-01), Downey
patent: 4121532 (1978-10-01), Coryell, III
patent: 5123311 (1992-06-01), Dymek
"Mechanisms & Mechanical Devices Source Book" published in 1991 by McGraw-Hill, Inc. and written by Nicholas P. Chironis; Chapter 7 is titled "Coupling, Clutching and Braking Devices".
MerCruiser Gasoline Engines Ski Models manual (90-860178970).

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Thrust coupler does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Thrust coupler, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Thrust coupler will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-646933

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.