Driveshaft with a resiliently deformable cushioning...

F - Mech Eng,Light,Heat,Weapons – 16 – C

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

F16C 3/02 (2006.01) B63B 35/73 (2006.01)

Patent

CA 2351225

A watercraft includes an engine having an output shaft. A coupling structure is provided on one end of the output shaft. A driveshaft has an engine connecting axial end portion. The engine connecting end portion provides a first cooperating interlocking structure. A resiliently deformable cushioning structure has a second cooperating interlocking structure and is mounted to the engine connecting end portion with the first and second interlocking structures interlocking with one another to secure the cushioning structure on the engine connecting end portion. The coupling structure couples the output shaft and driveshaft together so that powered rotation of the output shaft is transmitted to the driveshaft. The cushioning structure is positioned between the engine connecting end portion and output shaft such that the cushioning structure prevents the engine connecting end portion from abutting directly against the output shaft during relative movement of the driveshaft and output shaft towards one another.

LandOfFree

Say what you really think

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

Rating

Driveshaft with a resiliently deformable cushioning... does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFCA-PAI-O-1866203

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