Aircraft belt loader hinge assembly having a spring loaded shock

Miscellaneous hardware (e.g. – bushing – carpet fastener – caster – Hinge – Resiliently biased hinge

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

E05F 112

Patent

active

046100490

ABSTRACT:
A hinge assembly having a polytetrafluorine block affixed to a support member with a guide rod having an enlarged head extending through a guide bore. A compression spring is trapped on the guide rod between the guide block and a nut affixed to the free end thereof. A tube is affixed to the head of a pin extending through the tube and aligned holes and a pair of ears positioned on each side of the tube and attached to the hinged member.

REFERENCES:
patent: 1340866 (1920-05-01), Witter
patent: 1467124 (1923-09-01), Sunde et al.
patent: 2420411 (1947-05-01), Blount, Sr.

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

Aircraft belt loader hinge assembly having a spring loaded shock does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Aircraft belt loader hinge assembly having a spring loaded shock, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft belt loader hinge assembly having a spring loaded shock will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-1009545

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