Aircraft belt loader hinge assembly having a spring loaded shock absorbing hinge support
US4610049A · kind A · utility
5Cited by
3References
7Claims
0Family size
Assignee
Inventor
Key dates
| Filing date | Sep 24, 1985 |
| Grant date | Sep 9, 1986 |
| Priority date | — |
| Expiry date | Sep 24, 2005 |
Classification
- Technology area (CPC E)Fixed Constructions
- CPC primaryE05Y2900/50
- WIPO fieldCivil engineering
- WIPO sectorOther fields
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.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.