Control system for aircraft
US5527004A · kind A · utility
20Cited by
16References
20Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Jan 28, 1994 |
| Grant date | Jun 18, 1996 |
| Priority date | — |
| Expiry date | Jan 28, 2014 |
Classification
- Technology area (CPC B)Performing Operations; Transporting
- CPC primaryB64C13/0421
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A control mechanism for aircraft having a vertically extending, member with a cross bar attached to its upper end and a pair of arcuate lower members extending from the cross bar toward the forward end of the aircraft with an adjustable positioning arm on each lower member extending rearwardly and which mounts a hand grip for controlling the aircraft. The mechanism includes a damping system with a frame connected to the crossbar with bearing elements.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.