Dual control mechanism for aircraft
US5427336A · kind A · utility
22Cited by
15References
19Claims
0Family size
Inventors
Key dates
| Filing date | Feb 24, 1993 |
| Grant date | Jun 27, 1995 |
| Priority date | — |
| Expiry date | Feb 24, 2013 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY10T74/20012
- WIPO fieldTransport
- WIPO sectorMechanical engineering
Abstract
A control mechanism for aircraft having a vertically extending, short stub 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. In a single control mechanism, one arcuate lower member is attached directly to the stub.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.