AIRCRAFT THROTTLE CONTROL SYSTEM WITH AN EMITTER UNIT AND A RECEIVER UNIT
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
N/A
Issued Date -
Jun 11, 2015
app pub date -
Dec 3, 2014
filing date -
Dec 4, 2013
priority date (Note) -
Published
status (Latency Note)
Importance
Abstract
An aircraft throttle control system having a control lever. The control system comprises an emitter unit having the pivot-mounted control lever and a receiver unit having a pivot-mounted lever, and a linkage connecting the control lever to the lever, and transmitting movement between the control lever and the lever. That makes it possible to optimize the space in a flight deck and typically makes it possible to dispense with the central pedestal generally present in the middle of flight decks while at the same time maintaining conventional ergonomics for controlling the throttle for example. A flight deck element is also disclosed having a fixed structure to which the control system is rigidly connected, to an associated flight deck and to an aircraft equipped with such a flight deck.
First Claim
Family
International Classification(s)
- [Classification Symbol]
- [Patents Count]
Cited Art Landscape
Patent Citation Ranking
Advertisement
Advertisement
Advertisement
Recipient Email Address
Recipient Email Address
Comment
Recipient Email Address
Add to Portfolio(s)
To add this patent to one, or more, of your portfolios, simply click the add button.
This Patent is in these Portfolios:
Add to additional portfolios:
Last Refreshed On:
Changes done successfully