Aircraft engine exhaust flap curved strut slot
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
May 25, 2010
Grant Date -
Feb 15, 2007
app pub date -
Aug 10, 2005
filing date -
Aug 10, 2005
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
An aircraft engine nozzle assembly includes an adjustable flap portion that is movable about a pivot for changing the size of an exhaust exit area. A bracket having a curved slot establishes a range of possible movement of the flap portion. A link includes a guide member portion that is received in the curved slot for guiding the movement of the flap portion. The link is connected to a static engine structure and the bracket is movable with the flap portion. The curved slot establishes a range of possible movement of the flap portion along a direction of the curved slot.
First Claim
Family
International Classification(s)
Cited Art Landscape
Patent Citation Ranking
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