Braking actuator for a hydraulic brake of an aircraft wheel
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
Oct 25, 2016
Grant Date -
May 7, 2015
app pub date -
Oct 31, 2014
filing date -
Nov 4, 2013
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
A braking actuator for a hydraulic aircraft brake, received in a cavity of a ring of the brake. The actuator comprises a liner structure (1) sealed in the cavity of the ring, and a piston (3) slidably mounted in the liner structure to apply a braking force. A wear-compensating device (10) defines a retreated position of the piston in the liner structure by an axially movable stop (11) which can be advanced by the piston during the application of a braking force and in frictional relationship with a fixed part (18) of the wear-compensating device secured to the liner. An elastic member (24) returns the piston to the retreated position defined by the piston bearing against the movable stop, the movable stop being in frictional relationship with the fixed part via at least one telescopic intermediate element (16) interposed between the movable stop (11) and the fixed part (18).
First Claim
Other Claims data not available
Family
International Classification(s)
- 2014 Application Filing Year
- F16D Class
- 1365 Applications Filed
- 1201 Patents Issued To-Date
- 87.99 % Issued To-Date
Cited Art Landscape
Patent Citation Ranking
- 1 Citation Count
- F16D Class
- 26.65 % this patent is cited more than
- 9 Age
Maintenance Fees
| Fee | Large entity fee | small entity fee | micro entity fee | due date |
|---|---|---|---|---|
| 11.5 Year Payment | $7400.00 | $3700.00 | $1850.00 | Apr 25, 2028 |
