Example actuator assemblies to deploy aircraft leading edge flaps and seals for aircraft leading edge flaps are described herein. An example apparatus includes an aircraft flap that is movable between a stowed position and a deployed position. The flap includes a top panel. A notch is formed in the top panel and extends into a side of the top panel near a trailing edge of the flap. The example apparatus also includes a seal coupled to the flap. The seal is movable to cover the notch when the flap is in the deployed position.
Actuator assemblies to deploy aircraft leading edge flaps and seals for aircraft leading edge flaps
19.02.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
ACTUATOR ASSEMBLIES TO DEPLOY AIRCRAFT LEADING EDGE FLAPS AND SEALS FOR AIRCRAFT LEADING EDGE FLAPS
Europäisches Patentamt | 2019
|ACTUATOR ASSEMBLIES TO DEPLOY AIRCRAFT LEADING EDGE FLAPS AND SEALS FOR AIRCRAFT LEADING EDGE FLAPS
Europäisches Patentamt | 2018
|ACTUATOR ASSEMBLIES TO DEPLOY AIRCRAFT LEADING EDGE FLAPS AND SEALS FOR AIRCRAFT LEADING EDGE FLAPS
Europäisches Patentamt | 2018
|Leading-edge flaps and variable camber
Engineering Index Backfile | 1953
Leading-Edge Flaps and Variable Camber
Emerald Group Publishing | 1953