Trailing edge components of aircraft structures, aircraft structures comprising such trialing edge components, and methods of manufacturing such trailing edge components are provided. In an exemplary embodiment, a trailing edge component includes a first skin comprising a first plurality of plies of carbon fiber reinforced polymer material and having a first mating region. The first plurality of plies includes a first ply with a first drop-off edge in the first mating region. A second skin includes a second plurality of plies of carbon fiber reinforced polymer material and having a second mating region affixed to the first mating region.
TRAILING EDGE COMPONENTS, AIRCRAFT STRUCTURES INCLUDING TRAILING EDGE COMPONENTS AND METHODS FOR MANUFACTURING TRAILING EDGE COMPONENTS
2017-02-16
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2017
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