An aircraft morphable aerodynamic surface structure including an elastomeric material having a glass transition temperature, a temperature management system for heating or cooling the elastomeric material, and a controller to control the temperature management system, the controller configured to control the temperature management system on the basis of a command received at the controller.
AIRCRAFT SURFACE STRUCTURE
2025-01-30
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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