A system is described to control the flight path of a parafoil. The physical control mechanism is a series of actuators embedded within the parafoil canopy that open a series of meshed venting systems in the upper surface of the parafoil canopy. Opening and closing the meshed venting system changes the forces and moments acting on the parafoil canopy in a consistent manner such that it can be used for flight control. The meshed venting system includes an internal sealing flap and a mesh member.
In canopy bleed air actuator with mesh vent
2017-02-21
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Bleed Air Control of a Single Surface Parafoil Canopy
TIBKAT | 2022
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British Library Conference Proceedings | 2022
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AIAA | 2022
|NTIS | 1964
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