Aurora Flight Sciences Corporation

Meta Platforms, Inc.

Cory Kays

Kevin Uleck

Gilbert Lewis Crouse, Jr

Christopher Courtin

Evangelos Livieratos

Daniel Uhlig

An aircraft design optimization system and associated aircraft design optimization architecture. The aircraft design optimization system may comprise an input circuit to provide input data and an optimizer circuit to receive the input data and to communicate with a plurality of modules to create output data. At least one abstraction layer can be provided between the optimizer circuit and each of the plurality of modules. The optimizer circuit is configured to output the output data to a post-processing circuit. Each of the plurality of modules implements a different function.

System and method for aircraft design optimization and performance

A wing-twist aircraft having a wing, an actuation system, a sensor, and/or a controller. The wing may have a wingspan that extends to a wing tip. The wing may further include a spar aligned in a span-wise direction, wherein at least one rib is operatively coupled to the spar. The actuation system may be configured to torsionally rotate the spar, which, in turn, torsionally rotates (pivots) the at least one rib coupled to the spar, thereby twisting the wing. The sensor may be configured to measure a characteristic of the wing, while the controller may be configured to command the actuation system to torsionally rotate the spar based at least in part on input from the sensor.

Active wing-twist mechanism and control system

The present disclosure directed to an aircraft comprising one or more propulsion devices, a flexible wing, at least two tail booms having a proximal end and a distal end, the tail booms being secured to said flexible wing at the proximal end, wherein the tail booms comprise of a tail section connected at the distal end of said tail boom and wherein the tail section comprises of at least one control surface.

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Manassas, VA, United States of America

Cory Kays