Danielle D Moore

US Patent:

20210253239, Aug 19, 2021

Filed:

Feb 19, 2020

Appl. No.:

16/795426

Inventors:

- Fort Worth TX, US
Brent Chadwick Ross - Flower Mound TX, US
Danielle Lynn Moore - Arlington TX, US
Berlin Bernard Benfield - Grapevine TX, US
Jason Paul Hurst - Fort Worth TX, US

Assignee:

Bell Textron Inc. - Fort Worth TX

International Classification:

B64C 29/04
B64C 27/50
B64D 27/10
B64D 35/04
B64C 25/32
B64C 5/06
B64C 5/08
B64C 5/04
B64C 7/00

Abstract:

Embodiments are directed to a high speed, vertical lift aircraft that has vertical take-off and landing (VTOL) capability and is capable of converting to a forward-flight mode (e.g., prop-mode). The rotors blades can be folded for high speed forward flight propelled by a turbine engine (e.g., jet-mode). The rotor blades on the tail sitter aircraft have a “stop-fold” capability, which means that the rotor blades are stopped in flight and folded back to reduce drag. This allows the tail sitter aircraft to achieve a higher speed than a tilt-rotor aircraft. In some embodiments, the tail sitter aircraft achieves both rotor-borne flight and jet-borne flight by having two separate engines. An additional advantage of the tail-sitter aircraft versus a horizontally oriented fixed engine aircraft is that supplemental jet thrust can be used for take-off if desired.

US Patent:

20190031316, Jan 31, 2019

Filed:

Oct 1, 2018

Appl. No.:

16/148005

Inventors:

- Fort Worth TX, US
Dakota Charles Easley - Dallas TX, US
Danielle Lynn Moore - Fort Worth TX, US

Assignee:

Bell Helicopter Textron Inc. - Fort Worth TX

International Classification:

B64C 3/56
B64C 11/48
B64C 29/02
B64C 39/02
B64C 39/00

Abstract:

A foldable wing system for an unmanned aerial system having a fuselage includes a left wing frame having an inboard gear rotatably coupled to the fuselage, a right wing frame having an inboard gear rotatably coupled to the fuselage and a wing actuator coupled to a linkage point on at least one of the wing frames. The wing frames are movable between a plurality of positions including a deployed position and a stowed position. The inboard gear of the left wing frame is engaged with the inboard gear of the right wing frame such that the wing frames move symmetrically between the plurality of positions in response to movement of the linkage point by the wing actuator.