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公开(公告)号:US20210380219A1
公开(公告)日:2021-12-09
申请号:US16894224
申请日:2020-06-05
Applicant: Bell Textron Inc.
Inventor: Tjepke Heeringa , James Everett Kooiman
Abstract: One embodiment includes a rotary aircraft, including: a rotary propulsion system; a body; and a pair of wings connected on opposite sides of the body, wherein each of the wings includes a flap rotatably connected to a trailing edge thereof and configured to rotate downward relative to the wing during low speed and stationary flight of the aircraft, and to rotate upward relative to the wing during high-speed flight of the aircraft.
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公开(公告)号:US20210309371A1
公开(公告)日:2021-10-07
申请号:US16841050
申请日:2020-04-06
Applicant: Bell Textron Inc.
Inventor: James Everett Kooiman , Jeffrey Matthew Williams , Clegg Benjamin Brian Smith , Michael E. Rinehart , Franklin Foster Caldwell , Tjepke Heeringa
Abstract: A system is described and includes a rack for carrying payload disposed in a payload bay; and a payload extension assembly for affecting linear translation of the rack between a first position in which the rack is fully retracted within the payload bay and a second position in which the payload extension assembly is fully extended and the rack is supported outside the payload bay. The payload extension assembly comprises forward and aft tracks respectively attached to forward and aft walls of the payload bay; a first stage for providing linear translation of the rack relative to the forward and aft tracks; and a second stage for providing linear translation of the rack relative to the first stage. The system further comprises a payload actuator system for selectively causing the rack extension assembly to move the rack between the first and second positions.
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