-
公开(公告)号：US11225323B2
公开(公告)日：2022-01-18
申请号：US16541561
申请日：2019-08-15
Applicant: Bell Textron Inc.
Inventor： Keith Alan Stanney , Steven Ray Ivans , Brent Chadwick Ross , Troy Bushmire
Abstract: Embodiments are directed to a rotorcraft comprising a body having a longitudinal axis, a wing coupled to the body, a single tiltrotor assembly pivotally coupled to the body, and the tiltrotor assembly configured to move between a position generally perpendicular to the longitudinal axis during a vertical flight mode and a position generally parallel to the longitudinal axis during a horizontal flight mode. The rotorcraft may further comprise an anti-torque system configured to counteract torque generated by the tiltrotor assembly during vertical flight. The rotorcraft may further comprise a center of gravity compensation system configured to manage a rotorcraft center of gravity during movement of the tiltrotor assembly between the vertical flight mode and the horizontal flight mode.
-
公开(公告)号：US20210047029A1
公开(公告)日：2021-02-18
申请号：US16541561
申请日：2019-08-15
Applicant: Bell Textron Inc.
Inventor： Keith Alan Stanney , Steven Ray Ivans , Brent Chadwick Ross , Troy Bushmire
Abstract: Embodiments are directed to a rotorcraft comprising a body having a longitudinal axis, a wing coupled to the body, a single tiltrotor assembly pivotally coupled to the body, and the tiltrotor assembly configured to move between a position generally perpendicular to the longitudinal axis during a vertical flight mode and a position generally parallel to the longitudinal axis during a horizontal flight mode. The rotorcraft may further comprise an anti-torque system configured to counteract torque generated by the tiltrotor assembly during vertical flight. The rotorcraft may further comprise a center of gravity compensation system configured to manage a rotorcraft center of gravity during movement of the tiltrotor assembly between the vertical flight mode and the horizontal flight mode.
-
Search Results
2
records
(took 0.011 seconds)
