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公开(公告)号：WO2018060970A2
公开(公告)日：2018-04-05
申请号：PCT/IB2017/056043
申请日：2017-09-29
Applicant: AMPAIRE, INC.
Inventor： COMBS, Cory Michael
Abstract: An oblique rotor-wing aircraft may be capable of vertical take-off and landing, subsonic cruise, transonic cruise, and/or supersonic cruise. The oblique rotor-wing aircraft may comprise one or more of a fuselage, a rotor-wing, a thrust-vectored propulsion system, a locking mechanism, and/or other components. The rotor-wing may be rotatably coupled to the fuselage. The rotor-wing may rotate about an axis in a first flight mode for vertical takeoff and landing. The oblique rotor-wing aircraft may include a thrust-vectored propulsion system that drives the rotation of the rotor-wing about the axis. The thrust-vectored propulsion system may include multiple, separately operable propulsion systems coupled to the rotor-wing and/or the fuselage. The oblique rotor-wing aircraft may comprise a locking mechanism that locks the rotor-wing at an angle oblique to the fuselage responsive to initiation of a second flight mode. The rotor-wing may be fixed at an angle oblique to the fuselage during the second flight mode.
Abstract translation: 倾斜的转子翼飞机可能能够垂直起飞和降落，亚音速巡航，跨音速巡航和/或超音速巡航。 倾斜转子翼飞机可以包括机身，转子翼，推力矢量推进系统，锁定机构和/或其他部件中的一个或多个。 转子翼可以可旋转地联接到机身。 转子翼可以以第一飞行模式围绕轴线旋转以垂直起飞和着陆。 倾斜转子翼飞机可以包括推进矢量推进系统，其推动转子翼绕轴线的旋转。 推力矢量推进系统可以包括联接到转子翼和/或机身的多个可单独操作的推进系统。 倾斜转子翼飞机可以包括锁定机构，该锁定机构响应于第二飞行模式的启动以相对于机身倾斜的角度锁定转子翼。 在第二次飞行模式中，转子机翼可以与机身倾斜一定角度进行固定。
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公开(公告)号：WO2018060970A3
公开(公告)日：2018-04-05
申请号：PCT/IB2017/056043
申请日：2017-09-29
Applicant: AMPAIRE, INC.
Inventor： COMBS, Cory Michael
Abstract: An oblique rotor-wing aircraft may be capable of vertical take-off and landing, subsonic cruise, transonic cruise, and/or supersonic cruise. The oblique rotor-wing aircraft may comprise one or more of a fuselage, a rotor-wing, a thrust-vectored propulsion system, a locking mechanism, and/or other components. The rotor-wing may be rotatably coupled to the fuselage. The rotor-wing may rotate about an axis in a first flight mode for vertical takeoff and landing. The oblique rotor-wing aircraft may include a thrust-vectored propulsion system that drives the rotation of the rotor-wing about the axis. The thrust-vectored propulsion system may include multiple, separately operable propulsion systems coupled to the rotor-wing and/or the fuselage. The oblique rotor-wing aircraft may comprise a locking mechanism that locks the rotor-wing at an angle oblique to the fuselage responsive to initiation of a second flight mode. The rotor-wing may be fixed at an angle oblique to the fuselage during the second flight mode.
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