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1. 发明申请

WO2018075414A1 MULTICOPTER WITH BOOM-MOUNTED ROTORS 审中-公开
标题翻译：带悬臂式转子的多用途飞机
公开(公告)号：WO2018075414A1
公开(公告)日：2018-04-26
申请号：PCT/US2017/056819
申请日：2017-10-16
申请人： KITTY HAWK CORPORATION
发明人： TIGHE, James, Joseph , ALLISON, Eric
IPC分类号： B64C27/26 , B64C29/00 , B64C39/04
摘要： A multicopter aircraft with boom-mounted rotors is disclosed. In various embodiments, a multicopter as disclosed herein includes a fuselage; a port side wing coupled to the fuselage; and a starboard side wing coupled to the fuselage. Each of the wings has mounted thereto one or more booms, each boom having a forward end extending forward of a corresponding wing to which the boom is mounted and an after end extending aft of said corresponding wing to which the boom is mounted. The aircraft further includes a first plurality of lift rotors, each rotor in said first plurality being mounted on a forward end of a corresponding one or said booms; and a second plurality of lift rotors, each rotor in said second plurality being mounted on an after end of a corresponding one or said booms. Each rotor produces vertical thrust independent of the thrust produced by the other rotors.
摘要翻译：披露了一种装有悬臂式转子的多用途飞机。在各种实施例中，如本文所公开的多旋翼飞行器包括机身; 联接到机身的端口侧翼; 和与机身连接的右舷侧翼。每个机翼上安装有一个或多个动臂，每个动臂具有向前延伸的前端和动臂安装到的相应机翼，后端延伸到动臂安装到的相应机翼的后部。该飞行器还包括第一多个提升转子，所述第一多个提升转子中的每个转子安装在相应的一个或所述悬臂的前端上; 以及第二多个升力转子，所述第二多个升力转子中的每个转子安装在对应的一个或所述动臂的后端上。每个转子产生垂直推力，与其他转子产生的推力无关。

2. 发明申请

WO2018075412A1 MULTICOPTER WITH ANGLED ROTORS 审中-公开
标题翻译：带有歪斜转子的多齿机
公开(公告)号：WO2018075412A1
公开(公告)日：2018-04-26
申请号：PCT/US2017/056817
申请日：2017-10-16
申请人： KITTY HAWK CORPORATION
发明人： TIGHE, James, Joseph , ALLISON, Eric
IPC分类号： B64C27/00
摘要： A multicopter with angled rotors is disclosed. In various embodiments, a multicopter as disclosed herein includes a fuselage and a plurality of rotors. At least some of the rotors are disposed on opposite sides of the fuselage and each is oriented at a corresponding angle to a substantially horizontal plane of the aircraft, the angle being of a magnitude such that a plane of rotation of the rotor does not intersect at least a critical portion of the fuselage.
摘要翻译：公开了一种具有倾斜转子的多旋翼飞行器。在各种实施例中，如本文所公开的多旋翼飞行器包括机身和多个转子。至少一些转子设置在机身的相对侧上，并且每个都以与飞机的基本上水平的平面成相应的角度定向，该角度的大小使得转子的旋转平面不与至少是机身的关键部分。

3. 发明申请

WO2018064209A1 TILT-WING AIRCRAFT 审中-公开
标题翻译：倾斜翼飞机
公开(公告)号：WO2018064209A1
公开(公告)日：2018-04-05
申请号：PCT/US2017/053796
申请日：2017-09-27
申请人： KITTY HAWK CORPORATION
发明人： KROO, Ilan , MARTINS-RIVAS, Herve , ALLISON, Eric
IPC分类号： B64C29/00 , G05D1/00
摘要： In various embodiments, a tilt-wing aircraft includes a fuselage; a first wing tiltably mounted at or near a forward end of the fuselage; and a second wing rotatably mounted to the fuselage at a position aft of the first wing. A first plurality of rotors is mounted on the first wing at locations on or near a leading edge of the first wing, with two or more rotors being mounted on wing portions on each side of the fuselage; and a second plurality of rotors mounted on the second wing at locations on or near a leading edge of the second wing, with two or more rotors being mounted on wing portions on each side of the fuselage. A flight control system generates a set of actuators and associated actuator parameters to achieve desired forces and moments.
摘要翻译：在各种实施例中，倾斜机翼飞机包括机身; 可倾斜地安装在机身的前端处或附近的第一机翼; 以及在第一机翼后方的位置可旋转地安装到机身的第二机翼。第一多个转子安装在第一机翼的前缘上或其附近的位置处的第一机翼上，其中两个或更多个转子安装在机身每侧的机翼部分上; 以及第二多个转子，所述第二多个转子在所述第二机翼的前缘上或附近的位置处安装在所述第二机翼上，并且两个或更多个转子安装在所述机身的每侧上的机翼部分上。飞行控制系统产生一组致动器和相关的致动器参数，以实现所需的力和力矩。

4. 发明公开

EP3529149A1 MULTICOPTER WITH ANGLED ROTORS 审中-公开
公开(公告)号：EP3529149A1
公开(公告)日：2019-08-28
申请号：EP17862880.6
申请日：2017-10-16
申请人： Kitty Hawk Corporation
发明人： TIGHE, James, Joseph , ALLISON, Eric
IPC分类号： B64C27/00

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