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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

WO2018236383A1 COMPOSITE STRUCTURE WITH INTEGRATED HINGE 审中-公开
公开(公告)号：WO2018236383A1
公开(公告)日：2018-12-27
申请号：PCT/US2017/038818
申请日：2017-06-22
申请人： KITTY HAWK CORPORATION
发明人： VAN PELT, Chris , TIGHE, James, Joseph
IPC分类号： B32B5/28 , E05D1/02
摘要： A composite structure with an integrated hinge is disclosed. In various embodiments, the composite structure includes a plurality of layers of fiber reinforced polymer material; and a hinge structure comprising one or more layers of bendably flexible hinge material a first region of which is interleaved between adjacent layers of said layers of fiber reinforced polymer material comprising the composite structure and bonded to said adjacent layers by bonding material comprising said composite structure, and a second region of which extends beyond said layers of fiber reinforced polymer material comprising the composite structure.

4. 发明申请

WO2018075413A1 VENTILATED ROTOR MOUNTING BOOM FOR PERSONAL AIRCRAFT 审中-公开
标题翻译：用于个人飞机的通风转子安装臂
公开(公告)号：WO2018075413A1
公开(公告)日：2018-04-26
申请号：PCT/US2017/056818
申请日：2017-10-16
申请人： KITTY HAWK CORPORATION
发明人： TIGHE, James, Joseph , LONG, Geoffrey, Alan , TZARNOTZKY, Uri
IPC分类号： B64C29/00 , B64D27/24 , B64D27/26 , B64D33/10
摘要： Described embodiments provide a rotor mounting boom assembly for a personal aircraft. The rotor mounting boom assembly includes a rotor mounting boom releasably attachable to a wing of the personal aircraft, one or more vertical lift rotors, and one or more rotor controller assemblies. Controller assemblies for each rotor are positioned on the rotor mounting booms such that downwash from the rotor causes increased airflow across the controller assembly to cool the controller assembly components. A rotor controller enclosure includes an air inlet and an air outlet to allow airflow through the enclosure to cool the controller components. The air inlet is positioned relative to the path of the rotor blades such that the downwash from the rotor that flows into the air inlet is maximized. The structure of the enclosure includes features for increasing the airflow through the enclosure.
摘要翻译：所描述的实施例提供了用于个人飞机的转子安装悬臂组件。该转子安装吊杆组件包括可拆卸地连接到该个人飞机的机翼的转子安装吊杆，一个或多个竖直提升转子以及一个或多个转子控制器组件。每个转子的控制器组件定位在转子安装吊杆上，使得来自转子的下洗气导致增加通过控制器组件的气流以冷却控制器组件组件。转子控制器外壳包括进气口和出气口，以允许气流通过外壳来冷却控制器组件。空气入口相对于转子叶片的路径定位成使得流入空气入口的来自转子的下洗气最大化。外壳的结构包括增加通过外壳的气流的功能。

5. 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

6. 发明公开

EP3529150A1 VENTILATED ROTOR MOUNTING BOOM FOR PERSONAL AIRCRAFT 审中-公开
公开(公告)号：EP3529150A1
公开(公告)日：2019-08-28
申请号：EP17862058.9
申请日：2017-10-16
申请人： Kitty Hawk Corporation
发明人： TIGHE, James, Joseph , LONG, Geoffrey, Alan , TZARNOTZKY, Uri
IPC分类号： B64C29/00 , B64D27/24 , B64D27/26 , B64D33/10

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