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公开(公告)号：WO2022015336A1
公开(公告)日：2022-01-20
申请号：PCT/US2020/042781
申请日：2020-07-20
Applicant: KITTY HAWK CORPORATION
Inventor： WONG, Derek , SHIMANOFF, Alexis , ROY, Arunanshu
IPC: H01M10/42 , B60L58/10 , B60L2200/10 , B60L50/64 , B60L58/18 , B64C2201/042 , B64C29/00 , B64D27/24 , H01M10/0422 , H01M10/4257 , H01M10/482 , H01M2010/4271 , H01M2220/20 , H01M50/20 , H01M50/528 , H02J7/0048 , H02J7/005
Abstract: A battery system which includes a plurality of cylindrical cells, including a first cylindrical cell and a second cylindrical cell, an electrical tab that is connected to the first cylindrical cell and the second cylindrical cell using spot welding, and a battery management printed circuit board, where the electrical tab provides a connecting surface for a battery management signal between (1) the first cylindrical cell and the second cylindrical cell and (2) the battery management printed circuit board.
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公开(公告)号：WO2021072065A1
公开(公告)日：2021-04-15
申请号：PCT/US2020/054772
申请日：2020-10-08
Applicant: KITTY HAWK CORPORATION
Inventor： SINHA, Pranay , VANDER LIND, Damon
IPC: B64D27/10 , B64D27/24 , B64D37/30 , B64C29/00 , B64C27/22 , B64C27/28 , B64D27/02 , B64D41/00 , F02C6/14 , B64D31/06
Abstract: A first power source, a second power source, and a power controller are provided, where a vehicle that includes the first power source, the second power source, and the power controller is capable of flying in a transitional mode between a hovering mode and a forward flight mode. The power controller selects one or more of the first power source and the second power source to power a rotor included in the vehicle during the transitional mode.
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公开(公告)号：WO2019112681A1
公开(公告)日：2019-06-13
申请号：PCT/US2018/053165
申请日：2018-09-27
Applicant: KITTY HAWK CORPORATION
Inventor： SAUNDERS, Christopher, Scott
Abstract: A commanded control signal is compared against an adaptive control signal in order to detect a rotor strike by a rotor included in an aircraft, wherein the adaptive control signal is associated with controlling the rotor and the adaptive control signal varies based at least in part on the commanded control signal and state information associated with the rotor. In response to detecting the rotor strike, a control signal to the rotor is adjusted in order to reduce a striking force associated with the rotor.
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4.发明申请
公开(公告)号：WO2019045864A1
公开(公告)日：2019-03-07
申请号：PCT/US2018/039974
申请日：2018-06-28
Applicant: KITTY HAWK CORPORATION
Inventor： SELWA, Alexander, David , REICHERT, Todd , CUTLER, Mark, Johnson
IPC: G05D1/00
Abstract: Hand controls for an aircraft, including a single axis hand control which is configured to control movement of an aircraft along a vertical axis where the aircraft includes a plurality of rotors that are attached to the aircraft at a fixed position and the plurality of rotors rotate independently of one another., The hand controls further include a three axis hand control which is configured to control movement of the aircraft within a plane defined by a roll axis and a pitch axis, as well as about a yaw axis.
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公开(公告)号：WO2018128716A1
公开(公告)日：2018-07-12
申请号：PCT/US2017/062087
申请日：2017-11-16
Applicant: KITTY HAWK CORPORATION
Inventor： LONG, Geoffrey Alan
Abstract: Techniques described here provide a rotor and a method of making a rotor. In an embodiment, a method of making a rotor includes forming a magnet array by assembling a plurality of magnets into the magnet array, providing pre-preg adjacent to the magnet array, co-curing the magnet array with the pre-preg, and magnetizing the magnet array subsequent to the formation of the magnet array.
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Patent Agency Ranking
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
Applicant: KITTY HAWK CORPORATION
Inventor： TIGHE, James, Joseph , ALLISON, Eric
Abstract: 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.
Abstract translation: 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。
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公开(公告)号：WO2018038822A1
公开(公告)日：2018-03-01
申请号：PCT/US2017/042394
申请日：2017-07-17
Applicant: KITTY HAWK CORPORATION
Inventor： REICHERT, Todd , ROBERTSON, Cameron , CUTLER, Mark, Johnson
Abstract: A multicopter aircraft with a wide span rotor configuration is disclosed. In various embodiments, a multicopter as disclosed herein includes a fuselage and a plurality of rotors. The plurality of rotors includes inner rotors and outer rotors, with the inner rotors being substantially surrounded by the outer rotors or the fuselage. The inner rotors and the outer rotors may be tilted based at least in part on their arrangement in relation to the fuselage.
Abstract translation: 公开了具有大跨度转子构造的多旋翼飞机。 在各种实施例中，如本文所公开的多旋翼飞行器包括机身和多个转子。 多个转子包括内转子和外转子，其中内转子基本上由外转子或机身围绕。 内转子和外转子可以至少部分地基于它们相对于机身的布置而倾斜。
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8.发明申请
公开(公告)号：WO2018026398A1
公开(公告)日：2018-02-08
申请号：PCT/US2017/022332
申请日：2017-03-14
Applicant: KITTY HAWK CORPORATION
Inventor： VANDER LIND, Damon , REICHERT, Todd
Abstract: A propeller includes a blade free to rotate about a longitudinal axis of the blade. The propeller also includes a mechanical stop positioned to engage mechanically a first portion of the blade and/or a first structure coupled mechanically to the blade when the blade is in a first position. The propeller also includes a magnetic stop positioned to engage magnetically a second portion of the blade and/or a second structure coupled mechanically to the blade when the blade is in a second position. The blade rotates to the first position against the mechanical stop when the propeller is rotated at a first rotational speed and the blade rotates to the second position against the magnetic stop when the propeller is rotated at a second rotational speed in a same direction as when the blade is in the first position.
Abstract translation: 螺旋桨包括刀片，该刀片围绕刀片的纵向轴线自由旋转。 螺旋桨还包括机械挡块，该机械挡块被定位成机械地接合叶片的第一部分和/或当叶片处于第一位置时机械地联接到叶片的第一结构。 螺旋桨还包括磁性止动件，磁性止动件定位成当叶片处于第二位置时磁力地接合叶片的第二部分和/或机械地联接至叶片的第二结构。 当螺旋桨以第一旋转速度旋转时，叶片抵抗机械止动件旋转到第一位置，并且当螺旋桨以与第二旋转速度相同的方向旋转时，叶片抵抗磁性止动件旋转到第二位置 刀片处于第一位。
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公开(公告)号：WO2021040906A1
公开(公告)日：2021-03-04
申请号：PCT/US2020/042631
申请日：2020-07-17
Applicant: KITTY HAWK CORPORATION
Inventor： ORENDER, Joseph , SAUNDERS, Christopher, Scott , WONG, Derek
Abstract: A configuration instruction associated with configuring a plurality of batteries which supply power to a plurality of motors in a vehicle is received. The batteries are configuring as specified by the configuration instruction, where the batteries are able to be configured in a plurality of configurations, including: a first configuration where at least some of the batteries are electrically connected together in parallel and a second configuration where at least some of the batteries are electrically connected together in series.
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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
Applicant: KITTY HAWK CORPORATION
Inventor： VAN PELT, Chris , TIGHE, James, Joseph
Abstract: 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.
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