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1. 发明专利

JP2020522841A 電動輸送機器ハイブリッドバッテリシステム审中-公开
公开(公告)号：JP2020522841A
公开(公告)日：2020-07-30
申请号：JP2019564919
申请日：2017-05-30
申请人：キティー・ホーク・コーポレーション , KITTY HAWK CORPORATION
发明人：バンダー・リンド・デーモン , ハンセル・ジョージ・ジェームズ
IPC分类号： B64C29/00 , B64D27/24 , H01M2/10
摘要：【解決手段】ハイブリッドバッテリシステムを備える電動輸送機器が開示されている。この輸送機器は、モータと、モータに結合されたハイブリッドバッテリシステムとを備える。ハイブリッドバッテリシステムは、第1のエネルギ密度および第1の電力密度を有する第1のバッテリと、第1のバッテリと並列する第2のバッテリとを備える。第2のバッテリは、第1のエネルギ密度より低い第2のエネルギ密度と、第1の電力密度より大きい第2の電力密度とを有する。この輸送機器は、電力を第1のモードで第1のバッテリから不均一に引き出し、第2のモードで第2のバッテリから不均一に引き出すように構成されている。【選択図】図5

2. 发明专利

JP6837146B2 分散型飛行制御システム有权
公开(公告)号：JP6837146B2
公开(公告)日：2021-03-03
申请号：JP2019534879
申请日：2016-12-22
申请人：キティー・ホーク・コーポレーション , KITTY HAWK CORPORATION
发明人：カトラー・マーク・ジョンソン , ライヘルト・トッド , ジャクソン・ジェームズ
IPC分类号： B64C27/08 , B64D47/00 , B64C13/18

3. 发明专利

JP2020503209A 分散型飛行制御システム审中-公开
公开(公告)号：JP2020503209A
公开(公告)日：2020-01-30
申请号：JP2019534879
申请日：2016-12-22
申请人：キティー・ホーク・コーポレーション , KITTY HAWK CORPORATION
发明人：カトラー・マーク・ジョンソン , ライヘルト・トッド , ジャクソン・ジェームズ
IPC分类号： B64C27/08 , B64D47/00 , B64C13/18
摘要：【解決手段】1つ以上の入力に応答して航空機の状態を変更するために、複数のアクチュエータの各々に対するコマンドのセットが生成される。コマンドのセットは、複数のアクチュエータを含む全てよりも少ないアクチュエータに提供される。【選択図】図4

4. 发明申请

WO2022015336A1 BATTERY SYSTEM WITH CYLINDRICAL CELLS 审中-公开
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
申请人： KITTY HAWK CORPORATION
发明人： WONG, Derek , SHIMANOFF, Alexis , ROY, Arunanshu
IPC分类号： 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
摘要： 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.

5. 发明申请

WO2021072065A1 HYBRID POWER SYSTEMS FOR DIFFERENT MODES OF FLIGHT 审中-公开
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
申请人： KITTY HAWK CORPORATION
发明人： SINHA, Pranay , VANDER LIND, Damon
IPC分类号： B64D27/10 , B64D27/24 , B64D37/30 , B64C29/00 , B64C27/22 , B64C27/28 , B64D27/02 , B64D41/00 , F02C6/14 , B64D31/06
摘要： 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.

6. 发明申请

WO2019112681A1 PROPELLER IMPACT DETECTION AND FORCE REDUCTION 审中-公开
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
申请人： KITTY HAWK CORPORATION
发明人： SAUNDERS, Christopher, Scott
IPC分类号： B64D31/06 , B64C11/46 , B64C27/08
摘要： 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.

7. 发明申请

WO2019045864A1 DECOUPLED HAND CONTROLS FOR AIRCRAFT WITH VERTICAL TAKEOFF AND LANDING AND FORWARD FLIGHT CAPABILITIES 审中-公开
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
申请人： KITTY HAWK CORPORATION
发明人： SELWA, Alexander, David , REICHERT, Todd , CUTLER, Mark, Johnson
IPC分类号： G05D1/00
摘要： 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.

8. 发明申请

WO2018128716A1 METHOD OF ROTOR PRODUCTION INCLUDING CO-CURING AND MAGNETIZATION IN PLACE 审中-公开
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
申请人： KITTY HAWK CORPORATION
发明人： LONG, Geoffrey Alan
IPC分类号： H02K1/27 , H02K1/22 , H02K1/28 , H02K15/03 , H02K16/02
摘要： 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.

9. 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。

10. 发明申请

WO2018038822A1 MULTICOPTER WITH WIDE SPAN ROTOR CONFIGURATION 审中-公开
标题翻译： MULTICOPTER宽广的范围转子配置
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
申请人： KITTY HAWK CORPORATION
发明人： REICHERT, Todd , ROBERTSON, Cameron , CUTLER, Mark, Johnson
IPC分类号： B64C27/08 , B64C11/46
摘要： 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.
摘要翻译：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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