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1. 发明申请

WO2018013368A1 MULTI-ROCKET PARACHUTE DEPLOYMENT SYSTEM 审中-公开
标题翻译：多火箭分布式部署系统
公开(公告)号：WO2018013368A1
公开(公告)日：2018-01-18
申请号：PCT/US2017/040420
申请日：2017-06-30
申请人： KITTY HAWK CORPORATION
发明人： ROBERTSON, Cameron , ROOP, Joseph , REICHERT, Todd , VANDER LIND, Damon
IPC分类号： B64D25/00 , B64D17/00 , B64D17/72 , B64D17/62
摘要： Techniques to deploy a parachute are disclosed. In various embodiments, a first projectile is configured to be propelled in a first direction, causing the parachute to be deployed. A second projectile configured to be propelled in a second direction is coupled to a line tethered to the parachute in such a way that a force in a direction opposite the first direction is applied to the line of the parachute when the second projectile is propelled in the second direction.
摘要翻译：披露了部署降落伞的技术。在各种实施例中，第一抛射体被配置为沿第一方向推进，使得降落伞展开。构造成在第二方向上推进的第二抛射体以这样的方式联接到拴系到降落伞上的线，即当第二抛射体在第一方向上被推进时，沿着与第一方向相反的方向的力被施加到降落伞的线第二方向。

2. 发明申请

WO2018026397A1 BISTABLE PITCH PROPELLER SYSTEM WITH BIDIRECTIONAL PROPELLER ROTATION 审中-公开
标题翻译：带双向螺旋桨旋转的双涡轮螺旋桨系统
公开(公告)号：WO2018026397A1
公开(公告)日：2018-02-08
申请号：PCT/US2017/022126
申请日：2017-03-13
申请人： KITTY HAWK CORPORATION
发明人： VANDER LIND, Damon , REICHERT, Todd
IPC分类号： B64C11/30 , B64C11/32 , B64C11/40 , B64C11/42 , B64C11/44
CPC分类号： B64C11/325 , B64C11/18 , B64C11/343 , B64C11/46 , B64C27/08 , B64C27/467 , B64C27/80 , B64C29/02 , B64C2201/108
摘要： A propeller includes a blade free to rotate. A first stop is positioned to mechanically engage one or both of a first portion of the blade and a first structure coupled to the blade when the blade is in a first position at a first end of the rotational range of motion. A second stop is positioned to mechanically engage one or both of a second portion, of the blade and a second structure coupled to the blade when the bia.de is in a second position at a second end of the defined rotational range. The blade rotates to the first position against the first stop when the propeller is rotated in a first direction and to the second position against the second stop when the propeller is rotated in a second direction.
摘要翻译：螺旋桨包括可自由旋转的刀片。当叶片处于旋转运动范围的第一端处的第一位置时，第一止动件定位成机械地接合叶片的第一部分和联接到叶片的第一结构中的一个或两个。第二止动件定位成当偏置件在限定的旋转范围的第二端处于第二位置时机械地接合叶片的第二部分和联接至叶片的第二结构中的一个或两个。当螺旋桨沿第一方向旋转时，叶片抵抗第一止动件旋转到第一位置，而当螺旋桨沿第二方向旋转时，叶片抵抗第二止动件旋转到第二位置。

3. 发明申请

WO2018118070A1 DISTRIBUTED FLIGHT CONTROL SYSTEM 审中-公开
公开(公告)号：WO2018118070A1
公开(公告)日：2018-06-28
申请号：PCT/US2016/068377
申请日：2016-12-22
申请人： KITTY HAWK CORPORATION
发明人： CUTLER, Mark Johnson , REICHERT, Todd , JACKSON, James
IPC分类号： B64C13/00 , B64C19/00 , G05D1/00 , G05D1/08
摘要： A set of commands for each of a plurality of actuators to alter an aircraft's state responsive to one or more inputs is produced. The set of commands is provided to fewer than all actuators comprising the plurality of actuators.

4. 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.

5. 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。

6. 发明申请

WO2018026398A1 BISTABLE PITCH PROPELLER SYSTEM WITH UNIDIRECTIONAL PROPELLER ROTATION 审中-公开
标题翻译：具有单向螺旋桨旋转的双柔性螺旋桨系统
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
申请人： KITTY HAWK CORPORATION
发明人： VANDER LIND, Damon , REICHERT, Todd
IPC分类号： B64C11/30 , B64C11/20 , B64C11/32 , B64C11/44
摘要： 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.
摘要翻译：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。

7. 发明申请

WO2018031075A1 ROTOR-BLOWN WING WITH PASSIVELY TILTING FUSELAGE 审中-公开
标题翻译：带有被动倾斜辅助装置的转子发条
公开(公告)号：WO2018031075A1
公开(公告)日：2018-02-15
申请号：PCT/US2017/023218
申请日：2017-03-20
申请人： KITTY HAWK CORPORATION
发明人： REICHERT, Todd
IPC分类号： B64C29/02
CPC分类号： B64C29/0033 , B64C11/28 , B64C39/062 , B64C39/08
摘要： An aircraft includes a wing where a first rotor and a second rotor are coupled to the wing at a fixed position relative to the wing. The aircraft also includes a fuselage and a bearing. The bearing mechanically couples the wing and the fuselage and permits the wing and the fuselage to rotate with respect to each other about an axis of rotation. The bearing permits the fuselage to rotate under the influence of gravity to be in a same orientation relative to ground when the wing is in a first orientation relative to the ground as well as a second orientation relative to the ground.
摘要翻译：飞行器包括机翼，其中第一转子和第二转子在相对于机翼的固定位置处联接到机翼。该机还包括一个机身和一个轴承。轴承机械地连接机翼和机身，并允许机翼和机身相对于彼此围绕旋转轴线旋转。当机翼处于相对于地面的第一方位以及相对于地面的第二方位时，该轴承允许机身在重力的影响下转动成与地面相同的方位。

8. 发明申请

WO2017218220A1 SELF-ADJUSTING SYSTEM FOR AIRCRAFT CONTROL 审中-公开
标题翻译：航空器自动调整系统
公开(公告)号：WO2017218220A1
公开(公告)日：2017-12-21
申请号：PCT/US2017/035824
申请日：2017-06-02
申请人： KITTY HAWK CORPORATION
发明人： REICHERT, Todd , VAWTER, Zachais , ROOP, Joseph , CUTLER, Mark, Johnson
IPC分类号： A63F9/24 , A63F13/00 , A63F13/12 , A63F13/20 , A63F13/98 , B60R21/00
摘要： A self-adjusting flight control system is disclosed. In various embodiments, an input interface receives an input signal generated by an inceptor based at least in part on a position of an input device comprising the inceptor. A processor coupled to the input interface determines dynamically a mapping to be used to map input signals received from the inceptor to corresponding output signals associated with flight control and uses the determined mapping to map the input signal to a corresponding output signal. The processor determines the mapping at least in part by computing a running average of the output signal over an averaging period and adjusting the mapping at least in part to associate a neutral position of the input device comprising the inceptor with a corresponding output level that is determined at least in part by the computed running average.
摘要翻译：公开了一种自调节飞行控制系统。在各种实施例中，输入接口至少部分地基于包括感受器的输入装置的位置来接收由感测器生成的输入信号。耦合到输入接口的处理器动态地确定要用于将从感测器接收的输入信号映射到与飞行控制相关联的对应输出信号的映射，并使用所确定的映射将输入信号映射到对应的输出信号。处理器至少部分地通过在平均周期内计算输出信号的运行平均值并且至少部分地调整映射来确定映射，所述映射至少部分地将包括输入设备的输入设备的中性位置与被确定的对应输出水平相关联至少部分取决于计算出的运行平均值。

9. 发明公开

EP3676679A1 DECOUPLED HAND CONTROLS FOR AIRCRAFT WITH VERTICAL TAKEOFF AND LANDING AND FORWARD FLIGHT CAPABILITIES 审中-公开
公开(公告)号：EP3676679A1
公开(公告)日：2020-07-08
申请号：EP18850604.2
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

10. 发明公开

EP3558815A1 DISTRIBUTED FLIGHT CONTROL SYSTEM 审中-公开
公开(公告)号：EP3558815A1
公开(公告)日：2019-10-30
申请号：EP16924390.4
申请日：2016-12-22
申请人： Kitty Hawk Corporation
发明人： CUTLER, Mark Johnson , REICHERT, Todd , JACKSON, James
IPC分类号： B64C13/00 , B64C19/00 , G05D1/00 , G05D1/08

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