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公开(公告)号：US09033273B2
公开(公告)日：2015-05-19
申请号：US13287115
申请日：2011-11-01
Applicant: Jonathan Edelson , Neal Gilleran , Isaiah Cox , Scott Perkins , Robert Sweet
Inventor： Jonathan Edelson , Neal Gilleran , Isaiah Cox , Scott Perkins , Robert Sweet
CPC classification number: B64C25/405 , G08G5/065 , Y02T50/823
Abstract: An aircraft ground control system that moves an aircraft on the ground between landing and take off without external mechanical assistance from airport tugs or tow vehicles or reliance on thrust produced by the aircraft's engines is provided. The aircraft ground control system interfaces only with an aircraft auxiliary power unit or other aircraft power supply, but otherwise operates independently of aircraft systems. A system integrator and controller links cockpit controls designed to actuate the transmission of power to system components and to activate system components only under predetermined conditions with selectively activatable drivers in driving connection with one or more aircraft wheels to move the aircraft on the ground at selected torques and speeds.
Abstract translation: 提供一种飞机地面控制系统，其在飞机着陆和起飞之间移动飞机，而不需要机场拖船或拖车的外部机械帮助，或依赖飞机发动机产生的推力。 飞机地面控制系统只能与飞机辅助动力装置或其他飞机电源相连接，而与飞机系统无关。 系统集成商和控制器连接驾驶舱控制器，其设计用于致动向系统组件传递电力，并且仅在预定条件下激活系统组件，其中选择性地激活驱动器与一个或多个飞行器轮驱动连接，以在选定的转矩下将飞机移动到地面上 和速度。
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公开(公告)号：US08820675B2
公开(公告)日：2014-09-02
申请号：US13549520
申请日：2012-07-16
Applicant: Isaiah W. Cox , Hans J. Walitzki , Jonathan Edelson
Inventor： Isaiah W. Cox , Hans J. Walitzki , Jonathan Edelson
IPC: B64C25/34
CPC classification number: B64C25/001 , B64C25/40 , B64C25/405 , Y02T50/823
Abstract: The invention disclosed is a self-propelled aircraft undercarriage for driving an aircraft on the ground, comprising: an axle; a strut supporting said axle; at least one wheel rotatably mounted on said axle; and drive means for driving said at least one wheel; characterized in that said drive means is disk shaped and is external to said wheel. In one embodiment of the invention, said drive means is mounted on said axle between said strut and said wheel. In a second embodiment, said drive means is mounted on said axle, on the side of said wheel furthest from said strut.
Abstract translation: 所公开的发明是用于驾驶飞机在地面上的自行式飞机起落架，包括：一个轴; 支撑所述轴的支柱; 至少一个可旋转地安装在所述轴上的轮; 以及用于驱动所述至少一个车轮的驱动装置; 其特征在于，所述驱动装置是盘形的并且在所述轮的外部。 在本发明的一个实施例中，所述驱动装置安装在所述支柱和所述轮之间的所述轴上。 在第二实施例中，所述驱动装置安装在所述轴上，在所述轮的离所述支柱最远的一侧。
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33.发明授权公开(公告)号：US08658391B2
公开(公告)日：2014-02-25
申请号：US11741125
申请日：2007-04-27
Applicant: Jonathan Edelson
Inventor： Jonathan Edelson
IPC: C12Q1/46
CPC classification number: G01N33/5088 , G01N33/944 , G01N2333/33
Abstract: The present invention provides methods for assessing the activity of topically administered chemodenervating agents. In some embodiments, methods for assessing the activity of topically administered chemodenervating agents involve determining the extent of inhibition of acetylcholine release near the site of administration. In some embodiments, methods for assessing activity of topically administered chemodenervating agents involve observing a reflex motion of a limb of a subject.
Abstract translation: 本发明提供了评估局部给药的化学修复剂的活性的方法。 在一些实施方案中，用于评估局部施用的化学修饰剂的活性的方法涉及确定施用部位附近乙酰胆碱释放的抑制程度。 在一些实施方案中，用于评估局部施用化学去神经剂的活性的方法涉及观察受试者肢体的反射运动。
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公开(公告)号：US20130064688A1
公开(公告)日：2013-03-14
申请号：US13436967
申请日：2012-04-01
Applicant: Hans Walitzki , Jonathan Edelson , Rodney T. Cox
Inventor： Hans Walitzki , Jonathan Edelson , Rodney T. Cox
CPC classification number: F04D27/004 , F02C7/268 , H02K15/02 , Y10T29/49009
Abstract: A starter/generator machine for a turbine with a turbine enclosure, an air duct, and a plurality of fan blades is provided. The starter/generator machine includes a plurality of stator elements spaced at intervals in a ring shape adjacent to the air duct and a plurality of rotor elements mounted on the fan blades. The stator elements and the rotor elements are mounted to interact magnetically to exert a force sufficient to move the rotor elements. The stator elements are shaped to minimize air flow interference and are formed with a core, at least one pole, and multiple windings. The spacing between the stator elements and the rotor elements forms an air gap on the order of 5-10 mm, and the number of stator elements is different from the number of rotor elements.
Abstract translation: 提供了一种用于具有涡轮机壳体，空气管道和多个风扇叶片的涡轮机的起动/发电机。 起动机/发电机包括多个定子元件，它们以与空气管道相邻的环形间隔开，并且多个转子元件安装在风扇叶片上。 定子元件和转子元件被安装成磁力相互作用以施加足以移动转子元件的力。 定子元件成形为使空气流动干扰最小化并且形成有芯，至少一个极和多个绕组。 定子元件和转子元件之间的间隔形成大约5-10mm的气隙，并且定子元件的数量与转子元件的数量不同。
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公开(公告)号：US20080007070A1
公开(公告)日：2008-01-10
申请号：US11900614
申请日：2007-09-11
Applicant: Jonathan Edelson
Inventor： Jonathan Edelson
IPC: F03D9/00
CPC classification number: H02K3/28 , F03D9/25 , F05B2240/9111 , H02K3/46 , H02K5/08 , H02K7/183 , H02K2213/06 , Y02E10/465 , Y02E10/725 , Y02E10/728
Abstract: The present invention is a ring generator with a rotor internal diameter equal to the turbine outside diameter, and having the turbine mounted on the inside of the rotor.
Abstract translation: 本发明是一种环形发电机，其转子内径等于涡轮机外径，并且具有安装在转子内侧的涡轮机。
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Patent Agency Ranking
公开(公告)号：US20070158497A1
公开(公告)日：2007-07-12
申请号：US11542975
申请日：2006-10-04
Applicant: Jonathan Edelson , Isaiah Cox
Inventor： Jonathan Edelson , Isaiah Cox
IPC: B64C25/40
CPC classification number: B64C25/405 , B64C25/40
Abstract: The present invention is directed to an apparatus for driving an aircraft having an undercarriage wheel, comprising aircraft drive means for driving an undercarriage wheel, and a clutch disposed between said driven means and said wheel, wherein said drive means and said clutch are directly connected to the undercarriage apparatus. Said apparatus may have gears disposed between said drive means clutch, or between said clutch and said wheel. In a most preferred arrangement, the apparatus of the invention fits inside the hub of said wheel. When the invention is applied to an aircraft undercarriage wheel, the clutch allows the wheel to be disengaged for takeoff and landing.
Abstract translation: 本发明涉及一种用于驾驶具有底盘轮的飞机的装置，包括用于驱动底架轮的飞行器驱动装置和设置在所述从动装置和所述车轮之间的离合器，其中所述驱动装置和所述离合器直接连接到 起落架装置。 所述装置可以具有设置在所述驱动装置离合器之间或设置在所述离合器和所述车轮之间的齿轮。 在最优选的布置中，本发明的装置安装在所述轮的轮毂内。 当本发明应用于飞机底盘轮时，离合器允许车轮脱离起飞和着陆。
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公开(公告)号：US6054837A
公开(公告)日：2000-04-25
申请号：US715482
申请日：1996-09-18
Applicant: Jonathan Edelson
Inventor： Jonathan Edelson
CPC classification number: H02P27/08 , H02K17/12 , H02K3/28 , H02K29/03 , H02P27/047
Abstract: A polyphase induction machine operated by an inverter drive system. The machine is constructed with concentrated full span windings. Twelve or more phases are used to sufficiently cover the airgap region, in contrast to the conventional three phases using distributed and chorded windings. Substantial efficiency and starting torque benefits are thereby obtained.
Abstract translation: 由逆变驱动系统操作的多相感应电机。 该机器采用集中的全跨度绕组构成。 与使用分布式和弦式绕组的常规三相相比，使用12个或更多相来充分覆盖气隙区。 从而获得了显着的效率和启动转矩效益。
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公开(公告)号：US08505308B2
公开(公告)日：2013-08-13
申请号：US13436967
申请日：2012-04-01
Applicant: Hans Walitzki , Jonathan Edelson , Rodney T. Cox
Inventor： Hans Walitzki , Jonathan Edelson , Rodney T. Cox
IPC: F02C1/00
CPC classification number: F04D27/004 , F02C7/268 , H02K15/02 , Y10T29/49009
Abstract: A starter/generator machine for a turbine with a turbine enclosure, an air duct, and a plurality of fan blades is provided. The starter/generator machine includes a plurality of stator elements spaced at intervals in a ring shape adjacent to the air duct and a plurality of rotor elements mounted on the fan blades. The stator elements and the rotor elements are mounted to interact magnetically to exert a force sufficient to move the rotor elements. The stator elements are shaped to minimize air flow interference and are formed with a core, at least one pole, and multiple windings. The spacing between the stator elements and the rotor elements forms an air gap on the order of 5-10 mm, and the number of stator elements is different from the number of rotor elements.
Abstract translation: 提供了一种用于具有涡轮机壳体，空气管道和多个风扇叶片的涡轮机的起动/发电机。 起动机/发电机包括多个定子元件，它们以与空气管道相邻的环形间隔开，并且多个转子元件安装在风扇叶片上。 定子元件和转子元件被安装成磁力相互作用以施加足以移动转子元件的力。 定子元件成形为使空气流动干扰最小化并且形成有芯，至少一个极和多个绕组。 定子元件和转子元件之间的间隔形成大约5-10mm的气隙，并且定子元件的数量与转子元件的数量不同。
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公开(公告)号：US20130119190A1
公开(公告)日：2013-05-16
申请号：US13549520
申请日：2012-07-16
Applicant: Isaiah W. Cox , Hans J. Walitzki , Jonathan Edelson
Inventor： Isaiah W. Cox , Hans J. Walitzki , Jonathan Edelson
IPC: B64C25/00
CPC classification number: B64C25/001 , B64C25/40 , B64C25/405 , Y02T50/823
Abstract: The invention disclosed is a self-propelled aircraft undercarriage for driving an aircraft on the ground, comprising: an axle; a strut supporting said axle; at least one wheel rotatably mounted on said axle; and drive means for driving said at least one wheel; characterized in that said drive means is disk shaped and is external to said wheel. In one embodiment of the invention, said drive means is mounted on said axle between said strut and said wheel. In a second embodiment, said drive means is mounted on said axle, on the side of said wheel furthest from said strut.
Abstract translation: 所公开的发明是用于驾驶飞机在地面上的自行式飞机起落架，包括：一个轴; 支撑所述轴的支柱; 至少一个可旋转地安装在所述轴上的轮; 以及用于驱动所述至少一个车轮的驱动装置; 其特征在于，所述驱动装置是盘形的并且在所述轮的外部。 在本发明的一个实施例中，所述驱动装置安装在所述支柱和所述轮之间的所述轴上。 在第二实施例中，所述驱动装置安装在所述轴上，在所述轮的离所述支柱最远的一侧。
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公开(公告)号：US20120328549A1
公开(公告)日：2012-12-27
申请号：US13356634
申请日：2012-01-23
Applicant: Jonathan EDELSON , Timothy KOTYLA , Klaus THEOBALD
Inventor： Jonathan EDELSON , Timothy KOTYLA , Klaus THEOBALD
IPC: A61K31/225 , A61K8/37 , A61K31/7048 , A61K31/70 , A61P35/00 , A61K31/4436 , A61P17/08 , A61P17/10 , A61Q15/00 , A61P17/02 , C07C57/02 , A61K31/65
CPC classification number: A61K31/20
Abstract: The present invention provides oil compositions and associated methods and reagents, particularly useful for the treatment of dermatologic conditions. In some embodiments, provided compositions are formulated for and achieve transdermal delivery, for example by topical administration.
Abstract translation: 本发明提供油组合物和相关方法和试剂，特别可用于治疗皮肤病学条件。 在一些实施方案中，所提供的组合物被配制用于并实现透皮递送，例如通过局部施用。
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