专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US09022316B2 System and method for failsafe operation of aircraft ground movement system 有权
标题翻译：飞机地面运动系统故障安全运行系统及方法
公开(公告)号：US09022316B2
公开(公告)日：2015-05-05
申请号：US13301498
申请日：2011-11-21
申请人： Neal Gilleran , Robert Sweet , Jonathan Edelson , Isaiah Watas Cox
发明人： Neal Gilleran , Robert Sweet , Jonathan Edelson , Isaiah Watas Cox
IPC分类号： B64C25/00 , B64C25/40
CPC分类号： B64C25/405 , Y02T50/823
摘要： A failsafe system and method for ensuring the safe operation of an aircraft with a ground movement system to drive the aircraft independently on the ground is provided. The system includes at least one aircraft nose or main drive wheel powered by an onboard wheel driver responsive to sensed aircraft and ground movement system operating parameters to continue operation in response to parameters within normal limits or to prevent continued operation if sensed parameters are outside normal limits and indicate continued operation to be unsafe. The onboard wheel driver includes a locking assembly responsive automatically or manually to signals indicating sensed parameters to lock the onboard wheel driver in an activated or an inactivated condition, depending on whether operation of the ground movement system can be continued safely.
摘要翻译：提供一种用于确保具有地面运动系统的飞机的安全操作以在地面独立地驱动飞机的故障安全系统和方法。该系统包括至少一个飞行器鼻部或主驱动轮，其由响应于感测到的飞行器和地面移动系统操作参数的车载驱动器驱动，以响应于正常限度内的参数继续操作，或者如果感测到的参数在正常限度之外，则防止继续操作并指示持续运作不安全。车载轮驱动器包括一个自动或手动响应的信号，该锁定组件响应于指示感测参数的信号，以根据地面移动系统的操作是否可以安全地继续操作将车载车轮驱动器锁定在激活状态或非激活状态。

2. 发明申请

US20120217339A1 System and Method for Failsafe Operation of Aircraft Ground Movement System 有权
标题翻译：飞机地面运动系统故障安全运行系统与方法
公开(公告)号：US20120217339A1
公开(公告)日：2012-08-30
申请号：US13301498
申请日：2011-11-21
申请人： Neal Gilleran , Robert Sweet , Jonathan Edelson , Isaiah Watas Cox
发明人： Neal Gilleran , Robert Sweet , Jonathan Edelson , Isaiah Watas Cox
IPC分类号： B64C25/50 , G08G5/06
CPC分类号： B64C25/405 , Y02T50/823
摘要： A failsafe system and method for ensuring the safe operation of an aircraft with a ground movement system to drive the aircraft independently on the ground is provided. The system includes at least one aircraft nose or main drive wheel powered by an onboard wheel driver responsive to sensed aircraft and ground movement system operating parameters to continue operation in response to parameters within normal limits or to prevent continued operation if sensed parameters are outside normal limits and indicate continued operation to be unsafe. The onboard wheel driver includes a locking assembly responsive automatically or manually to signals indicating sensed parameters to lock the onboard wheel driver in an activated or an inactivated condition, depending on whether operation of the ground movement system can be continued safely.
摘要翻译：提供一种用于确保具有地面运动系统的飞机的安全操作以在地面独立地驱动飞机的故障安全系统和方法。该系统包括至少一个飞行器鼻部或主驱动轮，其由响应于感测到的飞行器和地面移动系统操作参数的车载驱动器驱动，以响应于正常限度内的参数继续操作，或者如果感测到的参数在正常限度之外，则防止继续操作并指示持续运作不安全。车载轮驱动器包括一个自动或手动响应的信号，该锁定组件响应于指示感测参数的信号，以根据地面移动系统的操作是否可以安全地继续操作将车载车轮驱动器锁定在激活状态或非激活状态。

3. 发明申请

US20120168557A1 Integrated Aircraft Ground Navigation Control System 有权
标题翻译：综合飞机地面导航控制系统
公开(公告)号：US20120168557A1
公开(公告)日：2012-07-05
申请号：US13287115
申请日：2011-11-01
申请人： Jonathan Edelson , Neal Gilleran , Isaiah Cox , Scott Perkins , Robert Sweet
发明人： Jonathan Edelson , Neal Gilleran , Isaiah Cox , Scott Perkins , Robert Sweet
IPC分类号： B64C25/50
CPC分类号： B64C25/405 , G08G5/065 , Y02T50/823
摘要： 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.
摘要翻译：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。

4. 发明授权

US09033273B2 Integrated aircraft ground navigation control system 有权
标题翻译：综合飞机地面导航控制系统
公开(公告)号：US09033273B2
公开(公告)日：2015-05-19
申请号：US13287115
申请日：2011-11-01
申请人： Jonathan Edelson , Neal Gilleran , Isaiah Cox , Scott Perkins , Robert Sweet
发明人： Jonathan Edelson , Neal Gilleran , Isaiah Cox , Scott Perkins , Robert Sweet
IPC分类号： B64C25/00 , B64C25/40 , G08G5/06
CPC分类号： B64C25/405 , G08G5/065 , Y02T50/823
摘要： 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.
摘要翻译：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。

5. 发明申请

US20110305734A1 NUCLEIC ACID NANOPARTICLES AND USES THEREFOR 有权
标题翻译：核酸纳米粒及其用途
公开(公告)号：US20110305734A1
公开(公告)日：2011-12-15
申请号：US12671693
申请日：2008-05-30
申请人： Jonathan Edelson , Timothy Kotyla , Boke Zhang
发明人： Jonathan Edelson , Timothy Kotyla , Boke Zhang
IPC分类号： A61K48/00 , A61K9/10 , A61Q17/04 , A61K9/70 , A61K8/02 , A61P35/04 , A61P17/00 , A61P17/06 , A61P17/02 , A61Q19/00 , A61Q19/04 , A61K31/7105 , A61K9/51 , B82Y5/00
CPC分类号： A61K31/7105 , A61K9/0014 , A61K9/1075
摘要： The present invention provides nanoparticle compositions including one or more nucleic acids. The present invention achieves delivery (particularly transdermal delivery) of such nucleic acids without the need for nucleic acid modification, or for use of chemical or mechanical abrasion or disruption of skin.
摘要翻译：本发明提供包含一种或多种核酸的纳米颗粒组合物。本发明实现了这种核酸的递送（特别是透皮递送），而不需要核酸修饰，或者用于化学或机械磨损或皮肤破坏。

6. 发明申请

US20080007130A1 Motor using magnetic normal force 审中-公开
标题翻译：电机采用磁力法向力
公开(公告)号：US20080007130A1
公开(公告)日：2008-01-10
申请号：US11900475
申请日：2007-09-11
申请人： Jonathan Edelson
发明人： Jonathan Edelson
IPC分类号： H02K37/14 , H02K7/10 , H02K7/06
CPC分类号： H02K41/06 , Y10T74/19
摘要： A motor is disclosed, comprising at least one fixed member comprising at least one magnetic winding, having an internal cavity; at least one driven member inside said fixed member, comprising magnetically conductive materials; constraining means for constraining said driven member to a path of movement with respect to said fixed member, said driven member being able to move within said fixed member, wherein magnetic normal force is induced in said fixed member periodically, whereby said driven member is periodically moved around said path by magnetic force, whereby rotary motion is produced.
摘要翻译：公开了一种电动机，包括至少一个包括至少一个具有内腔的磁性绕组的固定构件; 所述固定构件内的至少一个从动构件包括导磁材料; 约束装置，用于将所述从动构件约束成相对于所述固定构件运动的路径，所述从动构件能够在所述固定构件内移动，其中周期性地在所述固定构件中引起电磁法力，由此所述从动构件周期性地移动通过磁力围绕所述路径，从而产生旋转运动。

7. 发明申请

US20070057245A1 Artificial band gap 有权
公开(公告)号：US20070057245A1
公开(公告)日：2007-03-15
申请号：US11598918
申请日：2006-11-13
申请人： Avto Tavkhelidze , Jonathan Edelson , Isaiah Cox , Stuart Harbron
发明人： Avto Tavkhelidze , Jonathan Edelson , Isaiah Cox , Stuart Harbron
IPC分类号： H01L29/06 , H01S5/00 , H01L31/00
CPC分类号： B82Y10/00 , B82Y30/00 , B82Y40/00 , G03F7/0002 , H01J1/30 , H01L21/4867 , H01L29/127 , H01L31/0352 , Y10S977/755 , Y10S977/781 , Y10S977/782 , Y10S977/81
摘要： A method is disclosed for the induction of a suitable band gap and electron emissive properties into a substance, in which the substrate is provided with a surface structure corresponding to the interference of electron waves. Lithographic or similar techniques are used, either directly onto a metal mounted on the substrate, or onto a mold which then is used to impress the metal. In a preferred embodiment, a trench or series of nano-sized trenches are formed in the metal.

8. 发明申请

US20050218863A1 High phase order electrical rotating machine with distributed windings 失效
标题翻译：具有分布绕组的高相位电动旋转机
公开(公告)号：US20050218863A1
公开(公告)日：2005-10-06
申请号：US10509777
申请日：2003-04-03
申请人： Jonathan Edelson
发明人： Jonathan Edelson
IPC分类号： H02K3/28 , H02K11/04 , H02K17/12 , H02P25/22 , H02P7/36
CPC分类号： H02P25/22 , H02K3/28 , H02K11/33 , H02K17/12
摘要： A rotating induction machine, containing five or more different phases, having windings distributed according to a sinc function with a cutoff frequency allowing low-order spatial harmonics but preventing higher order spatial harnomics from flowing. In a preferred embodiment, the machine is connected to drive means capable of injecting third harmonic into the machine. In a further preferred embodiment, the windings are connected to the drive means with a mesh connection and the machine has five phases.
摘要翻译：一种包含五个或更多个不同相位的旋转感应电机，具有根据sinc功能分布的绕组，其截止频率允许低阶空间谐波，但是阻止更高阶空间的流失。在优选实施例中，机器连接到能够将三次谐波注入机器的驱动装置。在另一优选实施例中，绕组通过网状连接连接到驱动装置，并且机器具有五个相位。

9. 发明申请

US20050116474A1 Electronically controlled engine generator set 有权
标题翻译：电控发动机发电机组
公开(公告)号：US20050116474A1
公开(公告)日：2005-06-02
申请号：US11000612
申请日：2004-11-30
申请人： Jonathan Edelson
发明人： Jonathan Edelson
IPC分类号： B60L11/04 , B60L11/12 , H02P9/04 , B61C9/38 , B60L11/02 , F02N11/04
CPC分类号： B60L11/12 , B60L11/04 , H02P9/04 , H02P2101/10 , H02P2101/15 , Y02T10/642 , Y02T10/7077
摘要： An electronically controlled electrical power generator comprises a generator driven by a heat engine, operated by control means, and carrying an electrical load. Operation of the heat engine is at wide open throttle. Control over engine operation and electrical output of the generator is achieved by electronically manipulating the electric load, and/or adjusting excitation levels at the generator's magnetic fields, so as to change engine/generator equilibrium speed. In a beneficial embodiment, the generator is powered by an energy storage unit, to temporarily act as a motor and rotate the engine when starting, and during power absorbing strokes.
摘要翻译：电控发电机包括由发动机驱动的发电机，由控制装置操作并承载电力负载。热机的运行处于较宽的开度。通过电子操纵电气负载和/或调整发电机的磁场处的激励电平来实现对发电机的发动机操作和电力输出的控制，以便改变发动机/发电机的平衡速度。在有益的实施例中，发电机由能量存储单元供电，临时充当电动机，并且在启动时和在功率吸收行程期间使发动机旋转。

10. 发明授权

US09233752B2 Drive system with harmonic drive for self-propelled aircraft wheel 有权
标题翻译：用于自行式飞轮的谐波驱动系统
公开(公告)号：US09233752B2
公开(公告)日：2016-01-12
申请号：US13561066
申请日：2012-07-29
申请人： Hans Walitzki , Jonathan Edelson , Rodney T. Cox , Isaiah W. Cox
发明人： Hans Walitzki , Jonathan Edelson , Rodney T. Cox , Isaiah W. Cox
IPC分类号： B64C25/50 , B64C25/40
CPC分类号： B64C25/405 , Y02T50/823
摘要： A drive system with harmonic drive designed to meet the high power and torque requirements required to drive an aircraft independently on the ground is provided. The drive system includes an electric motor driven by a harmonic drive assembly that may be configured to be integral with the motor. This drive system with harmonic drive can be effectively installed in an existing aircraft nose wheel or main wheel without changes to other components.
摘要翻译：提供谐波驱动器的驱动系统，其设计用于满足在地面上独立驾驶飞机所需的高功率和扭矩要求。驱动系统包括由谐波驱动组件驱动的电动马达，谐波驱动组件可被配置为与马达成一体。这种具有谐波驱动的驱动系统可以有效地安装在现有的飞机前轮或主轮上，而不会改变其他部件。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式