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公开(公告)号：US07116019B2
公开(公告)日：2006-10-03
申请号：US11029978
申请日：2005-01-04
Applicant: Jonathan Sidney Edelson
Inventor： Jonathan Sidney Edelson
IPC: H02K37/24
CPC classification number: H02K17/12 , H02K3/28 , H02K5/225 , H02K11/33 , H02P25/18 , H02P25/22 , H02P27/00 , H02P29/50
Abstract: An electrical rotating apparatus is provided that has variable impedance. This is achieved by connecting one of the polyphase components of the apparatus in a mesh connection. The spanning value, L, of such a mesh connection may be varied by changing the harmonic content supplied by an inverter component. Also provided is a method for connecting an inverter to a motor, wherein a switching arrangement permits the simple alteration between various mesh connections of different span value, changing thereby the Volts/Hertz ratio of the motor.
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公开(公告)号：US06570361B1
公开(公告)日：2003-05-27
申请号：US09255291
申请日：1999-02-22
Applicant: Jonathan Sidney Edelson
Inventor： Jonathan Sidney Edelson
IPC: H02P7628
Abstract: An electrical rotating apparatus comprises an inverter system that outputs more than three phases. The apparatus further includes a stator comprising a plurality of slots and full span concentrated windings, with the windings being electrically coupled to the inverter system, and a rotor electromagnetically coupled to a magnetic field generated by the stator. A signal generator generates a drive waveform signal, that has a fundamental frequency, and the drive waveform signal drives the inverter system. The drive waveform signal has a pulsing frequency and is in fixed phase relation to the fundamental frequency. Additionally, the inverter system may be fed by a drive waveform signal that is fed through at least one signal delay device.
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公开(公告)号：US6103298A
公开(公告)日：2000-08-15
申请号：US955097
申请日：1997-10-22
Applicant: Jonathan Sidney Edelson , Isaiah Watas Cox
Inventor： Jonathan Sidney Edelson , Isaiah Watas Cox
IPC: C23C14/12 , F25B21/00 , H01J1/02 , H01J1/13 , H01J1/14 , H01J1/30 , H01J21/04 , H01J21/10 , H01J45/00 , C25B11/04
CPC classification number: F25B21/00 , C23C14/12 , H01J1/02 , H01J1/13 , H01J1/14 , H01J1/30 , H01J21/04 , H01J21/105 , H01J45/00 , F25B2321/003 , F25B2400/15 , H01J2201/30426 , Y02B30/66
Abstract: Methods for making low work function electrodes either made from or coated with an electride material in which the electride material has lattice defect sites are described. Lattice defect sites are regions of the crystal structure where irregularities and deformations occur. Also provided are methods for making electrodes which consist of a substrate coated with a layer of a compound comprised of a cation complexed by an electride former, in which said complex has lattice defect sites. In addition, methods for making electrodes which consist of a bulk metal coated with a layer of an electride former having lattice defect sites are described. The electride former stabilizes the loss of electrons by surface sites on the metal, lowering the work-function of the coated surface.
Abstract translation: 描述了由电镀材料具有晶格缺陷部位的电极材料制成或涂覆低功函电极的方法。 晶格缺陷位点是发生不规则和变形的晶体结构区域。 还提供了制造电极的方法，其由涂覆有由电化学成形剂络合的阳离子组成的化合物层的基底组成，其中所述络合物具有晶格缺陷位点。 此外，描述了制造电极的方法，其由涂覆有具有晶格缺陷位点的电化学成形剂层的体金属组成。 电子前体通过金属上的表面位点稳定电子的损失，降低涂覆表面的功能。
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公开(公告)号：US6089311A
公开(公告)日：2000-07-18
申请号：US498199
申请日：1995-07-05
Applicant: Jonathan Sidney Edelson
Inventor： Jonathan Sidney Edelson
CPC classification number: F25B21/00 , F25B2321/003 , F25B2400/15 , Y02B30/66
Abstract: A new use for thermionic vacuum diode technology is disclosed wherein a vacuum diode is constructed using very low work function electrodes. A negative potential bias is applied to the cathode relative to the anode, and electrons are emitted. In the process of emission the electrons carry off kinetic energy, carrying heat away from the cathode and dissipating it at an opposing anode. The resulting heat pump is more efficient than conventional cooling methods, as well as being substantially scalable over a wide range of applications. Fabrication using conventional microelectronic fabrication techniques is possible.
Abstract translation: 公开了一种用于热离子真空二极管技术的新用途，其中使用极低功函电极构建真空二极管。 阴极相对于阳极施加负电位偏压，发射电子。 在发射过程中，电子携带动能，将热量从阴极携带并在相对的阳极上散发。 所得到的热泵比传统的冷却方法更有效，并且在广泛的应用范围内具有可扩展性。 使用常规微电子制造技术的制造是可能的。
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公开(公告)号：US5973259A
公开(公告)日：1999-10-26
申请号：US854302
申请日：1997-05-12
Applicant: Jonathan Sidney Edelson
Inventor： Jonathan Sidney Edelson
Abstract: A close spaced planar vacuum diode is constructed with a photoemissive first electrode and a low work function second electrode. As a result of photon flux on said photoemissive first electrode, electrons are emitted into the vacuum space and travel to said second electrode. This electron current may then flow through an external load, powering said external load.
Abstract translation: 采用光发射的第一电极和低功函数的第二电极构成一个紧密平面的真空二极管。 作为所述光发射第一电极上的光子通量的结果，电子被发射到真空空间中并行进到所述第二电极。 然后，该电子电流可以流过外部负载，为所述外部负载供电。
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Patent Agency Ranking
公开(公告)号：US5810980A
公开(公告)日：1998-09-22
申请号：US744574
申请日：1996-11-06
Applicant: Jonathan Sidney Edelson
Inventor： Jonathan Sidney Edelson
CPC classification number: H01J1/13 , H01J1/30 , F25B2321/003
Abstract: A metal surface is coated with a heterocyclic multidentate ligand compound, reducing work function and facilitating the emission of electrons.
Abstract translation: 金属表面涂覆有杂环多齿配体化合物，降低功函数并促进电子的发射。
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公开(公告)号：US20150159968A1
公开(公告)日：2015-06-11
申请号：US13615930
申请日：2012-09-14
Applicant: Jonathan Sidney Edelson , Rodney T. Cox , Nechama Cox , Isaiah W. Cox
Inventor： Jonathan Sidney Edelson , Rodney T. Cox , Nechama Cox , Isaiah W. Cox
CPC classification number: B64C25/405 , B60K7/0007 , B60K11/02 , B60K2001/006 , B60K2007/0038 , B60K2007/0092 , B60Y2200/50 , B60Y2200/51 , B60Y2306/03 , H02K7/14 , H02K9/19 , Y02T50/823
Abstract: A system is provided for dissipating heat in an onboard non-engine powered aircraft wheel drive assembly with drive means that power one or more aircraft wheels to drive the aircraft autonomously on the ground without directly using the aircraft engines. The heat dissipation system is integral with a wheel drive assembly mounted substantially completely within a nose or main landing gear wheel. A reservoir mounted outboard or inboard of the wheel drive assembly increases thermal distribution mass and fluidically communicates with wheel drive assembly components to automatically circulate heat transfer fluid between the wheel drive assembly and the reservoir when the operating temperature exceeds a predetermined maximum temperature during aircraft ground travel. The heat dissipating system can be retrofitted in an existing aircraft to improve thermal distribution and prolong wheel drive assembly and drive means operation and useful life.
Abstract translation: 提供了一种用于在车内非发动机动力的飞机车轮驱动组件上散热的系统，其具有驱动装置，所述驱动装置为一个或多个飞行器轮提供动力，以在地面上自主地驱动飞行器而不直接使用飞机发动机。 散热系统与基本上完全安装在鼻子或主起落架轮内的轮驱动组件是一体的。 安装在车轮驱动组件的外侧或内侧的储存器增加了热分配质量并且与车轮驱动组件部件流体连通，以便在飞行器地面行驶期间工作温度超过预定最大温度时，在轮驱动组件和储存器之间自动循环传热流体 。 散热系统可以在现有的飞机上进行改装，以改善热分配，延长轮驱装配和驱动装置的使用寿命。
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公开(公告)号：US08924040B2
公开(公告)日：2014-12-30
申请号：US12310610
申请日：2007-08-29
Applicant: Jonathan Sidney Edelson , Isaiah Watas Cox
Inventor： Jonathan Sidney Edelson , Isaiah Watas Cox
CPC classification number: B64F1/22 , B64C25/405 , Y02T50/823 , Y10S180/904
Abstract: A method and apparatus is disclosed for reversing an aircraft on the ground comprising driving the aircraft using at least one self-propelled undercarriage wheel. An apparatus for controlling at least one of speed and at least one direction of an aircraft having a self-propelled nosewheel, on the ground, is disclosed. The apparatus comprises a control arm; a control unit; means for transmitting information to said self-propelled nosewheel; means for receiving information at said self-propelled nosewheel; and means for controlling at least one of the speed and direction of said nosewheel; whereby airport ground staff can intuitively control the movements of said aircraft by holding said arm and moving it in the direction of required movement of said aircraft.
Abstract translation: 公开了一种用于使地面上的飞机反转的方法和装置，包括使用至少一个自走式起落架轮驱动飞行器。 公开了一种用于在地面上控制具有自推进的nosewheel的飞行器的速度和至少一个方向中的至少一个的装置。 该装置包括控制臂; 一个控制单元; 将信息传送到所述自推进式报刊的手段; 用于在所述自推进轮胎上接收信息的装置; 以及用于控制所述nosewheel的速度和方向中的至少一个的装置; 由此机场地勤人员可以通过握住所述臂并沿着所述飞行器的所需运动的方向移动它来直观地控制所述飞行器的运动。
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公开(公告)号：US08532957B2
公开(公告)日：2013-09-10
申请号：US12069614
申请日：2008-02-11
Applicant: Isaiah Watas Cox , Jonathan Sidney Edelson
Inventor： Isaiah Watas Cox , Jonathan Sidney Edelson
IPC: G01G19/00
CPC classification number: B64C25/405 , Y02T50/823
Abstract: A method of measuring the weight of an aircraft is disclosed. The method comprises, in a self-propelled aircraft undercarriage having a electrical rotating machine, the steps of: measuring the current and voltage going into the rotating machine using current and voltage measuring means, calculating the power into the rotating machine, measuring the speed (or torque or acceleration) of said machine using speed sensing means, and comparing the power and speed (or torque or acceleration) results with a database of power and speed relationships of comparable aircraft of varying weights.
Abstract translation: 公开了一种测量飞机重量的方法。 该方法包括在具有旋转电机的自走式飞机起落架中，采用电流和电压测量装置测量进入旋转机器的电流和电压，计算旋转机器的功率，测量速度（ 或扭矩或加速度），并且将功率和速度（或扭矩或加速度）结果与不同重量的可比飞机的功率和速度关系的数据库进行比较。
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公开(公告)号：US20090126369A1
公开(公告)日：2009-05-21
申请号：US12291258
申请日：2008-11-06
Applicant: Hans Juergen Walitzki , Jonathan Sidney Edelson , Rodney Thomas Cox
Inventor： Hans Juergen Walitzki , Jonathan Sidney Edelson , Rodney Thomas Cox
IPC: F02C7/268
CPC classification number: F04D27/004 , F02C7/268 , H02K15/02 , Y10T29/49009
Abstract: A turbine starter/generator machine for a turbine, said turbine comprising: at least one fan blade; at least one turbine enclosure; said starter/generator machine comprising: at least one rotor having rotor elements; at least one stator having stator elements; wherein said stator elements are mounted on said at least one air duct and said rotor elements are mounted on said at least one fan blade; whereby said stator elements magnetically interact with said rotor elements.
Abstract translation: 一种用于涡轮机的涡轮起动器/发电机，所述涡轮机包括：至少一个风扇叶片; 至少一个涡轮机外壳; 所述起动/发电机包括：具有转子元件的至少一个转子; 至少一个定子具有定子元件; 其中所述定子元件安装在所述至少一个空气管道上，并且所述转子元件安装在所述至少一个风扇叶片上; 由此所述定子元件与所述转子元件磁性地相互作用。
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