-
公开(公告)号：US06657334B1
公开(公告)日：2003-12-02
申请号：US09713654
申请日：2000-11-15
Applicant: Jonathan Sidney Edelson
Inventor： Jonathan Sidney Edelson
IPC: H02K700
Abstract: A high phase order induction machine drive system is disclosed. This has an inverter system for the synthesis of a plurality of phases of alternating current output, and a N-phase induction motor (N is greater than 3). The motor is connected to the inverter terminals so that each motor phase is electrically connected to a first inverter terminal and a second inverter terminal S+1 inverter terminals distant from the first inverter terminal in order of electrical phase angle (S in the skip number). The phase angle difference between the pair of inverter terminals to which each motor phase is connected is identical for each motor phase.
Abstract translation: 公开了一种高阶感应电机驱动系统。 这具有用于合成交流输出的多相的逆变器系统和N相感应电动机（N大于3）。 电动机连接到逆变器端子，使得每个电动机相以电相位角（S为跳过数）的顺序与第一逆变器端子和远离第一逆变器端子的第二逆变器端子S + 1逆变器端子电连接， 。 每个电动机相连接的一对逆变器端子之间的相位角差对于每个电动机相位是相同的。
-
公开(公告)号：US06348775B1
公开(公告)日：2002-02-19
申请号：US09570166
申请日：2000-05-11
Applicant: Jonathan Sidney Edelson , Brian Von Herzen
Inventor： Jonathan Sidney Edelson , Brian Von Herzen
IPC: H02P124
Abstract: A polyphase induction motor is operated by an inverter drive system comprising a logic level controller. A number, preferably twelve or more, of independently driven phases causes harmonic fields, up to a number equal to the number of phases, to oscillate in synchrony with the fundamental oscillating field. A pulse-width modulation (“PWM”) carrier is used by the logic level controller to synthesize a desired drive alternating current, in which the pulsing distortion produced by the pulse width modulation produces a synchronous oscillating field in the driven polyphase induction motor.
Abstract translation: 多相感应电动机由包括逻辑电平控制器的逆变器驱动系统操作。 独立驱动的相位的数量，优选地十二个或更多个，使相等数量的相位的谐波场与基本振荡场同步地振荡。 逻辑电平控制器使用脉冲宽度调制（“PWM”）载波来合成期望的驱动交流电，其中由脉冲宽度调制产生的脉冲失真在驱动的多相感应电动机中产生同步振荡场。
-
公开(公告)号：US06285769B1
公开(公告)日：2001-09-04
申请号：US08843678
申请日：1997-04-10
Applicant: Jonathan Sidney Edelson , Nicholas Paul Ward
Inventor： Jonathan Sidney Edelson , Nicholas Paul Ward
IPC: H04R300
CPC classification number: H04R3/002
Abstract: The present invention is a microphone that applies the principle of negative feedback directly to the diaphragm, greatly reducing the non-linearity of the diaphragm. In a further embodiment, digital negative feedback is used, incorporating the diaphragm into the digitization loop of a sigma-delta converter, creating a direct sound pressure to digital electrical output converter. In one embodiment, positive feedback is used in an analog circuit, causing a negative feedback response on the diaphragm.
Abstract translation: 本发明是将负反馈原理直接应用于隔膜的麦克风，大大降低了隔膜的非线性。 在另一实施例中，使用数字负反馈，将隔膜结合到Σ-Δ转换器的数字化环路中，产生对数字电输出转换器的直接声压。 在一个实施例中，在模拟电路中使用正反馈，导致隔膜上的负反馈响应。
-
公开(公告)号：US6117344A
公开(公告)日：2000-09-12
申请号：US45299
申请日：1998-03-20
Applicant: Isaiah Watas Cox , Avto Tavkhelidze , Jonathan Sidney Edelson , Stuart Harbron
Inventor： Isaiah Watas Cox , Avto Tavkhelidze , Jonathan Sidney Edelson , Stuart Harbron
CPC classification number: B82Y10/00 , B82Y40/00 , G03F7/0002 , H01J1/30 , H01J45/00 , H01J9/022 , G03F7/2059 , G03F7/2065
Abstract: Methods for fabricating nano-structured surfaces having geometries in which the passage of elementary particles through a potential barrier is enhanced are described. The methods use combinations of electron beam lithography, lift-off, and rolling, imprinting or stamping processes.
Abstract translation: 描述了具有几何形状的纳米结构表面的方法，其中基本粒子通过势垒的通过被增强。 该方法使用电子束光刻，剥离和滚压，压印或冲压工艺的组合。
-
公开(公告)号：US5981866A
公开(公告)日：1999-11-09
申请号：US016089
申请日：1998-01-30
Applicant: Jonathan Sidney Edelson
Inventor： Jonathan Sidney Edelson
IPC: H01L31/00
CPC classification number: H01J40/16
Abstract: Manufacture of a photoelectric converter by a photolithographic or stamping process prior to coating with a photoelectrically emissive material is described. This gives an economic and simple means of mass-producing photoelectric converter cells, and in one aspect is analogous to that used for pressing optical discs.
Abstract translation: 描述在用光电发射材料涂覆之前通过光刻或冲压工艺制造光电转换器。 这提供了大量生产光电转换器电池的经济和简单的方法，并且在一个方面类似于用于按压光盘的方式。
-
Patent Agency Ranking
公开(公告)号：US09216819B2
公开(公告)日：2015-12-22
申请号：US13074801
申请日：2011-03-29
Applicant: Neal Gilleran , Robert M. Sweet , Jonathan Sidney Edelson , Rodney T. Cox , Isaiah Watas Cox
Inventor： Neal Gilleran , Robert M. Sweet , Jonathan Sidney Edelson , Rodney T. Cox , Isaiah Watas Cox
IPC: B64C25/40
CPC classification number: B64C25/405 , Y02T50/823
Abstract: A wheel design is provided for an aircraft landing gear wheel that is configured to maximize the space available within a landing gear wheel well to support a motor driver assembly that drives the aircraft wheel when the aircraft is on the ground. The wheel includes inboard and outboard support walls that are spaced apart a selected distance along the wheel axle so that the motor driver assembly components are substantially completely contained within the wheel space defined by the support walls. The preferred motor driver assembly includes an electric motor and a gear and clutch assembly operatively connected to the wheel to drive the wheel and move the aircraft on the ground. The wheel and motor driver assembly described herein may be retrofitted in an existing aircraft wheel without changing existing landing gear components, including tires, piston, and axle.
Abstract translation: 为飞机起落架齿轮提供轮设计，其被配置为使起落架轮井内的可用空间最大化，以支持在飞行器处于地面时驱动飞行器轮的马达驱动器组件。 车轮包括沿着轮轴间隔开选定距离的内侧和外侧支撑壁，使得电动机驱动器组件部件基本上完全包含在由支撑壁限定的车轮空间内。 优选的马达驱动器组件包括电动马达和可操作地连接到车轮的齿轮和离合器组件，以驱动车轮并使飞机在地面上移动。 本文所述的车轮和马达驱动器组件可以在现有的飞机车轮中改装而不改变现有的起落架部件，包括轮胎，活塞和车轴。
-
公开(公告)号：US08714481B2
公开(公告)日：2014-05-06
申请号：US13082932
申请日：2011-04-08
Applicant: Robert M. Sweet , Neal Gilleran , Jonathan Sidney Edelson , Isaiah Watas Cox , Rodney T. Cox
Inventor： Robert M. Sweet , Neal Gilleran , Jonathan Sidney Edelson , Isaiah Watas Cox , Rodney T. Cox
IPC: B64C25/50
CPC classification number: B64C25/405 , Y02T50/823
Abstract: A wheel design is provided for an aircraft landing gear wheel that is configured to maximize the space available within a landing gear wheel well to support a geared motor assembly that drives the aircraft wheel when the aircraft is on the ground. The wheel includes inboard and outboard support walls that are spaced apart a selected distance along the wheel axle so that the geared motor assembly components are substantially completely contained within the wheel space defined by the support walls. The preferred motor driver assembly includes an electric motor and a gear and clutch assembly operatively connected to the wheel to drive the wheel and move the aircraft on the ground. The wheel and motor driver assembly described herein may be retrofitted in an existing aircraft wheel without changing existing landing gear components, including tires, piston, and axle.
Abstract translation: 为飞机起落架齿轮提供轮设计，其被配置为使起落架轮井内的可用空间最大化，以支撑当飞机在地面上时驱动飞行器轮的齿轮传动马达组件。 车轮包括沿着轮轴间隔开选定距离的内侧和外侧支撑壁，使得齿轮传动的马达组件部件基本上完全包含在由支撑壁限定的车轮空间内。 优选的马达驱动器组件包括电动马达和可操作地连接到车轮的齿轮和离合器组件，以驱动车轮并使飞机在地面上移动。 本文所述的车轮和马达驱动器组件可以在现有的飞机车轮中改装而不改变现有的起落架部件，包括轮胎，活塞和车轴。
-
公开(公告)号：US08240599B2
公开(公告)日：2012-08-14
申请号：US12217635
申请日：2008-07-07
Applicant: Jonathan Sidney Edelson , Isaiah Watas Cox , Daniel Liviu Barbalata
Inventor： Jonathan Sidney Edelson , Isaiah Watas Cox , Daniel Liviu Barbalata
IPC: B64C25/50
CPC classification number: B64F1/22 , B64C25/405 , Y02T50/823 , Y10S180/904
Abstract: An apparatus for controlling the movement 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: 公开了一种用于控制在地面上具有自推进式nosewheel的飞行器的运动的装置。 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。
-
公开(公告)号：US08198746B2
公开(公告)日：2012-06-12
申请号：US11900614
申请日：2007-09-11
Applicant: Jonathan Sidney Edelson
Inventor： Jonathan Sidney 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。
-
公开(公告)号：US20110284685A1
公开(公告)日：2011-11-24
申请号：US13074801
申请日：2011-03-29
Applicant: Neal Gilleran , Robert M. Sweet , Jonathan Sidney Edelson , Rodney T. Cox , Isaiah Watas Cox
Inventor： Neal Gilleran , Robert M. Sweet , Jonathan Sidney Edelson , Rodney T. Cox , Isaiah Watas Cox
IPC: B64C25/50
CPC classification number: B64C25/405 , Y02T50/823
Abstract: A wheel design is provided for an aircraft landing gear wheel that is configured to maximize the space available within a landing gear wheel well to support a motor driver assembly that drives the aircraft wheel when the aircraft is on the ground. The wheel includes inboard and outboard support walls that are spaced apart a selected distance along the wheel axle so that the motor driver assembly components are substantially completely contained within the wheel space defined by the support walls. The preferred motor driver assembly includes an electric motor and a gear and clutch assembly operatively connected to the wheel to drive the wheel and move the aircraft on the ground. The wheel and motor driver assembly described herein may be retrofitted in an existing aircraft wheel without changing existing landing gear components, including tires, piston, and axle.
Abstract translation: 为飞机起落架齿轮提供轮设计，其被配置为使起落架轮井内的可用空间最大化，以支持在飞行器处于地面时驱动飞行器轮的马达驱动器组件。 车轮包括沿着轮轴间隔开选定距离的内侧和外侧支撑壁，使得电动机驱动器组件部件基本上完全包含在由支撑壁限定的车轮空间内。 优选的马达驱动器组件包括电动马达和可操作地连接到车轮的齿轮和离合器组件，以驱动车轮并使飞机在地面上移动。 本文所述的车轮和马达驱动器组件可以在现有的飞机车轮中改装而不改变现有的起落架部件，包括轮胎，活塞和车轴。
-
-
-
-
-
-
-
-
-
Search Results
70
records
(took 0.039 seconds)
