公开(公告)号：US10293947B2

公开(公告)日：2019-05-21

申请号：US13115081

申请日：2011-05-24

Applicant: Jin Hu ,  James M. Roman

Inventor： Jin Hu ,  James M. Roman

IPC: B64D15/12 ,  B64D33/02

Abstract: An aircraft heating system wherein the heater includes a haven (34) constructed from dielectric layers (40-50), conductive lanes (60), bus bars (70), and strips (80-150). Façade sections (41, 51, 61) of the dielectric layers (40-50) and the lanes (60) form the primary heating surface (31). The strips (80-150), along with sections (42, 52, 62) of the layers/lanes, form havens (34) for harbor sections (72) of the bus bars (70).

公开(公告)号：US20110290786A1

公开(公告)日：2011-12-01

申请号：US13115081

申请日：2011-05-24

Applicant: Jin Hu ,  James M. Roman

Inventor： Jin Hu ,  James M. Roman

IPC: H05B3/48

CPC classification number: B64D15/12 ,  B64D33/02 ,  B64D2033/0233 ,  B64D2033/0286

Abstract: An aircraft heating system wherein the heater includes a haven (34) constructed from dielectric layers (40-50), conductive lanes (60), bus bars (70), and strips (80-150). Façade sections (41, 51, 61) of the dielectric layers (40-50) and the lanes (60) form the primary heating surface (31). The strips (80-150), along with sections (42, 52, 62) of the layers/lanes, form havens (34) for harbor sections (72) of the bus bars (70).

Abstract translation: 一种飞机加热系统，其中加热器包括由电介质层（40-50），导电通道（60），汇流条（70）和条带（80-150）构成的避风港（34）。 电介质层（40-50）和通道（60）的外墙部分（41,41,61）形成主加热表面（31）。 条带（80-150）以及层/车道的部分（42,52,62）形成用于汇流条（70）的港口部分（72）的避风港（34）。

公开(公告)号：US20100204848A1

公开(公告)日：2010-08-12

申请号：US12702685

申请日：2010-02-09

Applicant: Galdemir C. Botura ,  Richard J. Cole ,  James M. Roman

Inventor： Galdemir C. Botura ,  Richard J. Cole ,  James M. Roman

IPC: H02J3/14 ,  B60L1/00 ,  G06F19/00 ,  B64D15/12

CPC classification number: B64D15/12 ,  H02J1/14 ,  H02J3/14 ,  H02J4/00 ,  Y10T307/336 ,  Y10T307/391 ,  Y10T307/406 ,  Y10T307/414

Abstract: An aircraft electric power supply system (10) for supplying electric power to onboard electric devices (20) during flight. To reduce the devices' power draw, the electric power is supplied via modulation at an increment-percentage that is determined by present conditions. An optimum portfolio can be established for the electrical devices (20) collectively, this portfolio being selected in accordance with an energy-management criterion or other aircraft objectives.

Abstract translation: 一种用于在飞行期间向车载电气设备（20）供电的飞行器电力供应系统（10）。 为了减少设备的功率消耗，电力通过调制以当前条件确定的增量百分比提供。 可以为电气设备（20）集体建立最佳投资组合，该投资组合是根据能源管理标准或其他飞机目标进行选择的。

公开(公告)号：US4760483A

公开(公告)日：1988-07-26

申请号：US913895

申请日：1986-10-01

Applicant: Michael M. Kugelman ,  James M. Roman

Inventor： Michael M. Kugelman ,  James M. Roman

IPC: H01H9/54 ,  H01H9/30

CPC classification number: H01H9/542 ,  H01H2009/545 ,  Y10T307/918

Abstract: In a circuit having an electro-mechanical relay, the contacts of which are subject to arcing, bridging across the electro-mechanical relay in a manner configured to begin conducting electrical current around the electro-mechanical relay prior to closing the electro-mechanical relay and to continue conducting electrical power around the electro-mechanical relay for a predetermined time after the onset of separation of contacts of the electro-mechanical relay pursuant to discontinuance of current flow through the electro-mechanical relay. An optical coupler is provided to ascertain a current flow through the relay coil effected to close the electro-mechanical relay contacts, and activates a shunt device in bridging electrical current flow around the electro-mechanical relay. The shunt device is provided to be substantially non-load carrying while the electro-mechanical relay is closed. Utility is found in protecting electro-mechanical relay contacts against damage due to arcing.

Abstract translation: 在具有机电继电器的电路中，其触点经受电弧放电，桥接跨机电继电器，其配置为在闭合机电继电器之前开始在电 - 机械继电器周围传导电流，并且 在电 - 机械继电器的电流中断之后，在电 - 机械继电器的触点分离开始之后的预定时间内，继续在机电继电器周围进行电力。 提供光耦合器以确定通过继电器线圈的电流，以便闭合机电继电器触点，并且激活分流装置以桥接机电继电器周围的电流。 在机电继电器闭合的同时，分流装置被设置为基本上不负载。 在保护机电继电器触点不会因电弧而损坏的情况下发现效用。

公开(公告)号：US4814931A

公开(公告)日：1989-03-21

申请号：US191728

申请日：1988-05-06

Applicant: Michael M. Kugelman ,  James M. Roman

Inventor： Michael M. Kugelman ,  James M. Roman

IPC: B64D15/14 ,  G05D23/19 ,  H02H9/00

CPC classification number: B64D15/14 ,  G05D23/19

Abstract: An all solid state timer-controller for the timed, sequential application of electrical current to loads within a circuit at high amperage, the circuit finding utility in the application of electrical current to de-icers employed aboard aircraft.

Abstract translation: 一种全固态定时器 - 控制器，用于定时，顺序地以高电流对电路内的负载施加电流，该电路用于向飞机上使用的除冰器施加电流。

公开(公告)号：US08260522B2

公开(公告)日：2012-09-04

申请号：US12702685

申请日：2010-02-09

Applicant: Galdemir C. Botura ,  Richard J. Cole ,  James M. Roman

Inventor： Galdemir C. Botura ,  Richard J. Cole ,  James M. Roman

IPC: G06F19/00

CPC classification number: B64D15/12 ,  H02J1/14 ,  H02J3/14 ,  H02J4/00 ,  Y10T307/336 ,  Y10T307/391 ,  Y10T307/406 ,  Y10T307/414

Abstract: An aircraft electric power supply system (10) for supplying electric power to onboard electric devices (20) during flight. To reduce the devices' power draw, the electric power is supplied via modulation at an increment-percentage that is determined by present conditions. An optimum portfolio can be established for the electrical devices (20) collectively, this portfolio being selected in accordance with an energy-management criterion or other aircraft objectives.

Abstract translation: 一种用于在飞行期间向车载电气设备（20）供电的飞行器电力供应系统（10）。 为了减少设备的功率消耗，电力通过调制以当前条件确定的增量百分比提供。 可以为电气设备（20）集体建立最佳投资组合，该投资组合是根据能源管理标准或其他飞机目标进行选择的。

公开(公告)号：US4745511A

公开(公告)日：1988-05-17

申请号：US913894

申请日：1986-10-01

Applicant: Michael M. Kugelman ,  James M. Roman

Inventor： Michael M. Kugelman ,  James M. Roman

IPC: H01H9/54 ,  H02H7/00

CPC classification number: H01H9/542 ,  H01H2009/545

Abstract: In a circuit having a electro-mechanical relay the contacts of which are subject to arcing, a shunt across the electro-mechanical relay configured to begin conducting electrical current across the electro-mechanical relay prior to closing the electro-mechanical relay contacts and to continue conducting electrical power across the electro-mechanical relay for a predetermined time after the onset of separation of electro-mechanical relay contacts pursuant to discontinuance of current flow through the elecro-mechanical relay. An optical coupler is employed to detect the current flow through the relay coil and activate a shunt device to initiate current flow around the electro-mechanical relay. The shunt device is configured to be substantially non-current load carrying while the electro-mechanical relay is closed. Utility is found in protecting relay contacts against damage due to arcing.

Abstract translation: 在具有机电继电器的电路中，其触点经受电弧放电，跨机电继电器的分流器被配置为在闭合机电继电器触点之前开始跨机电继电器的导通电流并且继续 在机电继电器触点开始分离之后的预定时间内，通过电 - 机械继电器的电流流过机电继电器。 使用光耦合器来检测通过继电器线圈的电流，并激活分流装置以启动机电继电器周围的电流。 分流装置被配置为当机电继电器闭合时基本上是非电流负载。 发现效用是为了保护继电器触点免受由于电弧引起的损坏。