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公开(公告)号：US11798324B2
公开(公告)日：2023-10-24
申请号：US16721601
申请日：2019-12-19
发明人： Robert A. Lockmiller , Amit Toprani
CPC分类号： G07C5/0808 , F02C7/26 , F02P15/003 , F02P17/12 , H01T13/60 , F05D2220/32 , F05D2260/83
摘要： A device for monitoring a life condition of a spark igniter in a gas turbine ignition system. The device includes an evaluation circuit having circuit components that include a hold capacitor, a transistor, and an operational amplifier arranged to form a sample-and-hold circuit, wherein an igniter spark impulse signal is applied to an input node of the evaluation circuit causing the transistor to turn on and the hold capacitor to discharge for a duration of the igniter spark impulse signal, and wherein a discharged voltage at the hold capacitor is maintained and output by the operational amplifier, the discharged voltage representing the duration of the igniter spark impulse and indicating the life condition of the spark igniter.
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公开(公告)号：US07880281B2
公开(公告)日：2011-02-01
申请号：US12194933
申请日：2008-08-20
申请人： Steve J. Kempinski
发明人： Steve J. Kempinski
IPC分类号： H01L23/495 , H01L23/34 , H01L23/498
CPC分类号： H01L23/24 , H01L23/49844 , H01L24/34 , H01L2924/00014 , H01L2924/01006 , H01L2924/01013 , H01L2924/01023 , H01L2924/01029 , H01L2924/01033 , H01L2924/01082 , H01L2924/1301 , H01L2924/13055 , H01L2924/13091 , H01L2924/14 , H01L2924/15787 , H01L2924/00 , H01L2224/37099
摘要： A switching assembly is disclosed for a high voltage aircraft ignition system. The switching assembly includes a ceramic substrate and switch die that includes an anode bonded to an electrical pad on the ceramic substrate. The switch die includes a semiconductor device having a plurality of interleaved gates and cathodes, and includes a ceramic cap having at least one gate pad connected to the gates and at least one cathode pad connected to the cathodes. The switching assembly includes leads connected to the gate pad, the cathode pad, and the electrical pad on the substrate. The switch die and a portion of the leads are potted to form the completed assembly.
摘要翻译： 公开了一种用于高压飞行器点火系统的开关组件。 开关组件包括陶瓷衬底和开关管芯，其包括结合到陶瓷衬底上的电焊盘的阳极。 开关管芯包括具有多个交错栅极和阴极的半导体器件，并且包括具有连接到栅极的至少一个栅极焊盘和连接到阴极的至少一个阴极焊盘的陶瓷帽。 开关组件包括连接到栅极焊盘，阴极焊盘和衬底上的电焊盘的引线。 开关模具和引线的一部分被封装以形成完成的组件。
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公开(公告)号：US08687394B2
公开(公告)日：2014-04-01
申请号：US12607090
申请日：2009-10-28
CPC分类号： H02M7/06
摘要： An aircraft power supply for providing DC power with improved power quality characteristics. The aircraft power supply includes a transformer control system that can use closed-loop feedback from a DC power output to control switches that can short primary windings turns of a step-down transformer. By shorting turns in the primary, the transformer control system can control or manipulate the turns ratio in the transformer and compensate for decreases in the DC power output.
摘要翻译： 用于提供直流电源的飞机电源具有改进的电力质量特性。 飞机电源包括变压器控制系统，其可以使用来自直流电力输出的闭环反馈来控制可以使降压变压器的初级绕组匝短的开关。 通过短路主变压器，变压器控制系统可以控制或操纵变压器的匝数比，并补偿直流电源输出的减小。
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公开(公告)号：US20240223048A1
公开(公告)日：2024-07-04
申请号：US18544421
申请日：2023-12-18
IPC分类号： H02K11/33 , B64D27/04 , F02P1/08 , H02K1/27 , H02K11/215
CPC分类号： H02K11/33 , B64D27/04 , F02P1/08 , H02K1/27 , H02K11/215
摘要： An aircraft piston engine magneto having a magnetic rotor and an ignition circuit with a reconfigurable charging coil inductively coupled to magnetic rotor. The charging coil includes multiple coils inductively powered by the magnetic rotor and electronically reconfigurable from a higher turn, lower amperage power coil for use when running at low speeds into a lower turn, higher amperage coil at higher speeds. The charging coil is configured into the higher turn coil by electronically connecting the multiple coils in series, and into the lower turn power coil by electronically connecting the coils in parallel. The ignition circuit is a fully electronic ignition circuit that generates and distributes ignition pulses to the piston engine spark plugs using only non-mechanically actuated electrical components within the magneto.
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公开(公告)号：US20130111914A1
公开(公告)日：2013-05-09
申请号：US13459053
申请日：2012-04-27
申请人： Steve J. Kempinski
发明人： Steve J. Kempinski
IPC分类号： F02C7/266
CPC分类号： F02C7/266 , F05D2220/768
摘要： An aircraft ignition system having a power circuit, a control circuit, and a discharge circuit and coupled to the spark plugs of an aircraft engine. The power circuit may include two independent power sources; e.g., alternator power (such as a permanent magnet alternator) and power from aircraft or DC power bus. The control circuit may control one or more aspects of the discharge circuit, e.g., the ignition timing. And the discharge circuit may trigger a capacitive discharge ignition event to the spark plugs.
摘要翻译： 一种具有电源电路，控制电路和放电电路并与飞机发动机的火花塞耦合的飞行器点火系统。 电源电路可以包括两个独立的电源; 例如交流发电机功率（例如永磁式交流发电机）和来自飞行器或直流电力总线的电力。 控制电路可以控制放电电路的一个或多个方面，例如点火正时。 并且放电电路可能触发火花塞的电容放电点火事件。
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公开(公告)号：US10030584B2
公开(公告)日：2018-07-24
申请号：US15410901
申请日：2017-01-20
发明人： Steve J. Kempinski
摘要： A solid state spark device that operates as a two terminal spark gap in a CDI exciter of an aircraft ignition system. The device includes a triggering transformer, a triggering circuit, and a control circuit. The triggering circuit is electrically connected to a first coil of the transformer and includes circuit elements connected to supply current to the first coil upon charging of the triggering circuit up to a triggering voltage. This current through the first coil of the triggering transformer induces an output in a second coil of the transformer. The control circuit is electrically connected to the second coil and includes a switch controlled by the output from the second coil. The switch, when activated by the triggering circuit, discharges energy from the exciter into an igniter of the aircraft ignition system.
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公开(公告)号：US07750496B2
公开(公告)日：2010-07-06
申请号：US12052821
申请日：2008-03-21
CPC分类号： H02J9/06 , Y10T307/625 , Y10T307/735
摘要： A power supply unit that provides uninterrupted power to an aircraft power bus during switchovers of the aircraft bus from one power source to another. The power supply unit includes circuitry to distinguish between loss of bus power due to switchovers between power sources and loss of bus power due to shutdown of the aircraft. The power supply unit includes a low voltage lockout circuit to interrupt the supply of power when the aircraft bus voltage falls below a minimum value.
摘要翻译： 电源单元，用于在飞机总线从一个电源切换到另一个电源期间，为飞机电源总线提供不间断电源。 电源单元包括用于区分由于电源之间的切换而导致的总线功率损耗以及由于飞机关闭而造成的总线功率损失的电路。 电源单元包括一个低压锁定电路，用于当飞机总线电压降到最低值以下时中断供电。
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