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公开(公告)号：US20080099617A1
公开(公告)日：2008-05-01
申请号：US11883102
申请日：2006-02-03
申请人： Christopher Gilmore , Greg Fixter
发明人： Christopher Gilmore , Greg Fixter
摘要： An electrothermal heater mat for anti-icing or de-icing of a helicopter rotor blade or other aerodynamic surface comprises a substrate, such as a flexible polyimide sheet, bearing tracks of a material of selected electrical resistivity, these tracks being formed by printing onto the substrate with a thermosetting ink loaded with electrically conductive (e.g. carbon) particles. Electrical bus bars/terminals for the supply of electrical energy to the resistive tracks may also be printed, using an ink loaded with particles of higher conductivity material such as copper or silver.
摘要翻译： 用于直升机转子叶片或其它空气动力学表面的除冰或除冰的电热加热器垫包括诸如柔性聚酰亚胺片的基底，承载具有所选电阻率的材料的轨道，这些迹线通过印刷形成 具有负载有导电（例如碳）颗粒的热固性油墨的基材。 还可以使用装载有诸如铜或银的较高导电性材料的颗粒的油墨来印刷用于向电阻轨道供应电能的电汇流条/端子。
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公开(公告)号：US6129314A
公开(公告)日：2000-10-10
申请号：US10379
申请日：1998-01-21
CPC分类号： B64D15/163 , B64D15/00 , B64D15/12 , B64D15/14 , B64D15/166
摘要： A deicer comprises a skin heating device immediately subjacent an outer skin overlying an apex of a leading edge, and a skin deflection device immediately subjacent the outer skin chordwise aft of the apex. The skin heating device prevents the formation of ice over the apex and the skin deflection device deflects the outer skin to expulse ice formed chordwise aft of the apex. A controller controls the heating and deflection cycles to minimize power consumption of the deicer.
摘要翻译： 除冰机包括紧邻在前缘顶点的外皮下方的皮肤加热装置，以及紧邻在顶点的后外侧皮肤的皮肤偏转装置。 皮肤加热装置防止在顶点上形成冰，并且皮肤偏转装置使外部皮肤偏转，从而在尖端后方形成箭头形成的冰。 控制器控制加热和偏转循环以最小化除冰机的功率消耗。
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公开(公告)号：US5947418A
公开(公告)日：1999-09-07
申请号：US978045
申请日：1997-11-25
CPC分类号： B64D15/14
摘要： A number of resistive elements are incorporated into the aerofoil in the vicinity of its leading edge. Each of the resistive elements is electrically connected to the other resistive elements at its distal end and is fitted at its proximal end with means of connection to an electrical power supply. The resistive elements are split between a first set that includes at least two resistive elements and a second set that includes at least one resistive element. In service, the resistive of the first set are powered in turn, while each resistive element of the second set acts as a return path for the electricity and is powered continuously or almost continuously.
摘要翻译： 多个电阻元件被并入其前缘附近的机翼中。 每个电阻元件在其远端处电连接到另一个电阻元件，并且在其近端处装配有连接到电源的装置。 电阻元件在包括至少两个电阻元件的第一组和包括至少一个电阻元件的第二组之间分开。 在使用中，第一组的电阻依次供电，而第二组的每个电阻元件用作电力的返回路径，并连续地或几乎连续地供电。
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64.发明授权Method and apparatus for covering bodies with a uniform glow discharge plasma and applications thereof 失效用于覆盖具有均匀辉光放电等离子体的主体的方法和装置及其应用
公开(公告)号：US5669583A
公开(公告)日：1997-09-23
申请号：US254264
申请日：1994-06-06
申请人： John Reece Roth
发明人： John Reece Roth
IPC分类号： B63B1/34 , B64C23/00 , B64D15/14 , C23C16/40 , C23C16/50 , F15D1/12 , H01J37/32 , H05H1/46 , B64C1/38
CPC分类号： H01J37/32082 , B63B1/34 , B64C23/005 , B64D15/14 , C23C16/402 , C23C16/50 , F15D1/12 , H01J37/32532 , H05H1/46 , Y02T50/166 , Y02T70/121
摘要： Method and apparatus for covering a free-standing body with a uniform glow discharge plasma, particularly at atmospheric pressure. The method may be used to provide a body coated with such a plasma, and also to treat a workpiece.
摘要翻译： 用于用均匀辉光放电等离子体覆盖独立体的方法和装置，特别是在大气压下。 该方法可以用于提供涂覆有这种等离子体的物体，并且还可以处理工件。
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公开(公告)号：US5475204A
公开(公告)日：1995-12-12
申请号：US63367
申请日：1993-05-17
摘要： A de-icer for a structural member of an aircraft is provided. The de-icer includes first and second heaters having first and second electrically conductive strips, respectively. The first and second conductive strips are configured to form first and second marginal portions, respectively. The first and second heaters are positioned relative to each other such that the marginal portions are overlapped.
摘要翻译： 提供飞机结构构件的除冰器。 除冰器包括分别具有第一和第二导电条的第一和第二加热器。 第一和第二导电条被分别构造成形成第一和第二边缘部分。 第一和第二加热器相对于彼此定位，使得边缘部分重叠。
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公开(公告)号：US4868486A
公开(公告)日：1989-09-19
申请号：US58903
申请日：1987-06-05
申请人： Takahisa Shinoda
发明人： Takahisa Shinoda
CPC分类号： H02M1/083
摘要： An AC power control apparatus including a power circuit for supplying an AC current to a load, and a circuit connected to a power supply, for initiating energization of the load at a zero-cross point of an AC current waveform. A control circuit for controlling the change of energization time between a current turn on time to a current turn off time in units of AC waveform cycles, and a detector for detecting an AC zero level. From a given polarity of the AC current waveform, the initiating energization of the load and deenergization of the load at a zero-cross point of the AC current waveform is from the same polarity as the given polarity of the AC current waveform.
摘要翻译： 一种AC电力控制装置，包括用于向负载提供AC电流的电源电路和连接到电源的电路，用于在交流电流波形的零交叉点启动负载的通电。 控制电路，用于以交流波形周期为单位控制电流导通时间与当前关断时间之间的通电时间的变化;以及检测器，用于检测交流零电平。 从交流电流波形的给定极性，在交流电流波形的零交叉点处负载的启动通电和负载的断电是与交流电流波形的给定极性相同的极性。
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公开(公告)号：US4814931A
公开(公告)日：1989-03-21
申请号：US191728
申请日：1988-05-06
摘要： 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.
摘要翻译： 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。
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公开(公告)号：US4779036A
公开(公告)日：1988-10-18
申请号：US58941
申请日：1987-06-05
申请人： Takahisa Shinoda
发明人： Takahisa Shinoda
CPC分类号： G05D23/1913 , H02M5/257 , Y10T307/702
摘要： An AC power control apparatus includes a plurality of power supply circuits for generating powers having different maximum values, a switching circuit for, after an AC current is continuously set in a desired turn on control state, alternately selecting a first power supply circuit used until that time and a second power supply circuit for supplying a power approximating a power supplied to a load at that time from the plurality of power supply circuits, a turn on time control circuit for gradually shortening a turn on time of the first power supply circuit while gradually prolonging a turn on time of the second power supply circuit until the turn on time of the second power supply circuit corresponds to the entire period, and a circuit for changing the turn on time of the power supply circuit in units of periods of the AC current.
摘要翻译： 交流电力控制装置包括用于产生具有不同最大值的功率的多个电源电路，切换电路，用于在期望的转向控制状态下连续设置交流电流之后，交替地选择直到那时使用的第一电源电路 时间和第二电源电路，用于从多个电源电路提供近似供给到负载的电力的功率;开启时间控制电路，用于逐渐缩短第一电源电路的导通时间，同时逐渐缩短 延长第二电源电路的导通时间，直到第二电源电路的导通时间对应于整个周期，以及用于以交流电流的周期为单位改变电源电路的导通时间的电路 。
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69.发明授权Switching system for cyclic supply of electrical power to a plurality of loads 失效用于向多个负载循环供应电力的开关系统
公开(公告)号：US4410794A
公开(公告)日：1983-10-18
申请号：US258722
申请日：1981-04-29
申请人： David C. Williams
发明人： David C. Williams
IPC分类号： B64D15/14 , H03K17/693 , H05B1/02
CPC分类号： B64D15/14 , H03K17/693 , Y10T307/477 , Y10T307/484
摘要： A switching system for sequential connection of a plurality of loads to an alternating current supply comprises a computer for generating switch selection data in the form of serial bits along a single line to a distributor arrangement which decodes the selection data and provides control signals to switch devices which connect the loads to the supply. The distributor arrangement includes a circuit for inhibiting supply of the control signals to the respective switch devices unless the voltage of the supply phase connected by the device is substantially zero. Additionally the control signals are time-advanced with respect to the zero voltage conditions so that the switch devices can be placed in states in which they can connect a load before disconnection of a preceding load.
摘要翻译： 用于将多个负载顺序连接到交流电源的开关系统包括计算机，用于沿着单个线路将串行位形式的开关选择数据生成到分配器装置，该分配器装置对选择数据进行解码并向开关装置提供控制信号 将负载连接到电源。 分配器装置包括用于禁止向各个开关装置提供控制信号的电路，除非由装置连接的电源相位的电压基本为零。 此外，控制信号相对于零电压条件是时间提前的，使得开关装置可以被置于在先前负载断开之前它们可以连接负载的状态。
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公开(公告)号：US4021008A
公开(公告)日：1977-05-03
申请号：US579152
申请日：1975-05-20
申请人： Fritz Eichenauer
发明人： Fritz Eichenauer
摘要： A device for preventing ice formation on parts of aircraft-support surfaces (wings or aerofoils), propellers, rotor blades or the like-comprises electrical resistance heaters embedded in a shell of thermally conducting material (e.g. aluminium sheet or moulding) sheathing the aircraft part. Thermally insulating, thermally conducting and electrically insulating layers may be provided within the shell. The heaters, or some of them, may be controlled by a temperature sensor in or on the shell.
摘要翻译： 用于防止飞行器支撑表面（翼或翼型体），螺旋桨，转子叶片等的部件上的冰形成的装置包括嵌入在导热材料（例如铝板或模制件）的外壳中的电阻加热器， 。 可以在壳体内设置绝热，导热和电绝缘的层。 加热器或其中的一些可以由外壳内或外壳上的温度传感器控制。
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