MEMORY CONSERVATION DATA ALIGNMENT METHOD FOR SOLID STATE RECORDING
    12.
    发明申请
    MEMORY CONSERVATION DATA ALIGNMENT METHOD FOR SOLID STATE RECORDING 审中-公开
    用于实时状态记录的记忆保存数据对齐方法

    公开(公告)号:WO1993013520A2

    公开(公告)日:1993-07-08

    申请号:PCT/US1992010941

    申请日:1992-12-16

    IPC: G11B0

    CPC classification number: G11C7/16 G11C2207/16

    Abstract: A recording system and process minimizes the storage capacity for recording multi-channel data into the memory space normally allocated to a single channel for a predetermined time period without compressing the data. In order to enable the data to be correlated with either real or relative time, the data is recorded along with its channel number and stored sequentially in an electronic memory in predetermined time increments. Additionally, the channel activity is monitored and stored. By recording the channel number with the data and identifying the periods of channel activity, the recorded data can be correlated with the time during which it was recorded. The recording apparatus in accordance with the present invention is particularly well suited for minimizing memory requirements for recording multi-channel sequential data, such as in certain voice communications, as well as simplex and half duplex communications even in situations where there is some overlap in channel activity without the use of data compression.

    Abstract translation: 记录系统和处理将存储容量最小化,以将多通道数据记录到通常分配给单个通道的存储空间中达预定时间段,而不压缩数据。 为了使数据能够与实时或相对时间相关联,数据与其通道号一起被记录,并以预定的时间增量顺序地存储在电子存储器中。 另外,监视和存储通道活动。 通过记录具有数据的通道号和识别通道活动的周期,记录的数据可以与其记录的时间相关联。 根据本发明的记录装置特别适用于最小化用于记录多信道顺序数据的存储器要求,例如在某些语音通信中,以及即使在通道中存在一些重叠的情况下的单工和半双工通信 活动没有使用数据压缩。

    GROUND PROXIMITY WARNING INSTRUMENT USING FLIGHT PATH MODULATION OF GLIDE SLOPE ALERTING FUNCTION
    13.
    发明申请
    GROUND PROXIMITY WARNING INSTRUMENT USING FLIGHT PATH MODULATION OF GLIDE SLOPE ALERTING FUNCTION 审中-公开
    地面临时警告仪器使用飞行路径调整滑坡坡度功能

    公开(公告)号:WO1993006574A1

    公开(公告)日:1993-04-01

    申请号:PCT/US1992007823

    申请日:1992-09-16

    CPC classification number: G05D1/0615 G05D1/0676

    Abstract: A ground proximity warning system monitors the flight path angle (78) or barometric or inertially derived descent rate (74) of the aircraft and modulates the glide slope alerting function (80) in accordance with flight path angle (78) or descent rate (74) when the aircraft is not descending rapidly even though it is below the glide slope in order to reduce nuisance warnings without compromising system sensitivity. Alternatively, the repetition rate of the alert may be varied as a function of the flight path angle (78) or descent rate (74) to provide less frequent alerts when the aircraft is not descending rapidly.

    PLURAL INVERTER CONTROL ARRANGEMENT
    14.
    发明申请
    PLURAL INVERTER CONTROL ARRANGEMENT 审中-公开
    多变频器控制装置

    公开(公告)号:WO1993004522A1

    公开(公告)日:1993-03-04

    申请号:PCT/US1992006835

    申请日:1992-08-14

    CPC classification number: H02M7/493 H02J3/46

    Abstract: An inverter arrangement for converting DC to AC having a first inverter (11) with an input for receiving DC and an output for providing a first inverter output, a second inverter (13) having an input for receiving DC and an output for providing a second inverter output, an AC output circuit (51) having a first input for receiving the first inverter output, a second input for receiving the second inverter output, and an AC output for providing AC based upon the first inverter output and the second inverter output, and a controller (49) for controlling the first inverter to minimize DC content in a first inverter output, and for controlling the second inverter output based upon DC content between the first inverter output and the second inverter output to minimize DC content in the second inverter output.

    CORIOLIS RATE SENSOR USING TUNNEL-EFFECT DISPLACEMENT SENSOR
    15.
    发明申请
    CORIOLIS RATE SENSOR USING TUNNEL-EFFECT DISPLACEMENT SENSOR 审中-公开
    CORIOLIS RATE传感器使用隧道效应位移传感器

    公开(公告)号:WO1993000589A1

    公开(公告)日:1993-01-07

    申请号:PCT/US1992004851

    申请日:1992-06-03

    CPC classification number: G01C19/5607

    Abstract: A rate detection system (10) uses a balanced resonant sensor (12) having first and second tines (14, 16) interconnected with a mounting pad (20). A sensing circuit (50) including a tunnel effect displacement sensor (38) having a first probe (40) connected to the mounting pad (20) and a second probe (42) connected to a reference pad (32) detects an output signal having a Coriolis component. A feedback circuit provides a compensation signal to the balanced resonant sensor (12).

    Abstract translation: 速率检测系统(10)使用具有与安装垫(20)互连的第一和第二尖齿(14,16)的平衡谐振传感器(12)。 一种感测电路(50),包括具有连接到安装垫(20)的第一探头(40)和连接到参考焊盘(32)的第二探头(42)的隧道效应位移传感器(38),检测输出信号, 科里奥利组件。 反馈电路向平衡谐振传感器(12)提供补偿信号。

    DUAL ROTOR TORQUE MOTOR
    16.
    发明申请
    DUAL ROTOR TORQUE MOTOR 审中-公开
    双转子扭矩电机

    公开(公告)号:WO1992014293A1

    公开(公告)日:1992-08-20

    申请号:PCT/US1992000919

    申请日:1992-02-04

    CPC classification number: G01C19/56

    Abstract: A torque motor for rotatably driving a rate sensor (10, 100) which includes a permanent magnet (30) that is magnetically coupled to an upper rotor (18, 106) and a lower rotor (44, 110). With no electrical current flowing through electromagnetic coils (56, 58), a plurality of flexures (46) that connect the upper and lower rotors to a base (12) provide a spring bias force sufficient to maintain an upper tab centered in a slot (66) and thus, equidistant between each of two lower tabs (62). As the electric current flows through the electromagnetic coils, distribution of the magnetic flux produced by permanent magnet changes so that the upper tab is attracted toward one of the electromagnetic coils and repelled away from the other.

    VELOCITY SENSOR THAT IS SENSITIVE IN ONLY ONE DEGREE OF FREEDOM
    17.
    发明申请
    VELOCITY SENSOR THAT IS SENSITIVE IN ONLY ONE DEGREE OF FREEDOM 审中-公开
    速度传感器只有一个自由度敏感

    公开(公告)号:WO1992014158A1

    公开(公告)日:1992-08-20

    申请号:PCT/US1992000920

    申请日:1992-02-05

    CPC classification number: G01P3/58 G01P3/46 G01P3/52

    Abstract: The invention comprises a velocity sensor (10, 30, 50, 60, 70, 110). The using differential flux splitting, and by sensing changes in flux, common mode effects are removed. A permanent magnet (17, 33, 55, 65, 71, 131) is used to create a flux field, and multiple return paths are used to split the flux. A plurality of pole pieces (20-21, 39-40, 58-59-66-67, 72-73, 111-112) simultaneously move an equal amount in relation to the return path for differentially varying the amount of flux carried by each return path (13-14, 34-36, 52-53, 63-64, 73A-B and 75A-C, 115-117), to thereby induce a differential voltage in secondary coils (15-16, 37-38, 56-57, 68-69, 80-83 and 90-91, 140-143 and 150-153). The pole pieces and return paths are overlapped by an amount to ensure that one may move relative to the other a limited extent in directions not parallel to the sensitive axis without effecting a change in the net overlapped area, and the coils are arranged in series-connected, oppositely wound pairs so that common mode error signals are cancelled.

    HYBRID COMPOSITE SANDWICH STRUCTURE
    18.
    发明申请
    HYBRID COMPOSITE SANDWICH STRUCTURE 审中-公开
    混合复合砂浆结构

    公开(公告)号:WO1991014556A1

    公开(公告)日:1991-10-03

    申请号:PCT/US1991000707

    申请日:1991-02-01

    Abstract: Current processes for the formation of hybrid composite sandwich structures are expensive, often result in weak unsound products, require time and labor intensive operations and are not readily adaptable for custom design work. These and other problems are solved by relatively simple and inexpensive process producing hybrid composite sandwiched structures which includes placing core materials (24) sandwiched by multiple layers including at least one ceramic layer (46) or metallic layer (38) and having polymeric films (32, 34, 40, 42) positioned between substantially all the layers in a mold cavity (18). When the contents of the mold cavity (18) are heated to consolidate this structure, the polymeric films (32, 34, 40, 42) melt and act as an adhesive between the layers of the structure formed.

    Abstract translation: 形成混合复合夹层结构的当前工艺是昂贵的,通常导致不良产品薄弱,需要时间和劳动密集的操作,并且不容易适用于定制设计工作。 这些和其他问题通过相对简单和便宜的工艺生产混合复合夹层结构来解决,其中包括将芯材料(24)放置在由多个层(包括至少一个陶瓷层)或金属层(38)夹在中间并具有聚合物膜 ,34,40,42),其位于模腔(18)中的基本上所有的层之间。 当模腔(18)的内容物被加热以固结该结构时,聚合物膜(32,34,40,42)熔化并充当形成的结构层之间的粘合剂。

    STEPPED-WAVEFORM INVERTER WITH FOUR SUBINVERTERS
    19.
    发明申请
    STEPPED-WAVEFORM INVERTER WITH FOUR SUBINVERTERS 审中-公开
    具有四个子转换器的STEPPED-WAVEFORM逆变器

    公开(公告)号:WO1991009453A1

    公开(公告)日:1991-06-27

    申请号:PCT/US1990006566

    申请日:1990-11-08

    CPC classification number: H02M7/49

    Abstract: Previously, while stepped-waveform inverters approximate a sine wave to reduce the size of filters needed at the output of such inverters, efficient and effective methods of controlling such inverters have heretofore been lacking. In order to overcome these drawbacks of previous inverters, an inverter (24) for use in a power conversion system (10) of the type used in an aircraft, for example, is provided with a first subinverter pair (30) that generates a first pair of waveforms and a second subinverter pair (32) that generates a second pair of waveforms. The two subinverter pairs (30, 32) are connected to a summing transformer (31, 33) having two pairs of primary windings (80, 92) and a plurality of secondary windings (90, 98) coupled to the primary windings (80, 92). A regulator (50, 52) is coupled to the output of the summing transformer (31, 33) and varies the phase angles between the waveforms generated by the two subinverter pairs (30, 32) based upon the voltage and current at the output of the summing transformer (31, 33) in order to regulate the voltage at the output of the summing transformer (31, 33).

    Abstract translation: 以前,阶梯式波形逆变器近似正弦波以减小这种逆变器的输出所需的滤波器的尺寸,但迄今为止,缺乏控制这种逆变器的有效和有效的方法。 为了克服以前的逆变器的这些缺点,例如在飞机中使用的类型的功率转换系统(10)中使用的逆变器(24)设置有第一子逆变器对(30),其产生第一 一对波形和产生第二对波形的第二子逆变器对(32)。 两个副变压器对(30,32)连接到具有两对初级绕组(80,92)和耦合到初级绕组(80,92)的多个次级绕组(90,98)的求和变压器(31,33) 92)。 调节器(50,52)耦合到求和变压器(31,33)的输出,并且基于在输出端的电压和电流来改变由两个副变换器对(30,32)产生的波形之间的相位角 求和变压器(31,33),以便调节求和变压器(31,33)的输出处的电压。

    STEPPED-WAVEFORM INVERTER WITH SIX SUBINVERTERS
    20.
    发明申请
    STEPPED-WAVEFORM INVERTER WITH SIX SUBINVERTERS 审中-公开
    具有六个子转换器的STEPPED-WAVEFORM逆变器

    公开(公告)号:WO1991009452A1

    公开(公告)日:1991-06-27

    申请号:PCT/US1990006563

    申请日:1990-11-08

    CPC classification number: H02M7/49

    Abstract: Previously while stepped-waveform inverters approximate a sine wave to reduce the size of filters needed at the output of such inverters, efficient and effective methods of controlling such inverters have heretofore been lacking. In order to overcome these drawbacks of previous inverters, an inverter (24) for use in a power conversion system (10) of the type used in an aircraft, for example, is provided with a first subinverter pair (30) that generates a first pair of waveforms, a second subinverter pair (32) that generates a second pair of waveforms, and a third subinverter pair (34) that generates a third pair of waveforms. The three subinverter pairs (30, 32, 34) are connected to a summing transformer having first, second and third transformers (31, 33, 35). A regulator (50, 51) is coupled to the output of the summing transformer (31, 33, 35) and varies the phase angles between the three pairs of waveforms generated by the three subinverter pairs (30, 32, 34) based upon the voltage and current at the output of the summing transformer (31, 33, 35) in order to regulate the voltage at the output of the summing transformer (31, 33, 35).

    Abstract translation: 以前,阶梯式波形逆变器近似正弦波以减小在这种逆变器的输出端所需的滤波器的尺寸,但迄今为止,缺乏控制这种逆变器的有效和有效的方法。 为了克服以前的逆变器的这些缺点,例如在飞机中使用的类型的功率转换系统(10)中使用的逆变器(24)设置有第一子逆变器对(30),其产生第一 一对波形,产生第二对波形的第二子逆变器对(32)和产生第三对波形的第三子反转器对(34)。 三个副变换器对(30,32,34)连接到具有第一,第二和第三变压器(31,33,35)的求和变压器。 调节器(50,51)耦合到求和变压器(31,33,35)的输出,并且基于所述三个副变换器对(30,32,34)产生的三对波形之间的相位角改变 为了调整求和变压器(31,33,35)输出端的电压,求和变压器(31,33,35)输出端的电压和电流。

Patent Agency Ranking