PIEZOELECTRIC TRANSDUCER DRIVE
    142.
    发明申请
    PIEZOELECTRIC TRANSDUCER DRIVE 审中-公开
    压电传感器驱动

    公开(公告)号:WO1994015178A1

    公开(公告)日:1994-07-07

    申请号:PCT/US1993012054

    申请日:1993-12-10

    Applicant: HONEYWELL INC.

    CPC classification number: H01L41/042 G01C19/665

    Abstract: Piezoelectric transducer drive apparatus applies varying pulse rates to the terminals of the transducer with the transducer acting as a capacitor and integrating the applied pulses. A conductive path from each transducer terminal removes charge from each terminal. Control of the voltage across the transducer is achieved by individually varying the pulse rates applied to each of the transducer terminals.

    Abstract translation: 压电换能器驱动装置将变化的脉冲速率应用于换能器的端子,换能器用作电容器并积分所施加的脉冲。 来自每个换能器端子的导电路径从每个端子去除电荷。 通过单独改变施加到每个换能器端子的脉冲速率来实现对传感器两端的电压的控制。

    PIEZOELECTRIC TRANSDUCER DRIVE
    143.
    发明申请
    PIEZOELECTRIC TRANSDUCER DRIVE 审中-公开
    压电传感器驱动

    公开(公告)号:WO1994015176A1

    公开(公告)日:1994-07-07

    申请号:PCT/US1993011811

    申请日:1993-12-07

    Applicant: HONEYWELL INC.

    CPC classification number: G01C19/665 H01L41/042

    Abstract: A piezoelectric transducer drive apparatus continuously charges the terminals of the transducer through either resistors or constant current diodes. Digital words related to desired voltages at the transducer terminals are converted to first and second pulse rates. The first and second pulse rates separately discharge the terminals of the transducer through resistors or constant current diodes to achieve control of the drive voltage.

    Abstract translation: 压电换能器驱动装置通过电阻器或恒流二极管连续地对换能器的端子充电。 与换能器端子处的期望电压相关的数字字被转换为第一和第二脉冲速率。 第一和第二脉冲速率通过电阻器或恒流二极管分别放大换能器的端子,以实现对驱动电压的控制。

    PLL SYNTHESIZER GAIN CONTROL COMPENSATOR
    144.
    发明申请
    PLL SYNTHESIZER GAIN CONTROL COMPENSATOR 审中-公开
    PLL合成器增益控制补偿器

    公开(公告)号:WO1994014244A1

    公开(公告)日:1994-06-23

    申请号:PCT/US1993011810

    申请日:1993-12-07

    Applicant: HONEYWELL INC.

    CPC classification number: H03L7/183 H03L7/093 H03L7/107

    Abstract: An improved PLL synthesizer (10) including a gain control compensator (40) which compensates the PLL synthesizer output over the frequency range of operation of the PLL synthesizer. The gain control compensator includes a gain control amplifier (48) and programmable resistor (46) which function to eliminate the effects of changing N over the frequency range of operation. The gain control amplifier couples a loop filter (18) output signal to the VCO (20) and generates a factor equal to an inverse N to compensate the PLL synthesizer. The PLL synthesizer can compensate for gain non-linearity in the VCO transfer function.

    Abstract translation: 一种改进的PLL合成器(10),包括增益控制补偿器(40),其在PLL合成器的操作频率范围内补偿PLL合成器输出。 增益控制补偿器包括增益控制放大器(48)和可编程电阻器(46),其用于消除在工作频率范围内改变N的影响。 增益控制放大器将环路滤波器(18)输出信号耦合到VCO(20),并产生等于倒数N的因子以补偿PLL合成器。 PLL合成器可以补偿VCO传递函数中的增益非线性。

    CASE-MOUNTED RLG READOUT HAVING BLOCK MOUNTED OPTICAL SENSOR
    145.
    发明申请
    CASE-MOUNTED RLG READOUT HAVING BLOCK MOUNTED OPTICAL SENSOR 审中-公开
    具有块安装光学传感器的壳体安装RLG读数

    公开(公告)号:WO1994014032A1

    公开(公告)日:1994-06-23

    申请号:PCT/US1993011808

    申请日:1993-12-07

    Applicant: HONEYWELL INC.

    CPC classification number: G01C19/662

    Abstract: A readout device is provided for use in a ring laser angular rate sensor assembly which has improved low rate performance. Low rate performance is improved by reducing sources of backscatter thus not allowing light to be reflected back into the optical signal carrying medium. Backscatter is reduced by placing the optical sensors (62, 64) directly upon the gyro output mirror (14), thus causing the optical sensors to be dithered along with the laser block (10). By dithering the optical sensors, any backscatter caused by these elements is dealt with by dithering. While the optical sensors are dithered, the readout apparatus (44) continues to utilize the advantages of a case mounting.

    Abstract translation: 提供了一种用于环形激光角速率传感器组件的读出装置,其具有改进的低速性能。 通过减少反向散射光源来改善低速率性能,从而不允许光反射回光信号载体介质。 通过将光学传感器(62,64)直接放置在陀螺仪输出反射镜(14)上来减少反向散射,从而使光学传感器与激光块(10)一起抖动。 通过抖动光学传感器,由这些元件引起的任何反向散射都由抖动来处理。 当光学传感器被抖动时,读出装置(44)继续利用壳体安装的优点。

    FUNCTIONAL RADAR WARNING RECEIVER BACK-UP GENERATOR
    146.
    发明申请
    FUNCTIONAL RADAR WARNING RECEIVER BACK-UP GENERATOR 审中-公开
    功能雷达警告接收器后备发电机

    公开(公告)号:WO1994011752A1

    公开(公告)日:1994-05-26

    申请号:PCT/US1993011051

    申请日:1993-11-15

    Applicant: HONEYWELL INC.

    CPC classification number: G01S7/021 A61K31/485 G01N33/9486

    Abstract: A functional radar warning receiver back-up generator (225) provides threat information in the total absence or partial absence of the radar warning receiver information (42, 208). Radar warning receiver information (42, 208) such as radar detection data and radar identification data is also generated by other systems such as the Pulsed Radar Jammer (36) and the Continuous Wave Radar Jammer (34). An on-board computer processes and presents the back-up information to the pilot as if the Radar Warning Receiver (12) was still operational. Voice (226) and video (224) functions of the Radar Warning Receiver (12) are also displayed and presented to the pilot. Partial back-up (222) and full back-up (220) of the Radar Warning Receiver (12) are provided. A temporal data correlation algorithm (206), a radar emitter ID conversion algorithm (260), cross sensor correlation algorithm (248) and prioritization algorithm (244, 252) provide the back-up data.

    Abstract translation: 功能性雷达警报接收器备用发生器(225)在完全不存在或部分不存在雷达警报接收器信息(42,208)的情况下提供威胁信息。 诸如雷达检测数据和雷达识别数据的雷达警告接收机信息(42,208)也由诸如脉冲雷达干扰器(36)和连续波雷达干扰器(34)的其他系统产生。 车载计算机处理并向飞行员呈现备份信息,就好像雷达警报接收器(12)仍然可用。 雷达警报接收器(12)的声音(226)和视频(224)功能也被显示并呈现给飞行员。 提供雷达警报接收器(12)的部分备份(222)和完全备份(220)。 时间数据相关算法(206),雷达发射器ID转换算法(260),交叉传感器相关算法(248)和优先化算法(244,252)提供备份数据。

    COMPLEMENTARY THREAT SENSOR DATA FUSION METHOD AND APPARATUS
    147.
    发明申请
    COMPLEMENTARY THREAT SENSOR DATA FUSION METHOD AND APPARATUS 审中-公开
    补充威胁传感器数据融合方法和装置

    公开(公告)号:WO1994011750A1

    公开(公告)日:1994-05-26

    申请号:PCT/US1993011049

    申请日:1993-11-15

    Applicant: HONEYWELL INC.

    CPC classification number: G01S7/38 G01S7/021

    Abstract: A complementary threat sensor data fusion capability for an aircraft survivability equipment system (10). A set of aircraft survivability sensors (12, 32, 34, 36) provides a threat sensor data fusion control process (302) with status data (304). The control process controls (302) whether or not a threat ambiguity detector (308) receives radar warning receiver data (42) or a radar emitter ID conversion apparatus (310) receives pulsed radar jammer data (38) or continuous wave radar jammer data (46). The threat sensor data fusion control process (302) also determines whether missile approach detector data (48) is sent to a countermeasures analyzing apparatus (326). The threat ambiguity detector (308) provides ambiguity data (340) to a threat ambiguity resolving apparatus (324). The radar emitter ID conversion apparatus (310) provides converted jammer data (342) to a functional sensor back-up apparatus (201). The radar emitter ID conversion process (310) receives a common radar emitter (ID) data base (312). The threat sensor data fusion process controller (302) also provides fusion process control (338) to the complementary threat data apparatus (322). Complementary threat data (332) is provided to the pilot through various presentation methods and to the jammers (34, 36) for electronic countermeasures. Also, threat ambiguity resolution data (334) is provided and back-up data (228, 230) is provided. The presentation methods include video (224) and voice (226) and a tactical electronics countermeasures command (330) is automatically initiated. A multi-pass sensor data correlation algorithm (328) and a threat prioritization algorithm (252) share information with the threat ambiguity resolving algorithm (324), complementary threat data algorithm (322), functional sensor back-up apparatus (201), and electronic countermeasures apparatus (326). The direction of jamming is determined by data correlation between the radar warning receiver (12) and the CW Jammer (34).

    Abstract translation: 用于飞机生存能力设备系统的补充威胁传感器数据融合能力(10)。 一组飞机生存能力传感器(12,32,34,36)提供具有状态数据(304)的威胁传感器数据融合控制过程(302)。 控制过程控制(302)威胁模糊度检测器(308)是否接收雷达警报接收器数据(42)或雷达发射器ID转换装置(310)接收脉冲雷达干扰信号(38)或连续波雷达干扰信息 46)。 威胁传感器数据融合控制处理(302)还确定是否将导弹进近检测器数据(48)发送到对策分析装置(326)。 威胁模糊度检测器(308)向威胁模糊度分解装置(324)提供歧义数据(340)。 雷达发射器ID转换装置(310)向功能传感器备份装置(201)提供转换的干扰信息(342)。 雷达发射器ID转换处理(310)接收公共雷达发射器(ID)数据库(312)。 威胁传感器数据融合过程控制器(302)还向互补威胁数据设备(322)提供融合过程控制(338)。 通过各种呈现方法和用于电子对抗的干扰器(34,36)向飞行员提供互补威胁数据(332)。 此外,提供了威胁模糊度分辨率数据(334),并且提供备份数据(228,230)。 演示方法包括视频(224)和语音(226),并且自动启动战术电子对抗指令(330)。 多传感器数据相关算法(328)和威胁优先化算法(252)与威胁模糊度分解算法(324),互补威胁数据算法(322),功能传感器备份装置(201)和 电子对抗装置(326)。 干扰的方向由雷达警报接收器(12)和CW干扰器(34)之间的数据相关确定。

    TRIANGULAR DITHER DRIVE APPARATUS FOR A RING LASER GYROSCOPE
    148.
    发明申请
    TRIANGULAR DITHER DRIVE APPARATUS FOR A RING LASER GYROSCOPE 审中-公开
    三角激光陀螺仪三重驱动装置

    公开(公告)号:WO1994008206A1

    公开(公告)日:1994-04-14

    申请号:PCT/US1993009316

    申请日:1993-09-30

    Applicant: HONEYWELL INC.

    CPC classification number: G01C19/70

    Abstract: Control apparatus for an RLG dither motor (10) includes a digital phase shifter (40) for providing a clock signal related to the RLG position signal. A rate pulse generator (50) for receiving an amplitude word signal generated by a processor (28) at intervals determined by the clock signal provides a pulse rate signal related to the amplitude word signal. The pulse rate signal (51) is combined with the RLG position signal (33) to provide a second pulse rate signal which is integrated to provide a triangular dither drive signal.

    Abstract translation: 用于RLG抖动电动机(10)的控制装置包括用于提供与RLG位置信号相关的时钟信号的数字移相器(40)。 用于以由时钟信号确定的间隔接收由处理器(28)产生的振幅字信号的速率脉冲发生器(50)提供与振幅字信号相关的脉冲速率信号。 脉冲率信号(51)与RLG位置信号(33)组合以提供第二脉冲速率信号,其被积分以提供三角形抖动驱动信号。

    MICROMECHANICAL THERMOELECTRIC SENSOR ELEMENT
    149.
    发明申请
    MICROMECHANICAL THERMOELECTRIC SENSOR ELEMENT 审中-公开
    微电子传感器元件

    公开(公告)号:WO1993026053A1

    公开(公告)日:1993-12-23

    申请号:PCT/US1992004894

    申请日:1992-06-11

    Applicant: HONEYWELL INC.

    CPC classification number: G01J5/20 H01L27/16 H01L35/32

    Abstract: A thermoelectric sensor element that is adapted to respond to thermal radiation is capable of manufacture into a sensor array on a single crystal semiconductor means, such as silicon. An anisotropically etched pit is provided under the sensing surface, and the pit generally corresponds to the geometry of the sensor element. The geometry is selected to be rectangular and falls along a selected orientation of the particular crystalline structure used for manufacture of the device to thereby allow for a high density of the sensor elements. The sensor elements are manufactured of two dissimilar metals in a sinuous pattern to provide the thermoelectric effect.

    Abstract translation: 适于响应于热辐射的热电传感器元件能够制造成诸如硅的单晶半导体装置上的传感器阵列。 在感测表面下方提供各向异性蚀刻的凹坑,并且凹坑通常对应于传感器元件的几何形状。 几何形状被选择为矩形并且沿着用于制造器件的特定晶体结构的选定方向落下,从而允许高密度的传感器元件。 传感器元件由两种不同的金属制成,以提供热电效应。

    DISPLAY APPARATUS FOR A FIRST OUT TYPE OF FAULT STATUS ANNUNCIATOR HAVING A SERIES STRING OF INTERLOCK SWITCHES
    150.
    发明申请
    DISPLAY APPARATUS FOR A FIRST OUT TYPE OF FAULT STATUS ANNUNCIATOR HAVING A SERIES STRING OF INTERLOCK SWITCHES 审中-公开
    具有一系列串联开关的第一类故障状态警报器的显示装置

    公开(公告)号:WO1993024912A1

    公开(公告)日:1993-12-09

    申请号:PCT/US1993005275

    申请日:1993-06-02

    Applicant: HONEYWELL INC.

    CPC classification number: F23N5/242 F23N2031/20 F23N2037/08 G08B25/14

    Abstract: An annunciator for the status of interlock switches connected into a series circuit for supplying power from a power source to a load, includes a memory recording the status of each switch at a selectable instant. A plurality of display elements are arranged in a pattern corresponding to the pattern of the interlock switch circuit. A manually operable switch allows a user to select for graphically showing with the display either the switch status recorded by the memory or the current status of the switches. The signals controlling the display are conditioned so that the particular display element assigned to the first out switch as recorded in the memory flashes to indicate the switch closest to the power source which was not conducting at the selectable instant.

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