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    • 5. 发明申请
    • CIRCUIT INTEGRITY TESTER
    • 电路完整性测试仪
    • WO1980000614A1
    • 1980-04-03
    • PCT/US1979000640
    • 1979-08-30
    • SPERRY CORP
    • SPERRY CORPPERRY ROST R
    • G01N27/00
    • G01R31/024G01R31/2805
    • The test device is an electrolytic apparatus for the simultaneous non-destructive testing of the integrity of pluralities of circuit boards for continuity and anti-continuity or short circuits, including such circuit boards (23, 23a) as employ multi-layer or multi-level interconnection wiring, whether it be printed wiring or screen printed or thermally deposited circuits. Transient electro-deposition of one ion from an alkali halide water solution temporarily modifies the optical reflectivity of exposed circuit terminals (100) or metal parts of the circuit boards under test in a characteristic and easily recognized manner according to the continuity status of the associated circuit paths (104, 106).
    • 该测试装置是用于同时无损检测用于连续性和抗连续性或短路的多个电路板的完整性的电解设备,包括采用多层或多层次的电路板(23,23a) 互连布线,无论是印刷线路还是丝网印刷或热沉积电路。 根据相关电路的连续性状态,以特征容易识别的方式临时修改来自碱金属卤化物水溶液的一个离子的瞬时电沉积临时修改暴露的电路端子(100)或被测电路板的金属部件的光学反射率 路径(104,106)。
    • 6. 发明申请
    • SYMBOLOGY WRITING APPARATUS FOR RADAR PLAN POSITION INDICATOR DISPLAYS
    • 雷达计划位置显示器的符号写字装置
    • WO1980001612A1
    • 1980-08-07
    • PCT/US1979001147
    • 1979-12-28
    • SPERRY CORP
    • SPERRY CORPMAINE RGRYMES JBEAN D
    • G01S07/22
    • G01S7/22
    • Symbology is written on a radar plan position indicator display (202) with a rotating beam deflection field generated, for example, by a rotating yoke (201). The symbology is written in radar real time as the system generates the radially oriented range sweeps (10). The displayed radar range is quantized into a predetermined number of range increments and digital data representative of the symbology to be written are inserted into a shift register (33) which is clocked in synchronism with the range sweeps to provide interleaved digital data to the video input of the display thereby writing the desired symbology in real time as the range sweeps provide the normal radar display. The normal radar video data is combined (39) with the symbology data so that the symbology and normal radar returns are simultaneously written in real time. A portion of the symbology generating apparatus (Fig. 2) provides a manual acquisition marker comprising a range ring (12) and an azimuth geometric figure (13). The symbology writing apparatus also includes a portion (Fig. 4) for providing alpha-numeric or other localized symbology (Fig. 3).
    • 7. 发明申请
    • BIPHASE DETECTOR
    • 双相检测器
    • WO1982002985A1
    • 1982-09-02
    • PCT/US1982000151
    • 1982-02-04
    • SPERRY CORP
    • SPERRY CORPMAINE REUBEN E
    • H03D03/18
    • H04L25/4904H04L27/2272
    • L'etat binaire de chaque cycle d'un signal d'entree module biphase est detecte par une bascule 'D' (17) lorsqu'elle est synchronisee par un signal de reference genere localement. Lorsque l'etat binaire du signal d'entree possede une premiere valeur a la synchronisation, le signal de reference passe par une premiere porte OU exclusif (5) inchangee. Lorsque l'etat binaire du signal d'entree possede la valeur opposee, le signal de reference est inverse par la meme porte OU (5). La sortie de la premiere porte OU (5) et le signal d'entree sont appliques sur une seconde porte OU exclusif (1) pour produire un train d'impulsions ayant un cycle de travail indiquant l'erreur de phase entre le signal d'entree et le signal de reference. Ce train d'impulsions est filtre et utilise pour ajuster la phase de l'oscillateur de reference (13) jusqu'a ce que l'erreur de phase soit eliminee et le circuit en equilibre. L'etat binaire de la bascule (17) indique l'etat binaire du signal d'entree.
    • 8. 发明申请
    • LINE LENGTH NAVIGATION SYSTEM
    • 线长导航系统
    • WO1980001308A1
    • 1980-06-26
    • PCT/US1979000864
    • 1979-10-19
    • SPERRY CORP
    • SPERRY CORPDEMATTE JSIMONELLI N
    • G06F15/50
    • G01C21/203B63B35/03B63B2213/00B63H15/00B63H25/42G01C21/165
    • Guidance system used in laying undersea pipe or cable (3) from a pipe-laying vessel (1) when radio transmissions are unreliable. The system processes parameters derived from sensors (80, 88) normally aboard a pipe-laying vessel and sensors (83) cooperating with active winches (52) applying tension to the several anchor lines (12). The vessel's pitch, roll and heading angles are supplied from gyrocompass (88) and vertical gyroscopic instruments (80). Anchor line (12) elevation and azimuth angles with respect to deck coordinates are yielded by conventional angle pick offs (56, 60) associated with fairlead devices, as are the line axial tension and the length of anchor line paid out. Initial conditions, including the initial position of the vessel (1), are easily obtained in the usual manner (106). From certain of these parameters, the invention derives intermediate anchor line parameters for use in computing fairlead motion (93). The intermediate data is used to compute compensated fairlead motion data by first computing apparent fairlead motion from anchor line tension changes (110). This version of fairlead motion contains undesired terms due to apparent fairlead motion caused by anchor line length changes and also due to actual fairlead motion caused by vessel attitude changes. Therefore, second and third computations (112, 117) are made of the contributions of the latter effects. This is done so that apparent fairlead motion due to anchor line length change and actual fairlead motion due to vessel attitude change may be subtracted (114) from the measure of apparent fairlead motion as calculated from anchor line tension change, yielding the desired compensated fairlead motion value free of significant disturbing components (115). An estimated value of vessel position change is then obtained by a least squares estimation (130) involving these fairlead motion terms. Correction of vessel position (133) then follows by cooperative operation of the winch and thruster assemblies (52).
    • 当无线电传输不可靠时,用于从铺管船(1)铺设海底管道或电缆(3)的引导系统。 系统处理通常在放管容器上传感器(80,88)的参数,以及与主动绞车(52)配合的传感器(83),其向几根锚定线(12)施加张力。 船舶的俯仰,俯仰角和航向角由陀螺罗经(88)和垂直陀螺仪(80)提供。 相对于甲板坐标的锚定线(12)的高程和方位角通过与导线装置相关联的常规角度拾取(56,60)产生,线路轴向张力和锚线长度被支付。 初始条件,包括容器(1)的初始位置,以常规方式(106)容易获得。 根据这些参数中的某些,本发明导出中间锚线参数以用于计算平行线运动(93)。 中间数据用于通过首先从锚线张力变化计算明显的弹道运动来计算补偿的交错运动数据(110)。 由于由锚线长度变化引起的明显的导线运动,并且由于船只姿态变化引起的实际的弹道运动,这种版本的导弹运动包含不需要的术语。 因此,第二和第三计算(112,117)由后一种效应的贡献构成。 这样做,使得由于锚线长度变化引起的明显的导线运动以及由于船舶姿态变化引起的实际的弹道运动可以从锚线张力变化计算出的明显的弹道运动的测量中减去(114),从而产生所需的补偿的弹道运动 没有显着干扰组件(115)。 然后通过涉及这些Fairlead运动项的最小二乘估计(130)获得船舶位置变化的估计值。 然后通过绞盘和推进器组件(52)的协同操作来跟随船舶位置(133)的修正。