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11. 发明申请

WO1989012371A1 METHOD AND APPARATUS FOR DETECTING INNOVATIONS IN A SCENE 审中-公开
标题翻译：用于检测场景创新的方法和装置
公开(公告)号：WO1989012371A1
公开(公告)日：1989-12-14
申请号：PCT/US1989002194
申请日：1989-05-19
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , KADAR, Ivan
IPC分类号： H04N07/18
CPC分类号： G08B13/19602 , G06E3/005 , G08B13/19634
摘要： System for detecting innovations in an image. A method includes gnerating plural parallel signals representing light incident on adjacent pixels (masks) which form an n by one vector, (Z), n being the number of mask pixels. L groups of adjacent pixels geometrically cover the image in parallel. The system replicates the generating step to generate plural (Z) vectors by taking multiple frames of observations of the image. These (Z) vectors are denoted (Zk), where k equals 1, 2, 3,..., m, m being the number of replicates. Each (Zk) vector relates to a vector ( beta k) having three parameters by the equation Zk = D beta k + ek, where (ek) is noise. A solution thereof yields estimates of the parameters beta k = D Zk, where D is a three by four matrix, beta k is a three by one vector and (Zk) is a four by one vector. beta k includes components (uk), (Ak) and ( beta k) whose values are monitored, and a signal is generated whenever one of these variables exceeds a threshold.
摘要翻译：用于检测图像创新的系统。一种方法包括使表示入射到形成n乘1的相邻像素（掩模）上的光的多个并行信号，（Z），n是掩模像素的数量。 L组相邻像素并行地几何地覆盖图像。系统通过拍摄图像的多个观察帧来复制生成步骤以生成多个（Z）向量。这些（Z）向量表示为（Zk），其中k等于1,2,3，...，m，m是重复的数量。每个（Zk）向量与具有三个参数的向量（βk）相关，其中（ek）是噪声。其解决方案产生参数βk = D Z k的估计，其中D T是三乘四矩阵，βk是三乘一矢量，（Zk）是四乘一矢量。 beta k包括其值被监视的组件（uk），（Ak）和（beta k），并且每当这些变量之一超过阈值时产生信号。

12. 发明申请

WO1988009289A1 STRUCTURAL MEMBERS CONNECTED BY INTERDIGITATING PORTIONS 审中-公开
标题翻译：结构部分由连接部分连接
公开(公告)号：WO1988009289A1
公开(公告)日：1988-12-01
申请号：PCT/US1988001528
申请日：1988-05-11
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , ANDERSON, Robert, E.
IPC分类号： B64C01/12
CPC分类号： B64C1/12
摘要： A wing skin (14) is usually mounted to a support structure (12) by using metal fasteners which cause high stress points and potential leakage points. The invention utilizes projections (16) formed in the wing skin to mate with recesses (13) formed in a support substructure thus forming interdigitations which prevent sliding displacement of the wing skin. A sliding bar (20) passes through the interdigitating sections to maintain an interlocking relation.

13. 发明申请

WO1988007764A1 DETECTOR BUFFER BOARD 审中-公开
标题翻译：检测器缓冲板
公开(公告)号：WO1988007764A1
公开(公告)日：1988-10-06
申请号：PCT/US1987003337
申请日：1987-12-11
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , SCHMITZ, Charles, E.
IPC分类号： H01L27/14
CPC分类号： H01L25/042 , H01L27/1446 , H01L2924/0002 , H01L2924/09701 , H01L2924/00
摘要： An infrared detection system is disclosed comprising a planar array segment of infrared detector elements (21), a multi-layer module (10) and a buffer board (15) disposed intermediate the detector array segment and the multi-layer module. The buffer board is disposed parallel to the planar array segment of detector elements and transverse to the plane of the module layers (11). The buffer board is disposed in abutting electrical connection with the detector elements and conductive patterns formed on the multi-layer module. The buffer board facilitates electrical communication between the detector elements and the module and conductive patterns formed on the module layers, and also enhances the structural characteristics and separate testability of the system components.
摘要翻译：公开了一种红外检测系统，其包括设置在检测器阵列段和多层模块之间的红外检测器元件（21），多层模块（10）和缓冲板（15）的平面阵列段。缓冲板平行于检测器元件的平面阵列段并且横向于模块层（11）的平面设置。缓冲板设置成与多层模块上形成的检测器元件和导电图案邻接电连接。缓冲板有助于检测器元件和模块之间的电气连通以及在模块层上形成的导电图案，并且还增强了系统部件的结构特性和分离的可测试性。

14. 发明申请

WO1988004097A1 FULLY PROGRAMMABLE LINEAR FEEDBACK SHIFT REGISTER 审中-公开
标题翻译：完全可编程的线性反馈移位寄存器
公开(公告)号：WO1988004097A1
公开(公告)日：1988-06-02
申请号：PCT/US1987003056
申请日：1987-11-23
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , GIANGANO, David, A. , JANKOWSKI, Cecelia , JOSEFSON, Eric
IPC分类号： G11C15/00
CPC分类号： G01R31/31813 , G06F7/584 , G11C19/00
摘要： Basic block shift registers (2) are cascaded to form a fully programmable linear feedback shift register. Each of the basic block shift registers comprises a plurality of flip-flops (FFA to FFD), each of which includes control logic circuits. A polynomial equation is first fed into the linear feedback shift register for setting the respective flip-flops into predetermined logic states, which are used to encode messages to be shifted by the programmable linear feedback shift register. The number of flip-flops in the programmable linear feedback shift register can be varied, in accordance to the polynomial equation. Likewise, the polynomial equation also determines the number of times the programmable linear feedback shift register is to circulate the encoded messages.

15. 发明申请

WO1988003112A1 SYNTHETIC SPEED STABILITY FLIGHT CONTROL SYSTEM 审中-公开
标题翻译：合成速度稳定性飞行控制系统
公开(公告)号：WO1988003112A1
公开(公告)日：1988-05-05
申请号：PCT/US1987002714
申请日：1987-10-22
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , BOUDREAU, Jean, A. , BERMAN, Howard, L. , CHIN, Jimmie , MARTORELLA, Romeo, P.
IPC分类号： B64C13/16
CPC分类号： B64C13/18 , G05D1/0623
摘要： A synthetic speed stability subsystem (12) for maintaining the speed and phugoid stability of an inherently unstable aircraft is connected to a main flight control system (6). The speed stability subsystem uses the pitch and roll angles, and the equivalent air speed of the aircraft for calculating a synthetic speed stability signal, which is fed to the main flight control system, for controlling the stability of the aircraft (2).

16. 发明申请

WO1988002146A1 APPARATUS AND METHOD OF STIMULATING AN EQUIPMENT 审中-公开
标题翻译：装置和刺激设备的方法
公开(公告)号：WO1988002146A1
公开(公告)日：1988-03-24
申请号：PCT/US1987002254
申请日：1987-09-08
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , NIELSEN, Robert, E.
IPC分类号： G06F11/00
CPC分类号： G01R31/31919
摘要： By using a combination memory (Z3), shift register (Z2), logic gates (Z4) and buffers (Z5), a stimulator (14) used in an automatic testing instrument (2) is able to provide two data rates for stimulating different equipment under test. The fast data rate is obtained by serially shifting parallel inputted data from the memory at a much faster rate than the operational speed of the memory. To accommodate equipment having a lower operating frequency, stimuli are transmitted to the equipment in a parallel mode.

17. 发明申请

WO1988001105A1 MODULAR ANTENNA ARRAY 审中-公开
标题翻译：模块天线阵列
公开(公告)号：WO1988001105A1
公开(公告)日：1988-02-11
申请号：PCT/US1987001782
申请日：1987-07-22
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , CANONICO, Lawrence, M.
IPC分类号： H01Q01/28
CPC分类号： H01Q21/08 , H01Q1/287 , H01Q21/0025
摘要： An antenna array includes a plurality of non-parasitic antenna drivers (22). A conductive member (14) serves as a ground plane and reflector. Each non-parasitic driver (22) is coupled to an energy transformer (18), by an energy conductor (20), which supports the element in spaced parallel relation with respect to the conductive member (14). The energy transformers (18) are releasably secured to the conductive member (14), formed of a plurality of portions, each portion having attached thereto a group of the energy transformers (18). The antenna array is formed by a series of modules (10) including a portion of the conductive member (14) with its attached energy transformers (18). The modules (10) form a wing leading edge radome that is hinged to the aircraft along a longitudinal edge of the radome (12) to permit easy access for servicing. The conductive member (14) in each module has a slot (24) for each driver (22) to permit replacement of antenna driver/energy transformer assemblies.

18. 发明申请

WO1988001056A1 METHOD AND APPARATUS FOR DETERMINING FLOW RESISTANCE OF FULLY ASSEMBLED ACOUSTIC LINERS 审中-公开
标题翻译：用于确定完全组装的声学衬里的流动阻力的方法和装置
公开(公告)号：WO1988001056A1
公开(公告)日：1988-02-11
申请号：PCT/US1987001788
申请日：1987-07-22
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , ARCAS, Noe , GOW, Joseph, P. , PARENTE, Charles, A.
IPC分类号： G01N29/04
CPC分类号： G01N29/11 , G01H15/00 , G01N29/223 , G01N2291/02863 , G01N2291/02872
摘要： An apparatus and method to determine the steady state flow resistance of assembled acoustic liners. Resistance is measured by applying a cylindrical waveguide (12) to the face of the liner (10). Two pressure transducers (17A) and (17B) mounted on the waveguide, measure pressure at two different points inside the waveguide, while the face of the liner is subject to a sinusoidal pressure field.
摘要翻译：确定组装的声学衬垫的稳态流阻的装置和方法。通过将圆柱形波导（12）施加到衬垫（10）的表面来测量电阻。安装在波导上的两个压力传感器（17A）和（17B）测量波导内部两个不同点处的压力，同时衬套的表面经受正弦压力场。

19. 发明申请

WO1996017697A1 ADJUSTABLE FORM DIE 审中-公开
标题翻译：可调式表格
公开(公告)号：WO1996017697A1
公开(公告)日：1996-06-13
申请号：PCT/US1995015423
申请日：1995-11-27
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , HAAS, Edwin, G. , KESSELMAN, Martin
IPC分类号： B21B37/24
CPC分类号： B30B15/02 , B21D37/02 , B21J13/02 , G05B2219/49025
摘要： This invention details a computer controlled self adjusting sheet metal forming die (10) which can provide rapid contour changes. It eliminates the need to manufacture, store, and change individual forming dies for forming different contours, and comprises a computer control device (100) which sends appropriately timed signals to translate each contour element so that a three dimension surface is formed by a discrete matrix of individual pins (15). This self adjusting sheet metal forming die is used on a sheet metal press wherein sheet metal can be formed by pressing or stretch forming the metal against the contoured surface.
摘要翻译：本发明详细描述了可以提供快速轮廓变化的计算机控制的自调整钣金成形模（10）。它不需要制造，存储和更换用于形成不同轮廓的各个成型模具，并且包括计算机控制装置（100），该计算机控制装置（100）发送适当的定时信号以平移每个轮廓元件，使得三维表面由离散矩阵形成（15）。这种自调整金属板成形模被用于金属板上，其中可以通过将金属压制或拉伸成形成轮廓表面而形成金属板。

20. 发明申请

WO1996002746A1 THRUST REVERSER 审中-公开
标题翻译：逆转器
公开(公告)号：WO1996002746A1
公开(公告)日：1996-02-01
申请号：PCT/US1995007697
申请日：1995-06-22
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , TINDELL, Runyon, H.
IPC分类号： F02K03/02
CPC分类号： F02K1/32 , F02K1/64 , F02K1/72 , F02K1/74 , Y02T50/671
摘要： A thrust reverser for an aircraft, having a podded nacelle (2) housing an engine (4), having a core (5), and a fan (6) producing normally aft-flowing exit streams (7), utilizes a stream director including an annular slot (8) through the outer wall (3) of the nacelle (2). The slot (8) has a convex forward surface (12) and a concave aft surface (13), a cascade of turning vanes (9) in the slot (8) for directing part of the core stream and most of the fan exit stream (7) forward through the slot (8). A jet injector (10a, 10b, and 10c) injects an annular jet of high pressure air into the fan exit stream (7) upstream of, and adjacent to the slot (8), thereby discharging the part of the core flow and most of the fan exit streams (7) forward through the slot (8), the turning vanes (9) and the outer wall (3) to provide a braking force for the aircraft.
摘要翻译：一种用于飞机的推力反向器，具有容纳具有芯部（5）的发动机（4）的吊舱（2）和产生正常流动的出口流（7）的风扇（6）），其利用包括通过机舱（2）的外壁（3）的环形槽（8）。槽（8）具有凸的前表面（12）和凹的后表面（13），在槽（8）中的级联的转向叶片（9），用于引导芯流的一部分和风扇的大部分出口流（7）向前穿过狭槽（8）。喷射喷射器（10a，10b和10c）将高压空气的环形射流喷射到风扇出口流（7）的上游并与槽（8）相邻并且邻近槽（8），从而排出芯流的一部分，并且大部分风扇出口流（7）向前穿过狭槽（8），转向叶片（9）和外壁（3），以为飞行器提供制动力。

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