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1. 发明申请

WO1995027576A1 FORMING GROOVES IN A TUBULAR MEMBER 审中-公开
标题翻译：在管状构件中形成沟槽
公开(公告)号：WO1995027576A1
公开(公告)日：1995-10-19
申请号：PCT/US1995004386
申请日：1995-04-10
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , ARENA, Aldo , BENOIT, Robert, L.
IPC分类号： B21D26/14
CPC分类号： B21J5/12 , B21C37/202 , B21D15/02 , B21D26/14
摘要： In a method of forming grooves in a tubular member having an inner surface and an outer surface, an end of the tubular member (1) is inserted into a forming die (4) having a bore (5) of cylindrical configuration with a selected pattern of grooves (6, 7, 8) formed in the bore. A deformation force is applied to the inner surface of the tubular member which impresses the pattern of grooves of the die on the outer surface of the tubular member in the die, and thereby causes the outer surface to acquire the shape of the pattern of grooves in the forming die.
摘要翻译：在具有内表面和外表面的管状构件中形成槽的方法中，管状构件（1）的端部插入具有圆柱形构造的孔（5）的成形模具（4）中，所述孔（5）具有选定的图案形成在孔中的槽（6,7,8）。对管状构件的内表面施加变形力，使模具的管状构件的外表面上的凹槽的图案印刷在模具中，从而使外表面获得凹槽图案的形状成型模具。

2. 发明申请

WO1995021387A1 SIGNAL PROCESSING FOR ULTRA-WIDEBAND IMPULSE RADAR 审中-公开
标题翻译：超宽带脉冲雷达信号处理
公开(公告)号：WO1995021387A1
公开(公告)日：1995-08-10
申请号：PCT/US1994014556
申请日：1994-12-29
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , BOLES, Sol , BUCKLAND, Dennis, J.
IPC分类号： G01S07/28
CPC分类号： G01S7/2926 , G01S13/0209 , G01S13/538
摘要： An ultra-wideband impulse radar system for use on an airborne platform includes circuitry (16) for coherently integrating the signals to improve signal-to-noise ratio so as to enhance the detection capability of the system, and for motion compensation of the signals to correct for inadvertent modulations of received signals due to buffeting or vibration of the airborne platform which may otherwise corrupt the filtering and signal integration processes. The inclusion of velocity filters and coherent integration despite the lack of phase information in the signals is accomplished by exploiting the time-delay properties of the received impulse signals, in which the observable pulse repetition frequency of the received signals differs from the transmitted pulse repetition frequency by virtue of the relative velocity between signal reflecting elements and the radar platform.
摘要翻译：在空中平台上使用的超宽带脉冲雷达系统包括用于相干地整合信号以提高信噪比的电路（16），以便增强系统的检测能力，并且用于将信号的运动补偿纠正由于空中平台的抖动或振动导致的接收信号的无意调制，否则可能会破坏滤波和信号集成过程。尽管信号中缺乏相位信息，但是包含速度滤波器和相干积分是通过利用接收到的脉冲信号的时间延迟特性来完成的，其中接收信号的可观察脉冲重复频率与所发射的脉冲重复频率不同凭借信号反射元件与雷达平台之间的相对速度。

3. 发明申请

WO1995014277A1 STABILIZED ADAPTIVE NEURAL NETWORK BASED CONTROL SYSTEM 审中-公开
标题翻译：稳定自适应神经网络控制系统
公开(公告)号：WO1995014277A1
公开(公告)日：1995-05-26
申请号：PCT/US1994011834
申请日：1994-10-20
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , HUANG, Chien, Y. , EIBERT, James, L. , ENGEL, Stephen, J.
IPC分类号： G06F15/18
CPC分类号： G05B13/027
摘要： A neural network (6) based control system includes a nominal control system (3) augmented by adaptive control such as a neuro-controller (1000) which generates additional compensating control signals based on differences between a model (8) and actual system output. The nominal control system (3) provides basic stability and performance, while the adaptive controller (1000) provides performance enhancement. The adaptive control can rely on any neural network (6) that can encode a-priori knowledge and employs a high resolution pattern discrimination capability suitable for real-time changes. To prevent unbounded adaptation, the output of the adaptive controller (1000) is constrained by a limiter (9), thus ensuring safety of the overall system.
摘要翻译：基于神经网络（6）的控制系统包括通过诸如神经控制器（1000）的自适应控制增强的标称控制系统（3），其基于模型（8）和实际系统输出之间的差异生成额外的补偿控制信号。标称控制系统（3）提供基本的稳定性和性能，而自适应控制器（1000）提供性能提升。自适应控制可以依赖于可以对先验知识进行编码的任何神经网络（6），并且采用适合于实时变化的高分辨率模式识别能力。为了防止无限制的适应，自适应控制器（1000）的输出受限制器（9）的限制，从而确保整个系统的安全。

4. 发明申请

WO1994025357A1 REUSABLE VACUUM BAG AND METHOD OF MANUFACTURING SAME 审中-公开
标题翻译：可重复使用的真空袋及其制造方法
公开(公告)号：WO1994025357A1
公开(公告)日：1994-11-10
申请号：PCT/US1994004979
申请日：1994-04-28
申请人： GRUMMAN AEROSPACE CORPORATION , CORNEAU, Louis, P., Jr.
发明人： GRUMMAN AEROSPACE CORPORATION
IPC分类号： B65D30/02
CPC分类号： B65D31/00 , B29C43/3642 , B29C65/4815 , B29C65/5057 , B29C66/02 , B29C66/1122 , B29C66/431 , B29C66/71 , B29C66/723 , B29K2027/12 , B29K2083/00 , B31B70/60 , Y02W30/807 , Y10S493/924
摘要： A reusable silicone vacuum bag (1) is manufactured by making a silicone vacuum bag envelope (1) having peripheral edges (2, 3, 4, 5). The bag envelope is spread so that the peripheral edges frame the envelope. Fluorinated ethylene propylene (FEP) is bonded to an area (6, 7, 8, 9) bordering the peripheral edges. The bag envelope is folded over on itself at the peripheral edges. Edge sealing tape (11) is applied to the FEP (10) in the area bordering the peripheral edges so that it covers the peripheral edges.
摘要翻译：通过制造具有外围边缘（2,3,4,5）的硅树脂真空袋封套（1）制造可重复使用的硅胶真空袋（1）。包袋被展开，使得外围边缘围绕信封。氟化乙烯丙烯（FEP）结合到与周边边界接近的区域（6,7,8,9）。袋子外壳边缘折叠在自身上。将边缘密封带（11）施加到与外围边缘接合的区域中的FEP（10），使其覆盖周边边缘。

5. 发明申请

WO1994022714A1 OCCUPANT ARM AND HEAD RESTRAINING ASSEMBLY 审中-公开
标题翻译：职业ARM和头部限制组件
公开(公告)号：WO1994022714A1
公开(公告)日：1994-10-13
申请号：PCT/US1994003443
申请日：1994-04-05
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , ARONNE, Armand, J.
IPC分类号： B64D25/115
CPC分类号： B64D25/02
摘要： An assembly (5) for restraining the upper limbs of an occupant of a seat, particularly an aircraft ejector seat (1), includes a storage unit (65) which is adapted to be fixedly secured to an upper back portion (16) of the seat (1). The storage unit (65) houses a pair of movable cover members (69, 70) and first and second bladder units (75, 76). The cover members (69, 70) and bladder units (75, 76) are connected by means of straps (90, 91) to quick release fittings (94, 95) which mate with corresponding connecting members (111, 112) carried by the occupant and then to a fixed structure adjacent the seat (1). When it is desired to deploy the restraint assembly (5), a tension is applied to the straps (90, 91) which causes the cover members (69, 70) to extend around opposite sides and laterally inward of the occupant's body, about respective arms of the occupant, and the bladder units (75, 76) to extend about the occupant's neck. The bladder units (75, 76) are then inflated so as to permit undesirable movement of the occupant's head.
摘要翻译：一种用于限制座椅乘员特别是飞行器弹射座（1）的上肢的组件（5）包括一个储存单元（65），该储存单元适于固定地固定在所述座椅的上部后部座位（1）。存储单元（65）容纳一对可移动盖构件（69,70）和第一和第二囊单元（75,76）。盖构件（69,70）和气囊单元（75,76）通过带（90,91）连接到快速释放配件（94,95），其与由相应的连接构件（111,112）携带的相应的连接构件乘客然后到靠近座椅（1）的固定结构。当期望展开约束组件（5）时，张力被施加到带（90,91）上，使得盖构件（69,70）围绕相应的侧面在乘员身体的相对侧和横向内侧延伸乘员的手臂和膀胱单元（75,76）围绕乘员的颈部延伸。然后将膀胱单元（75,76）充气以允许乘客头部的不期望的运动。

6. 发明申请

WO1994018718A1 PORTABLE ANTENNA TEST APPARATUS 审中-公开
标题翻译：便携式天线测试仪
公开(公告)号：WO1994018718A1
公开(公告)日：1994-08-18
申请号：PCT/US1994001386
申请日：1994-02-04
申请人： GRUMMAN AEROSPACE CORPORATION , TEICH, Stanley , ROLL-MECAK, Doru , KOMMEL, Morton
发明人： GRUMMAN AEROSPACE CORPORATION
IPC分类号： H01Q01/38
CPC分类号： H01Q3/267 , G01R29/10
摘要： Portable antenna test apparatus has a test set positioned a determined distance from a number of antennas (3) of an aircraft. A transmitting module (6) of the test set contains low frequency, mid frequency and high frequency antennas connected to a radio receiver (15) and power amplifier (14) in and of the test set for receiving control commands and for transmitting a number of simultaneous test signals to the number of antenna (3) in the aircraft. A signal generator (7) produce low frequency, mid frequency and high frequency signals. A hand-held computer (5) is connected to a communications radio (2) in and of the aircraft via a radio interface adapter (4) of the hand-held and a control computer (10) is connected to the signal generator. The hand-held computer transmits commands via the aircraft radio, which commands are received by the receiver in the transmitting module. This receiver conveys the said commands to a control computer which then programs the signal generator. By this means, an operator in the aircraft cockpit remotely controls the signal generator.
摘要翻译：便携式天线测试装置具有距离飞机的多个天线（3）确定距离的测试装置。测试装置的发射模块（6）包含连接到用于接收控制命令的测试装置中的无线电接收器（15）和功率放大器（14）的低频，中频和高频天线，并用于发送多个同时测试信号到飞机上天线（3）的数量。信号发生器（7）产生低频，中频和高频信号。手持式计算机（5）经由手持设备的无线电接口适配器（4）连接到飞行器内的通信无线电（2），并且控制计算机（10）连接到信号发生器。手持式计算机通过飞行器无线电发送命令，这些命令由接收机在发射模块中接收。该接收器将所述命令传送给然后对信号发生器进行编程的控制计算机。通过这种方式，飞机驾驶舱中的操作员远程控制信号发生器。

7. 发明申请

WO1994012836A1 SELF-CONTAINED COOLER/FREEZER APPARATUS 审中-公开
标题翻译：自含冷却器/冷冻装置
公开(公告)号：WO1994012836A1
公开(公告)日：1994-06-09
申请号：PCT/US1993011142
申请日：1993-11-16
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , BARTILUCCI, Anthony
IPC分类号： F25D03/12
CPC分类号： F25D3/125 , F25D29/001
摘要： A self-contained cooler/freezer apparatus for carrying items (46) in a frozen or refrigerated environment. The apparatus comprises an insulated container (10) which is divided into two portions. The first portion (42) is where the items are stored. The second portion (38) houses a coolant compartment for storing a solid coolant, namely, solid carbon dioxide or dry ice (54). Within a short period of time, the dry ice starts to sublimate, thereby forming cold gaseous carbon dioxide which fills the volume of the apparatus. A fan (52) is used to circulate the gaseous carbon dioxide throughout the insulated container thereby removing heat from the first portion and rejecting it to the dry ice in the coolant compartment, thereby cooling the first portion of the insulated container. The cold gaseous carbon dioxide is circulated throughout the insulated container via gas ducts located within the walls of the insulated container. A thermostatic controller (56) actuates the fan based upon temperature readings from thermocouples located within the first portion of the insulated container. A pressure relief valve (34) is positioned within the insulated container to prevent the pressure within the insulated container from building beyond a maximum value.
摘要翻译：一种用于在冷冻或冷藏环境中携带物品（46）的独立冷却器/冷冻装置。该装置包括分成两部分的隔热容器（10）。第一部分（42）是存储物品的地方。第二部分（38）容纳用于存储固体冷却剂的冷却剂室，即固体二氧化碳或干冰（54）。在短时间内，干冰开始升华，从而形成充满装置体积的冷气态二氧化碳。风扇（52）用于使气态二氧化碳在整个绝热容器中循环，从而从第一部分除去热量并将其排入冷却剂室内的干冰，从而冷却绝热容器的第一部分。冷的气态二氧化碳通过位于隔热容器的壁内的气体管道在整个绝热容器中循环。恒温控制器（56）基于位于绝热容器的第一部分内的热电偶的温度读数来致动风扇。压力释放阀（34）定位在绝热容器内，以防止绝热容器内的压力超过最大值。

8. 发明申请

WO1991005989A1 DETECTOR ELEMENT SIGNAL COMPARATOR SYSTEM 审中-公开
标题翻译：检测元件信号比较器系统
公开(公告)号：WO1991005989A1
公开(公告)日：1991-05-02
申请号：PCT/US1990005935
申请日：1990-10-16
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , SOLOMON, Allen, L.
IPC分类号： G01J05/14
CPC分类号： G08B13/194 , H04N5/33 , H04N5/3651
摘要： A detector element signal comparator system is used for noise reduction and image enhancement by comparing the output of any detector signal processor within a module to the output of any other detector signal processor within the same module. The detector element signal comparator system has a comparator (51-59) for each detector signal processor (41-49), a comparator bus (71) to connect the output of any detector processor to the comparators of all other detector signal processors, a switch (61-69) for each detector signal processor to selectively connect each detector signal processor to the comparator bus, and an output bus (73) for communicating the comparator signal from the detector element signal comparator to the next stage of signal processing.

9. 发明申请

WO1991001034A1 AN ACOUSTIC LINER 审中-公开
标题翻译：一个声音衬里
公开(公告)号：WO1991001034A1
公开(公告)日：1991-01-24
申请号：PCT/US1990003538
申请日：1990-06-21
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , ARCAS, Noe , PARENTE, Charles, A.
IPC分类号： G10K0

10. 发明申请

WO1990011619A1 SINGLE TRENCH MOSFET-CAPACITOR CELL FOR ANALOG SIGNAL PROCESSING 审中-公开
标题翻译：用于模拟信号处理的单个TRENCH MOSFET电容器单元
公开(公告)号：WO1990011619A1
公开(公告)日：1990-10-04
申请号：PCT/US1990000240
申请日：1990-01-09
申请人： GRUMMAN AEROSPACE CORPORATION
发明人： GRUMMAN AEROSPACE CORPORATION , SOLOMON, Allen, L.
IPC分类号： H01L27/108
CPC分类号： H01L29/7827 , H01L27/0629 , H01L27/092 , H01L29/4236
摘要： A process for forming a single trench MOS transistor/capacitor cell for analog signal processing, and the resulting structure, are disclosed. The transistor is formed by forming a first trench (31) in the semiconductor substrate, lining the trench with a layer of insulating material (33), a layer of conducting material (35), and filling the trench with a layer of insulator (41). A doped region is formed adjacent the trench, which serves as a transistor source (21). A second trench (32) is then formed which extends through and excavates a portion of the first trench. The second trench is lined with a layer of doped material (43) and insulator (45). The doped material (43) is isolated from the conductive layer (35) lining the first trench (31). The second trench (32) is then filled with a body of conductive material (47). The layer of doped material (43) lining the second trench serves as the transistor drain and a capacitor output is extracted from the body of conductive material (47).
摘要翻译：公开了用于形成用于模拟信号处理的单沟槽MOS晶体管/电容器单元的工艺，以及所得到的结构。通过在半导体衬底中形成第一沟槽（31）形成晶体管，用绝缘材料层（33），导电材料层（35）衬套沟槽，并用绝缘体层（41）填充沟槽）。形成与沟槽相邻的掺杂区，其用作晶体管源（21）。然后形成延伸穿过并挖掘第一沟槽的一部分的第二沟槽（32）。第二沟槽衬有一层掺杂材料（43）和绝缘体（45）。掺杂材料（43）与衬在第一沟槽（31）上的导电层（35）隔离。然后用导电材料体（47）填充第二沟槽（32）。衬在第二沟槽上的掺杂材料层（43）用作晶体管漏极，电容器输出从导电材料体（47）提取。

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