CENTER POST ELECTROCHEMICAL CELL STACK
    92.
    发明申请
    CENTER POST ELECTROCHEMICAL CELL STACK 审中-公开
    中心后电化学电池堆

    公开(公告)号:WO1998004762A1

    公开(公告)日:1998-02-05

    申请号:PCT/US1997013224

    申请日:1997-07-29

    CPC classification number: H01M8/247 C25B9/18

    Abstract: A center post electrochemical cell stack is disclosed for generating a product gas such as oxygen gas from a supply fluid such as water. The invention could be used to generate oxygen on board a space or aircraft and includes: a frame having a base plate (14) and a wall (16) affixed to the base plate so that the wall and base plate define a cell chamber (18) for housing at least one electrochemical cell; and a T-cap having a top plate (24) and a centeer post (26) affixed to and projecting away from the top plate, wherein the top plate is secured to the wall of the frame to close the cell chamber and the center post passes through a central throughbore in an electrochemical cell within the chamber and is adjustably secured to the base plate of the frame. Consequently, the T-cap and frame cooperate to contain pressure generated by operation of the electrochemical cell. In a specific embodiment of the center post electrochemical cell stack, an exterior surface of the center post of the T-cap cooperates with a central throughbore vented electrochemical cell to define a high pressure manifold (34) for venting of the product gas out of the cell, and an interior surface (36) of the wall of the frame cooperates with the vented central throughbore cell to define a low pressure manifold (40) for transmission of the supply fluid into and out of the cell.

    Abstract translation: 公开了一种中心后电化学电池堆,用于从诸如水的供应流体产生诸如氧气的产物气体。 本发明可以用于在空间或飞行器上产生氧气,并且包括:框架,其具有固定到基板的基板(14)和壁(16),使得壁和基板限定电池室(18 )用于容纳至少一个电化学电池; 以及T形盖,其具有固定到顶板并远离顶板的顶板(24)和中心柱(26),其中顶板固定到框架的壁以封闭电池室和中心柱 通过腔室内的电化学电池中的中心通孔,并且可调节地固定到框架的基板上。 因此,T形帽和框架配合以容纳由电化学电池的操作产生的压力。 在中心后电化学电池堆的具体实施例中,T形帽的中心柱的外表面与中心通孔排出的电化学电池配合以限定高压歧管(34),用于将产物气体排出 电池,并且框架的壁的内表面(36)与通气的中心透孔单元协作以限定用于将供应流体传输到电池中的低压歧管(40)。

    HIGH RELIABILITY LOGIC CIRCUIT FOR A RADIATION ENVIRONMENT
    93.
    发明申请
    HIGH RELIABILITY LOGIC CIRCUIT FOR A RADIATION ENVIRONMENT 审中-公开
    用于辐射环境的高可靠性逻辑电路

    公开(公告)号:WO1997040497A1

    公开(公告)日:1997-10-30

    申请号:PCT/US1997006643

    申请日:1997-04-18

    CPC classification number: H03K3/0375 G11C5/005

    Abstract: According to the present invention, a dual memory cell, includes a first memory cell receiving a first logic state input signal and providing an output signal, and further includes a second memory cell receiving a second logic state input signal and providing an output signal, where the first and second memory cell and second memory cell further receive and respond to one or more logic signals from the other. The output signal of the first memory cells and the output signal of the second memory cell may be further combined to provide one resultant logic state output signal which has improved reliability in a radiation environment.

    Abstract translation: 根据本发明,双存储单元包括接收第一逻辑状态输入信号并提供输出信号的第一存储单元,并且还包括接收第二逻辑状态输入信号并提供输出信号的第二存储单元,其中 第一和第二存储单元和第二存储单元进一步接收并响应来自另一个的一个或多个逻辑信号。 可以进一步组合第一存储单元的输出信号和第二存储单元的输出信号以提供在辐射环境中具有改进的可靠性的一个合成逻辑状态输出信号。

    METHOD AND APPARATUS FOR APPLYING MULTI-LAYERED COATINGS BY DETONATION
    94.
    发明申请
    METHOD AND APPARATUS FOR APPLYING MULTI-LAYERED COATINGS BY DETONATION 审中-公开
    通过爆炸法应用多层涂料的方法和装置

    公开(公告)号:WO1997023302A1

    公开(公告)日:1997-07-03

    申请号:PCT/US1996020154

    申请日:1996-12-23

    CPC classification number: B05B7/0006

    Abstract: A method and apparatus for applying multi-layered coatings utilizing a detonation gun process. The present invention consists of multiple powder feeders (7, 8) attached to the barrel (13) of a detonation gun (2). The powder feeders (7, 8) are disposed at axially spaced locations along the barrel (13) and supply coating materials to the barrel (13) in advance of a detonation wave front (100) such that the powders are exhausted from the barrel (13) in serial fashion producing a multi-layered coating on the workpiece (1). The multi-layered coating system of the present invention substantially enhances the quality and productivity of the detonation coating process.

    Abstract translation: 一种使用爆震枪工艺应用多层涂层的方法和装置。 本发明由附接到爆震枪(2)的枪管(13)的多个粉末馈送器(7,8)组成。 粉末进料器(7,8)沿着筒体(13)设置在轴向间隔开的位置处,并且在引爆波前(100)之前将涂覆材料供应到筒体(13),使得粉末从筒体(... 13),在工件(1)上产生多层涂层。 本发明的多层涂布体系大大提高了引爆涂层工艺的质量和生产率。

    ENHANCED PERFORMANCE BLASTING AGENT
    95.
    发明申请
    ENHANCED PERFORMANCE BLASTING AGENT 审中-公开
    增强性能喷砂剂

    公开(公告)号:WO1997006122A1

    公开(公告)日:1997-02-20

    申请号:PCT/US1996012848

    申请日:1996-08-02

    CPC classification number: C06B45/08 C06B31/285 C06B33/14

    Abstract: An improved blasting composition comprising from about 13 to 15 weight percent unrefined petroleum wax, from about 15 to 20 weight percent aluminum powder, from about 10 to 52 weight percent sodium perchlorate and from about 10 to 52 weight percent ammonium nitrate. The blasting composition may be used in combination with ANFO and in place of conventional solid AP propellants and represents an economical alternative thereto.

    Abstract translation: 一种改进的喷砂组合物,其包含约13至15重量%的未精制石油蜡,约15至20重量%的铝粉,约10至52重量%的高氯酸钠和约10至52重量%的硝酸铵。 喷砂组合物可以与ANFO组合使用,代替常规固体AP推进剂,代表其经济性。

    COMPRESSOR STALL AND SURGE CONTROL USING AIRFLOW ASYMMETRY MEASUREMENT
    96.
    发明申请
    COMPRESSOR STALL AND SURGE CONTROL USING AIRFLOW ASYMMETRY MEASUREMENT 审中-公开
    使用气流不对称测量的压缩机驻车和风机控制

    公开(公告)号:WO1997000381A1

    公开(公告)日:1997-01-03

    申请号:PCT/US1995017145

    申请日:1995-11-02

    CPC classification number: F04D27/001 F04D27/02

    Abstract: A technique for controlling compressor stall and surge is disclosed. In a gas turbine engine, static pressure asymmetry is sensed at a plurality of locations along the circumference of the compressor inlet. Time rate of change of the mass flow in the compressor is also estimated using pressure measurements in the compressor. A signal processor uses these signals to modulate a compressor bleed valve responsive to the level of flow property asymmetry, the time rate of change of the annulus average flow to enhance operability of the compressor.

    Abstract translation: 公开了一种用于控制压缩机失速和喘振的技术。 在燃气涡轮发动机中,沿着压缩机入口的圆周的多个位置处感测静压不对称性。 也可以使用压缩机中的压力测量来估计压缩机中的质量流量的时间变化率。 信号处理器使用这些信号来调节压缩机泄放阀,以响应于流动性不对称性的水平,环形平均流量的时间变化率以增强压缩机的可操作性。

    A HYBRID COMPOSITE FLEXBEAM FOR A HELICOPTER BEARINGLESS MAIN ROTOR ASSEMBLY
    97.
    发明申请
    A HYBRID COMPOSITE FLEXBEAM FOR A HELICOPTER BEARINGLESS MAIN ROTOR ASSEMBLY 审中-公开
    用于直升机无轴承主转子总成的混合复合软管

    公开(公告)号:WO1996039327A1

    公开(公告)日:1996-12-12

    申请号:PCT/US1995007371

    申请日:1995-06-09

    CPC classification number: B64C27/33 B29C70/202

    Abstract: A hybrid composite flexbeam (10) for a soft inplane bearingless main rotor assembly (100) has eight spanwise regions: a hub attachment region (12); a first tapered region (14); a second tapered region (16); an inboard transition region (18); a pitch region having a cruciform configuration (20); an outboard transition region (22); a tapered outboard transition region (24); and a main rotor blade, torque tube attachment region (26). The pitch region (20) is formed from unidirectional fiberglass plies, a 50/50 admixture of unidirectional fiberglass and graphite plies, and unidirectional graphite plies. Unidirectional fiberglass and graphite plies of varying lengths are interleaved in the second inboard tapered region (16). Fiberglass and graphite cross plies of varying lengths are interleaved in the first inboard tapered region (14). Fiberglass and graphite cross plies and unidirectional fiberglass plies of varying length are interleaved in the outboard tapered region (24). The distributed arrangement of ply endings cause kick loads (97) in the hybrid flexbeam (10) to be distributed across the ply buildups.

    Abstract translation: 用于软内平面无轴承主转子组件(100)的混合复合柔性梁(10)具有八个翼展区域:轮毂附接区域(12); 第一锥形区域(14); 第二锥形区域(16); 内部过渡区域(18); 具有十字形构造的节距区域(20); 外侧过渡区域(22); 锥形外侧过渡区域(24); 和主转子叶片,扭矩管附接区域(26)。 节距区域(20)由单向玻璃纤维层,单向玻璃纤维和石墨层的50/50混合物和单向石墨层形成。 不同长度的单向玻璃纤维和石墨层在第二内侧锥形区域(16)中交错。 不同长度的玻璃纤维和石墨交叉层在第一内侧锥形区域(14)中交错。 不同长度的玻璃纤维和石墨交叉层和单向玻璃纤维帘布层在外侧锥形区域(24)中交错。 层结构的分布布置导致混合柔性梁(10)中的脚蹬负载(97)分布在层叠层上。

    HYDRODYNAMIC AIR THRUST BEARING WITH OFFSET BUMP FOILS
    98.
    发明申请
    HYDRODYNAMIC AIR THRUST BEARING WITH OFFSET BUMP FOILS 审中-公开
    水动力空气轴承带偏心垫圈

    公开(公告)号:WO1996033350A1

    公开(公告)日:1996-10-24

    申请号:PCT/US1996003079

    申请日:1996-03-05

    CPC classification number: F16C17/042 F16C2300/02

    Abstract: The leading edges (40, 50) of the segmented corrugated springs of each of the two bump foils (16, 24) of a hydrodynamic thrust bearing (10) are offset such that the leading edge (40) in the upper segmented corrugated springs (16) are circumferentially spaced relative to the leading edge (50) of the lower segmented corrugated springs (24) that is underlying each respective segment of the bump foils. In some embodiments, the leading edge of the bump foil is attached and the trailing edge is free to move axially and in other embodiments, the reverse occurs where the trailing edge of the bump foil is attached and the leading edge is free to move axially.

    Abstract translation: 流体动力推力轴承(10)的两个凸块(16,24)中的每一个的分段波纹弹簧的前缘(40,50)被偏移,使得上部分段波纹弹簧中的前缘(40) 16)相对于下部分段的波纹弹簧(24)的前缘(50)周向间隔开,其位于凸块箔的每个相应部分的下方。 在一些实施例中,凸块箔的前缘被附接并且后缘自由地轴向移动,并且在其他实施例中,相反的情况发生在凸块箔的后缘被附接并且前缘自由地轴向移动的情况。

    METHOD AND APPARATUS FOR DETECTING BLOWOUT IN A GAS TURBINE COMBUSTOR
    99.
    发明申请
    METHOD AND APPARATUS FOR DETECTING BLOWOUT IN A GAS TURBINE COMBUSTOR 审中-公开
    用于检测气体涡轮机中的气泡的方法和装置

    公开(公告)号:WO1996028644A1

    公开(公告)日:1996-09-19

    申请号:PCT/US1996003534

    申请日:1996-03-14

    Abstract: Method for detecting burner blowout comprises the following steps: periodically measuring the actual pressure of ignition at successive intervals of time; periodically measuring the actual rotational speed of the generator shaft at the successive intervals of time; calculating the rate of change in the actual pressure over a successive interval of time; calculating the rate of change in the actual rotational speed over the successive interval of time; comparing the rate of change in the actual pressure of ignition over the successive interval of time to a reference pressure rate of change value; comparing the rate of change in the actual rotational speed over the successive interval of time to the reference speed rate of change value; and closing the fuel valve in response to the reference pressure rate of change value being greater than the rate of change of the actual pressure of ignition over the successive interval of time, in the presence of the rate of change of actual rotational speed over the successive interval of time being less than the reference speed rate of change value, thus stopping the fuel flow to the burner.

    Abstract translation: 检测燃烧器井喷的方法包括以下步骤:在连续的时间间隔周期性地测量点火的实际压力; 在连续的时间间隔周期性地测量发电机轴的实际转速; 计算连续时间间隔内实际压力的变化率; 计算连续时间间隔内实际转速的变化率; 将连续时间间隔内的实际点火压力的变化率与参考压力变化率值进行比较; 将连续时间间隔内的实际转速的变化率与参考速度变化率值进行比较; 以及响应于所述参考压力变化率值大于所述连续时间间隔内的实际转速的变化率,所述参考压力变化率值在所述连续时间间隔内的实际转速的变化率 时间间隔小于参考速度变化率值,从而停止燃油流向燃烧器。

    SEGMENTED BULKHEAD LINER
    100.
    发明申请

    公开(公告)号:WO1996018851A1

    公开(公告)日:1996-06-20

    申请号:PCT/US1995015095

    申请日:1995-11-17

    CPC classification number: F23R3/10 F23R3/283 F23R3/50

    Abstract: Truncated pie shaped bulkhead liner sections (60) are each divided into two liner segments (62). The division occurs adjacent fuel nozzle opening (20). Upstream extending lips (71, 75 and 77) abut the bulkhead (14). Cooling air passes through cooling flow openings in the bulkhead with all the flow continuing toward the shell (38, 40) edges of the liner segments.

    Abstract translation: 截断的饼形隔板衬套部分(60)分别分成两个衬垫段(62)。 分界面邻近燃料喷嘴开口(20)发生。 上游延伸唇缘(71,75和77)邻接舱壁(14)。 冷却空气通过隔板中的冷却流动开口,其中所有的流体都朝着衬套段的壳体(38,40)的边缘继续。

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