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    • 1. 发明申请
    • MICROMECHANICAL SLOW ACTING VALVE SYSTEM
    • 微机械慢动作阀系统
    • WO2008066485A1
    • 2008-06-05
    • PCT/SE2007/050912
    • 2007-11-28
    • ÅSTC AEROSPACE ABSTENMARK, Lars
    • STENMARK, Lars
    • F15C5/00F16K31/365F16K31/165F16K7/17
    • F16K99/0001F16K99/0005F16K99/0059F16K2099/0074F16K2099/0076F16K2099/0084
    • The present invention provides an integrated microvalve system (1) comprising at least a first fluid branch (8) and a microvalve (2) being controlled by a control pressure in a control channel (17). The microvalve (2) is adapted to control a fluid flow in the first fluid branch (8). A flow restrictor arrangement (21) is located between a control port (19) and the control channel (17) to give a pre- determined turn-on and turn-off response characteristics of the microvalve (2). Preferably the flow restrictor arrangement (21) comprises a deflate channel (30) and an inflate channel (31) arranged in parallel. Each channel (30, 31) comprises a check valve (34, 35) and a flow restrictor (24, 25), which may have different flow restriction to give different turn-on and turn-off response characteristics for the microvalve (2).
    • 本发明提供了一种集成的微型阀系统(1),其包括由控制通道(17)中的控制压力控制的至少第一流体分支(8)和微型阀(2)。 微型阀(2)适于控制第一流体分支(8)中的流体流动。 流量限制器装置(21)位于控制端口(19)和控制通道(17)之间,以给出微型阀(2)的预定的导通和关断响应特性。 优选地,限流器装置(21)包括平行布置的放气通道(30)和膨胀通道(31)。 每个通道(30,31)包括止回阀(34,35)和限流器(24,25),其可以具有不同的流量限制,以给出微阀(2)的不同的导通和关断响应特性, 。
    • 2. 发明申请
    • MINIATURIZED HIGH CONDUCTIVITY THERMAL/ELECTRICAL SWITCH
    • 微型高电导率热电开关
    • WO2007084070A1
    • 2007-07-26
    • PCT/SE2007/050030
    • 2007-01-18
    • ÅSTC AEROSPACE ABSTENMARK, Lars
    • STENMARK, Lars
    • H01L23/427B81B3/00B81B7/00H01H1/00
    • H01H37/36H01H37/46H01H2037/008
    • The present invention is a thermally controlled switch with high thermal or electrical conductivity. Microsystems Technology manufacturing methods are fundamental for the switch that comprises a sealed cavity 213 formed within a stack of bonded wafers 201 , 202, wherein the upper wafer 202 comprises a membrane assembly 205 adapted to be arranged with a gap 21 1 to a receiving structure 210. A thermal actuator material 215, which preferably is a phase change material, e.g. paraffin, adapted to change volume with temperature, fills a portion of the cavity 213. A conductor material, providing a high conductivity transfer structure 216 between the lower wafer 201 and the rigid part 208 of the membrane assembly 205, fills another portion of the cavity 213. Upon a temperature change, the membrane assembly 205 is displaced and bridges the gap 21 1 , providing a high conductivity contact from the lower wafer 201 to the receiving structure 210.
    • 本发明是具有高导热性或导热性的热控开关。 微系统技术制造方法是开关的基础,该开关包括形成在结合晶片201,202的叠层内的密封腔213,其中上晶片202包括膜组件205,膜组件205适于布置成与接收结构210间隙21 1 热致动器材料215,其优选为相变材料,例如 石蜡,适于随温度改变体积,填充空腔213的一部分。在下部晶片201和膜组件205的刚性部分208之间提供高电导率传递结构216的导体材料填充空腔的另一部分 温度变化时,膜组件205移位并桥接间隙21 1,从下晶片201向接收结构210提供高电导率的接触。
    • 4. 发明申请
    • MICRO SYSTEM BASED SOLID STATE GAS STORAGE
    • 基于微系统的固态气体储存
    • WO2008066486A1
    • 2008-06-05
    • PCT/SE2007/050913
    • 2007-11-28
    • ÅSTC AEROSPACE ABSTENMARK, Lars
    • STENMARK, Lars
    • B01J7/00F02K9/36F17C11/00
    • F02K9/36F02K9/95F17C11/00
    • The present invention provides a gas storage system (1) comprising individually addressable igniters (23) arranged as a two dimensional array in an igniter module (20) and fuel elements (2) extending from an end surface (21) of the igniter module (20). By igniting a fuel element (2) using an adjacent igniter (23), a decomposition of a solid propellant (9) in the fuel element (2) generates a gas (15). Deflection shields (28) may be arranged about the fuel elements (2) to thermally shield adjacent fuel elements (2) and to provide structural support. The gas storage system (1) may further comprise a tank (40) having a gas outlet (41); a filter module (50); and a control module (60). Thanks to the invention it is possible to provide a solid state gas storage system (1) having a high gas storage capacity per mass unit.
    • 本发明提供了一种气体存储系统(1),其包括在点火器模块(20)中排列成二维阵列的单独可寻址的点火器(23)和从点火器模块的端面(21)延伸的燃料元件(2) 20)。 通过使用相邻的点火器(23)点燃燃料元件(2),燃料元件(2)中的固体推进剂(9)的分解产生气体(15)。 偏转屏蔽件(28)可围绕燃料元件(2)布置以对相邻的燃料元件(2)进行热屏蔽并提供结构支撑。 气体储存系统(1)还可包括具有气体出口(41)的罐(40); 过滤器模块(50); 和控制模块(60)。 由于本发明,可以提供一种每质量单位具有高的储气容量的固态气体储存系统(1)。
    • 5. 发明申请
    • MICROMACHINED CONTINUOUS TIME DELAY PHASE SHIFTER
    • MICROMACHINED连续延时相移
    • WO2007084071A1
    • 2007-07-26
    • PCT/SE2007/050031
    • 2007-01-18
    • ÅSTC AEROSPACE ABSTENMARK, Lars
    • STENMARK, Lars
    • H01P3/00H01Q1/36
    • H01P1/184
    • The present invention relates to methods and structures for improved high speed radio transmission systems using phased array antennas. According tot the invention as phase shifter with a variable transmission line length is provided. The phase shifter has a microstrip or coplanar transmission line with a movable part (107) and a fixed part (105), wherein the movable part (107) is arranged in parallel and adjacent to the fixed part (105). The movable part (107) is arranged so that an end portion of the movable part (107) overlap an end portion of the fixed part (105) with a gap (115) between the movable part (107) and the fixed part (105), the gap (120) providing a capacitive coupling. By displacing the movable part (105) the length of the overlapping section (120) is varied and consequently the transmission line length of the phase shifter is varied.
    • 本发明涉及使用相控阵天线的改进的高速无线电传输系统的方法和结构。 根据本发明,提供了具有可变传输线长度的移相器。 移相器具有带有可移动部分(107)和固定部分(105)的微带或共面传输线,其中可移动部分(107)平行布置并与固定部分(105)相邻。 所述可动部(107)的配置使得所述可动部(107)的端部与所述固定部(105)的端部与所述可动部(107)与所述固定部(105)之间的间隙(115)重叠 ),所述间隙(120)提供电容耦合。 通过移动可移动部分(105),重叠部分(120)的长度是变化的,因此移相器的传输线长度是变化的。