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    • 1. 发明申请
    • A HIGH PRESSURE ISOLATION VALVE SYSTEM
    • 高压隔离阀系统
    • WO2007040455A1
    • 2007-04-12
    • PCT/SE2006/050375
    • 2006-10-04
    • NANOSPACE ABSTENMARK, LarsRANGSTEN, Pelle
    • STENMARK, LarsRANGSTEN, Pelle
    • F16K31/02F16K13/00F16K7/12G01L9/12B64G1/40
    • F16K17/383B64G1/402F16K17/403F16K99/0038Y10T137/0497Y10T137/1639Y10T137/1774Y10T137/8122Y10T137/8326
    • An isolation valve system comprises a main body (32), an actuator body (34) and a sealing membrane (307). The sealing membrane (307) is arranged at a high pressure portion (36) of the isolation valve system. The sealing membrane (307) mechanically attaches the actuator body (34) to the main body (32). The sealing membrane (307) further seals the high pressure portion (36) from a low pressure portion (38). A burst plug (315) is arranged against the main body (32) and supports the actuator body (34). An activation arrangement (50) is arranged for allowing an at least partial displacement of the burst plug (315), typically causing a phase transition. The sealing membrane (307) is dimensioned to break when the actuator body (34) is moved due to the displacement of the burst plug (315). The isolation valve system comprises preferably a stack (30) of substrates (301- 304) being bonded together. The substrates (301-304) have micromechanical structures, which form at least the actuator body (34) and the sealing membrane (307).
    • 隔离阀系统包括主体(32),致动器主体(34)和密封膜(307)。 密封膜(307)布置在隔离阀系统的高压部分(36)处。 密封膜(307)将致动器主体(34)机械地附接到主体(32)。 密封膜(307)进一步将高压部分(36)与低压部分(38)密封。 爆破塞(315)抵靠主体(32)设置并支撑致动器主体(34)。 激活装置(50)被布置成允许突发塞(315)的至少部分移位,通常导致相变。 当致动器主体(34)由于爆裂塞(315)的位移而移动时,密封膜(307)的尺寸被设计成断裂。 隔离阀系统优选地包括结合在一起的衬底(301-304)的堆叠(30)。 基板(301-304)具有至少形成致动器主体(34)和密封膜(307)的微机械结构。
    • 2. 发明申请
    • DISTRIBUTED GAS STORAGE
    • 分布式气体储存
    • WO2007032742A1
    • 2007-03-22
    • PCT/SE2006/050334
    • 2006-09-14
    • STENMARK, Lars
    • STENMARK, Lars
    • F17C1/00F17C13/02
    • F17C11/00F17C11/005F17C2201/0128F17C2201/0147F17C2201/0157F17C2250/043Y02E60/321
    • A gas storage system (1) comprises a tank (10), having a tank gas outlet (28), and a multitude of gas emitting entities (20) encapsulated by the tank (10). The gas emitting entities (20) are arranged for providing a gas volume, which when released from said gas emitting entities, is considerably larger than a volume of the gas emitting entities (20) themselves. The gas emitting entities (20) are freely contained in the tank (10), i.e. there are no gas conduits or electrical connections to the tank (10). The tank (10) has a sealable opening (18) suitable for removal or insertion of the gas emitting entities (20) and the gas emitting entities (20) have a respective gas release device, which is operable as a response on a stimulation signal. A volume (14) surrounding the gas emitting entities (20) inside the tank (10) is the sole fluid connection between an opening of the gas release device and the tank gas outlet (28). Methods for storing and releasing gas are also presented.
    • 气体储存系统(1)包括具有罐气体出口(28)的罐(10)和由罐(10)封装的多个气体发射实体(20)。 气体发射实体(20)被布置成提供气体体积,当从所述气体发射实体释放时,气体体积显着大于气体发射实体(20)本身的体积。 气体发射实体(20)自由地容纳在罐(10)中,即没有气体导管或与罐(10)的电连接。 罐(10)具有适合于移除或插入气体发射实体(20)的可密封开口(18),并且气体发射实体(20)具有相应的气体释放装置,其可用作对刺激信号的响应 。 围绕罐(10)内的气体发射实体(20)的体积(14)是气体释放装置的开口和罐气体出口(28)之间的唯一流体连接。 还介绍了储存和释放气体的方法。
    • 3. 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
    • ADVANCED VOLUME GAUGING DEVICE
    • 先进的体积测量装置
    • WO2002101336A1
    • 2002-12-19
    • PCT/SE2002/001120
    • 2002-06-10
    • STENMARK, Lars
    • STENMARK, Lars
    • G01F22/02
    • G01F22/02G01F23/18
    • A new high precision volume gauging system for measuring the volume of a propellant VL enclosed at a first pressure PU within a propellant tank (40) of a volume VT. The improved precision compared with prior art is achieved in that it comprises a high precision pressure sensor (90) which is comprised of a reference chamber (115) that is connected to the propellant tank (40) by a communication line (140), a valve (150) for controlling the gas flow through the line (140), and a high precision differential pressure sensor (95) that is arranged to record the pressure difference between the reference chamber (115) and the propellant tank (40) to which it is connected through a communication line (130).
    • 一种用于测量在体积VT的推进剂罐(40)内的第一压力PU封闭的推进剂VL的体积的新的高精度体积计量系统。 实现了与现有技术相比提高的精度,其包括高精度压力传感器(90),其包括通过通信线路连接到推进剂罐(40)的参考室(115), 用于控制通过管线(140)的气体流动的阀(150)和高精度差压传感器(95),其被配置为记录参考室(115)和推进剂罐(40)之间的压力差, 它通过通信线路(130)连接。
    • 5. 发明申请
    • A MEMBRANE-LESS FUEL CELL
    • 无薄膜燃料电池
    • WO2011010961A1
    • 2011-01-27
    • PCT/SE2010/050862
    • 2010-07-20
    • MÅNBAS ALPHA ABSTENMARK, Lars
    • STENMARK, Lars
    • H01M8/02H01M8/04
    • H01M8/0265H01M8/00H01M8/04097
    • The present invention provides a membrane-less fuel cell that comprises a microfluidic channel system at an interface (5) between two wafers (21, 22) with a fuel gas channel (9) and an oxidiser gas channel (7) overlapping each other in order to make a laminar fuel gas flow in the fuel gas channel (9) to meet a laminar oxidiser fuel gas flow in the oxidiser gas channel (7) in a fuel cell cavity between two parallel electrodes (10, 11), whereby ions are exchanged by diffusion between said flows via a diffusion zone (8). Each of the fuel gas channel (9) and the oxidiser gas channel (7) comprises serially connected sub-cells (1, 2, 3), thereby forming an array of sub-cell cavities for ion exchange. The efficiency of the fuel cell is improved by having a sub-cell configuration that differs from one sub-cell to another. Further the fuel cell can easily be scaled up with maintained efficiency by having a plurality of gas channels forming a matrix of sub-cell cavities.
    • 本发明提供了一种无膜燃料电池,其包括在具有燃料气体通道(9)的两个晶片(21,22)和氧化剂气体通道(7)之间的界面处的界面(5)处的微流体通道系统, 以使得燃料气体通道(9)中的层状燃料气体流动以满足在两个平行电极(10,11)之间的燃料电池腔中的氧化剂气体通道(7)中的层状氧化剂燃料气体流,其中离子为 通过扩散区(8)在所述流之间通过扩散交换。 燃料气体通道(9)和氧化剂气体通道(7)中的每一个包括串联连接的子电池(1,2,3),从而形成用于离子交换的子电池腔阵列。 通过具有不同于一个子单元的子单元配置来提高燃料电池的效率。 此外,燃料电池可以通过具有形成子电池腔矩阵的多个气体通道而容易地按照维持的效率放大。
    • 6. 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, 。
    • 7. 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)。
    • 8. 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。