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公开(公告)号：US08596462B2
公开(公告)日：2013-12-03
申请号：US11547668
申请日：2005-09-09
IPC分类号： B07B4/00
CPC分类号： B01D46/12 , G01N1/2208 , G01N1/2273 , G01N15/0255 , G01N2001/2223
摘要： A separator is disclosed for separating particles of at least first and second mass/size ranges from an ambient fluid (e.g. gaseous) medium in which they are present, particles of the first range being of generally larger size/mass than particles of the second range. The separator is especially designed for use in an air monitoring device which is designed for rapid detection of micro-organisms such as bacteria, viruses, pathogens and the like, and is designed to be portable so that it can be readily and rapidly deployed in both civilian and military environments and can be used indoors and outdoors; it can also be designed for personal use.
摘要翻译： 公开了用于从其存在的环境流体（例如气体）介质中分离至少第一和第二质量/尺寸范围的颗粒的分离器，第一范围的颗粒通常具有比第二范围的颗粒大的尺寸/质量 。 分离器特别设计用于空气监测装置，其被设计用于微生物如细菌，病毒，病原体等的快速检测，并且被设计为便携式，使得其可以容易地并且快速地部署在两者中 民用和军事环境，可在室内外使用; 它也可以设计为个人使用。
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公开(公告)号：US20100170333A1
公开(公告)日：2010-07-08
申请号：US12300564
申请日：2008-09-08
IPC分类号： G01M9/02
摘要： In order to discriminate between laminar flow and turbulent flow states, and to provide an indication, e.g. to a pilot of an aircraft of air flow over an aircraft wing, a sensor mounted on the wing provides an analogue signal of airflow, and an intermittency value of the analogue signal is derived in analogue circuitry including an AC coupling of the signal to an integrator for integrating the signal for a preset time. The integrated value is compared with a threshold value to indicate whether the intermittency represents quiet laminar flow or noisy turbulent flow.
摘要翻译： 为了区分层流和湍流状态，并提供指示，例如， 飞行器机翼上的飞行器飞行员的飞行员，安装在机翼上的传感器提供气流的模拟信号，并且在模拟电路中导出模拟信号的间歇值，包括信号与积分器的AC耦合 用于将信号整合为预设时间。 将积分值与阈值进行比较，以指示间歇性是否表示安静的层流或嘈杂的湍流。
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公开(公告)号：US08607543B2
公开(公告)日：2013-12-17
申请号：US11814927
申请日：2007-05-09
IPC分类号： F23C15/00
CPC分类号： F02K7/02 , F02K7/04 , F05D2230/14 , F05D2250/82 , F05D2250/84 , F05D2300/222
摘要： A millimeter-scale pulse jet engine comprises an engine body that defines a combustion chamber, a fuel, an air intake, and an exhaust. The fuel inlet is arranged to inject fuel directly into the combustion chamber. The air intake and the exhaust are in fluid communication with the combustion chamber, and the combustion chamber is configured such that air from the air intake and fuel from the fuel inlet cyclically combust in the combustion chamber to produce exhaust gases.
摘要翻译： 毫米级脉冲喷气发动机包括限定燃烧室，燃料，进气口和排气的发动机主体。 燃料入口被布置成将燃料直接喷射到燃烧室中。 进气口和排气口与燃烧室流体连通，并且燃烧室构造成使得来自进气口的空气和来自燃料入口的燃料在燃烧室中循环燃烧以产生废气。
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公开(公告)号：US20100275684A1
公开(公告)日：2010-11-04
申请号：US12377467
申请日：2008-09-10
IPC分类号： G01F1/69
摘要： To provide an indication of whether airflow is separated, as opposed to other states of flow, over a surface, two or more adjacent sensors at a location on the surface each produce an analogue signal representative of airflow. The analogue signals are correlated with each other, and the degree of correlation indicates whether the airflow is in a separated state. The correlation may be carried out by comparing processed values of the analogue signals, and thresholding the comparison result.
摘要翻译： 为了提供气流与表面上的其它流动状态相对应的指示，表面上的位置处的两个或更多个相邻传感器产生代表气流的模拟信号。 模拟信号彼此相关，并且相关程度指示气流是否处于分离状态。 可以通过比较模拟信号的处理值和阈值比较结果来执行相关性。
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公开(公告)号：US20090230499A1
公开(公告)日：2009-09-17
申请号：US11597280
申请日：2006-09-19
CPC分类号： G01F1/6845 , G01P5/12 , G01P13/025
摘要： A sensor device for sensing air flow speed at the exterior of an aircraft, comprising a substrate having an upper side on which is mounted a diaphragm over an aperture or recess in the substrate, the diaphragm being thermally and electrically insulative, and mounting on its upper surface a heating element comprising a layer of resistive material, and wherein electrical connections to the heating element are buried in the diaphragm and/or the substrate, and provide electrical terminals at the lower side of the substrate. The heating element is exposed to the environment, but the remaining electrical parts of the device are not exposed.
摘要翻译： 一种用于感测飞行器外部的空气流速的传感器装置，包括具有上侧的基板，在基板上的孔或凹部上安装有隔膜，所述隔膜具有热和电绝缘性，并且安装在其上部 表面包括电阻材料层的加热元件，并且其中与所述加热元件的电连接被掩埋在所述隔膜和/或所述基板中，并且在所述基板的下侧提供电端子。 加热元件暴露于环境中，但是该设备的其余电气部分不暴露。
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公开(公告)号：US07458287B2
公开(公告)日：2008-12-02
申请号：US11547654
申请日：2005-11-02
IPC分类号： G01N15/00
CPC分类号： G01N15/0255 , G01N1/2208 , G01N1/2273 , G01N2001/2223 , G01N2015/0261
摘要： A particle sampling device is disclosed for separating and collecting particles of at least first and second mass/size ranges from an ambient fluid (e.g. gaseous) medium in which they are present, particles of the first range being of generally larger size/mass than particles of the second range. The separator is especially designed for use in an air sampling device which is designed for rapid detection of micro-organisms such as bacteria, viruses, pathogens and the like, and is designed to be portable so that it can be readily and rapidly deployed in both civilian and military environments and can be used indoors and outdoors; it can also be designed for personal use.
摘要翻译： 公开了一种用于从其存在的环境流体（例如气体）介质中分离和收集至少第一和第二质量/尺寸范围的颗粒的颗粒取样装置，第一范围的颗粒的尺寸通常大于/ 的第二范围。 分离器特别设计用于空气采样装置，其被设计用于微生物如细菌，病毒，病原体等的快速检测，并且被设计为便携式，使得其可以容易地并且快速地部署在两者中 民用和军事环境，可在室内外使用; 它也可以设计为个人使用。
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公开(公告)号：US08143689B2
公开(公告)日：2012-03-27
申请号：US11597280
申请日：2006-09-19
IPC分类号： H01L31/058
CPC分类号： G01F1/6845 , G01P5/12 , G01P13/025
摘要： A sensor device for sensing air flow speed at the exterior of an aircraft, comprising a substrate having an upper side on which is mounted a diaphragm over an aperture or recess in the substrate, the diaphragm being thermally and electrically insulative, and mounting on its upper surface a heating element comprising a layer of resistive material, and wherein electrical connections to the heating element are buried in the diaphragm and/or the substrate, and provide electrical terminals at the lower side of the substrate. The heating element is exposed to the environment, but the remaining electrical parts of the device are not exposed.
摘要翻译： 一种用于感测飞行器外部的空气流速的传感器装置，包括具有上侧的基板，在基板上的孔或凹部上安装有隔膜，所述隔膜具有热和电绝缘性，并且安装在其上部 表面包括电阻材料层的加热元件，并且其中与所述加热元件的电连接被掩埋在所述隔膜和/或所述基板中，并且在所述基板的下侧提供电端子。 加热元件暴露于环境中，但是该设备的其余电气部分不暴露。
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公开(公告)号：US07984879B2
公开(公告)日：2011-07-26
申请号：US11995233
申请日：2007-08-31
申请人： Michael Victor Cook , Clyde Warsop
发明人： Michael Victor Cook , Clyde Warsop
IPC分类号： B64C21/04
摘要： A flow control actuator 10 for a body exposed to fluid flow comprises first and second flow surfaces 14, 16 spaced to define an elongate gap 20 therebetween. An elongate control element is disposed in or adjacent the gap and has an externally facing arcuate surface and defines a first slot 24 between the control element and said first flow surface and a second slot between said control element and said second flow surface 26. The control element 22 is moveable to allow the width of said slots to be adjusted generally proportionally. The flow of pressurized flow control fluid passes from a plenum chamber 30 out through one or both slots 24, 26 to be deflected around the arcuate surface under the influence of the Coanda effect. The flow control actuator 10 may be provided in the trailing or leading edge of an aerofoil; alternatively it may be provided between two surfaces spaced to provide said gap but otherwise providing a generally continuous surface.
摘要翻译： 用于暴露于流体流动的主体的流量控制致动器10包括间隔开的第一和第二流动表面14,16，以在其间限定细长间隙20。 细长的控制元件设置在间隙中或邻近间隙并且具有外部面对的弓形表面并且在控制元件和所述第一流动表面之间限定第一槽24和在所述控制元件和所述第二流动表面26之间的第二槽。控制 元件22可移动以允许所述槽的宽度大致成正比地调节。 加压流量控制流体的流动从通风室30通过一个或两个狭槽24,26，在柯恩达效应的影响下绕弧形表面偏转。 流量控制致动器10可以设置在机翼的后缘或前缘中; 或者可以在间隔开的两个表面之间提供以提供所述间隙，但是另外提供大致连续的表面。
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公开(公告)号：US07942994B2
公开(公告)日：2011-05-17
申请号：US11815875
申请日：2007-05-23
申请人： Martyn John Hucker , Clyde Warsop
发明人： Martyn John Hucker , Clyde Warsop
IPC分类号： B32B37/00
CPC分类号： B81C3/001 , B32B37/12 , B32B2457/14 , H01L41/313 , Y10T156/17
摘要： A bonding tool and method A bonding tool and method for bonding together layers of a MEMS transducer device, including at least one layer of a piezoelectric material, and an intermediate reinforcing layer of titanium, or other metal, comprising: positioning the layers above one another and spaced apart by means of spacing members, heating said layers to a bonding temperature, and retracting the spacing members so as to bring the layers together under pressure to effect a bond between adjacent surfaces of the layers, wherein a press head is employed with a compliant caul for evenly distributing the press force; and permitting said layers to cool to an operating temperature in which said piezoelectric layer is under compressive strain and the titanium layer is under tensile strain.
摘要翻译： 一种接合工具和方法用于将包括至少一层压电材料的MEMS换能器装置的层与钛或其它金属的中间加强层粘合在一起的粘结工具和方法包括：将层定位在彼此之上 并且通过间隔构件间隔开，将所述层加热至接合温度，并缩回间隔构件，以便在压力下将层压在一起，以实现层的相邻表面之间的结合，其中使用压头 均匀分布压力; 并允许所述层冷却至所述压电层处于压应变状态并且钛层处于拉伸应变下的工作温度。
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10.发明授权Thrust vectoring apparatus for a jet engine, corresponding jet engine, thrust vectoring method and upgrading method for a jet engine 有权用于喷气发动机的推力矢量装置，相应的喷气发动机，用于喷气发动机的推力矢量化方法和升级方法公开(公告)号：US08887484B2
公开(公告)日：2014-11-18
申请号：US13002532
申请日：2009-06-23
申请人： Clyde Warsop
发明人： Clyde Warsop
摘要： The thrust vectoring apparatus comprises: a housing defining a primary outlet for emitting the primary jet; Coanda surfaces extending from opposing regions of said housing, and radially spaced from the primary outlet such that a step is defined between each Coanda surface and the primary outlet; ducts leading from a fluid source to secondary outlets; and flow control means operable to control the mass flow through the secondary outlets. When the jet engine operates to exhaust a primary jet through the primary outlet, low pressure regions are formed in the vicinity of the steps. Each secondary outlet is located adjacent one of the Coanda surfaces so as to emit a secondary flow into a low pressure region. On activation of the secondary flow by the flow control means, the primary jet is entrained by the Coanda surface opposing the Coanda surface adjacent said the secondary outlet from which the secondary flow has been emitted. Method of vectoring the thrust or of upgrading existing jet engines with the thrust vectoring apparatus and jet engines comprising the thrust vectoring apparatus are disclosed.
摘要翻译： 推力矢量装置包括：壳体，其限定用于发射主射流的主出口; 柯南达表面从所述壳体的相对区域延伸并且与主出口径向间隔开，使得在每个科安达表面和主出口之间限定一个步骤; 从流体源引导到二级出口的管道; 流量控制装置可操作以控制通过次级出口的质量流量。 当喷气发动机操作以通过主出口排出主喷射器时，在台阶附近形成低压区域。 每个次级出口位于附近的一个Coanda表面，以便将二次流发射到低压区域。 在通过流量控制装置启动二次流动时，主喷流被柯南达表面所夹带，所述柯恩达表面与邻近所述二次流出口的次级出口相邻的柯安达表面相对。 公开了用推力矢量装置和包括推力矢量装置的喷气式发动机对推力或升级现有喷气发动机的方法。
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