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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：US20100126140A1
公开(公告)日：2010-05-27
申请号：US11814927
申请日：2007-05-09
IPC分类号： F02K7/02
CPC分类号： F02K7/02 , F02K7/04 , F05D2230/14 , F05D2250/82 , F05D2250/84 , F05D2300/222
摘要： A millimetre-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：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：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：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：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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公开(公告)号：US08322206B2
公开(公告)日：2012-12-04
申请号：US12300564
申请日：2008-09-08
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性值，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：US08061194B2
公开(公告)日：2011-11-22
申请号：US12377467
申请日：2008-09-10
IPC分类号： G01F1/68
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：US20100139860A1
公开(公告)日：2010-06-10
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
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合工具和方法包括：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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