| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 21 | 一种通风柜及通风柜面风速测量方法及装置 | CN201510846797.1 | 2015-11-27 | CN106814213A | 2017-06-09 | 孔鹏; 汪建锋 |
| 本发明提供一种通风柜及通风柜面风速测量方法及装置，所述通风柜面风速测量装置包括：设置于通风柜的正面通风区域的边缘至少一个测量探头传感器；所述测量探头传感器为热电阻探头传感器、热电偶探头传感器和/或压差传感器。所述测量探头传感器根据所测量的风速获取所述通风柜的面风速：去除所述测量探头测得的风速的最大值和最小值后获取所述风速的平均值，获取的所述风速的平均值即为所述通风柜的面风速。本发明可以完全避免外界气流的扰动，而且测量不受通风柜的视窗的高度影响，有利于提高测量精度，而且本发明安装方便，安装要求低，适应性强，工厂标定后，即可现场安装，无需现场再次标定，具有较强的通用性和实用性。 | ||||||
| 22 | 一种数显式烟气流速流量测量方法 | CN201610399748.2 | 2016-06-08 | CN106092219A | 2016-11-09 | 田必勇 |
| 本发明公开了一种数显式烟气流速流量测量方法，重金属测量模块、流量测量模块通过将气道内的重金属浓度和烟气流量进行采集，将采集的信息进行传递后输送给AD转换模块，AD模块将各个采集模块采集的数据进行模数转换，将数据传输给MCU进行分析，并将分析的数据输送至存储器，所述风机模块与差压变送器进行连接，差压变送器能够将风机输送出的风量进行压力控制和风力控制，能够进行烟气和烟量进行差压控制，显示器将MCU的数据进行数字显示。本发明能够快速、准确地获得流速信息，并能够对流量设备进行防护作用，避免设备受到外来因素的影响，导致设备产生故障。 | ||||||
| 23 | 静压端口装置 | CN201110344251.8 | 2011-11-03 | CN102466537B | 2015-10-21 | T·T·戈利 |
| 一种航行器的静压端口装置，该静压端口装置具有静压板，该静压板具有固定在所述航行器上的内表面和外表面。该静压板包括第一组多个端口孔和至少第二组多个端口孔。所述第二组端口孔的每个端口孔相对于所述第一组端口孔的每个端口孔同轴定位。 | ||||||
| 24 | 三维流速矢量能量与质量测量仪 | CN201310076423.7 | 2013-03-11 | CN103148992A | 2013-06-12 | 杜国平; 杜家佳; 宋晓峰; 杜广林 |
| 一种三维流速矢量能量与质量测量仪，其特征是它包括弹性皮囊（1），弹性皮囊（1）的两端各安装有一个刚性密封堵头（2），所述弹性皮囊（1）及所述的刚性密封堵头（2）形成一圆柱形密封腔体，其中上端的刚性密封堵头上设有电缆连接线进出孔，下端的刚性密封堵头上设有用于向所述圆柱形密封腔体中注入液体的注液孔，注液孔上安装有密封塞；圆柱形密封腔体中安装有测量流速矢量能量的测量装置及测量质量的装置。它具有结构简单，制造方便、检测全面的优点。 | ||||||
| 25 | 用于确定飞行器空速的方法和装备有实施装置的飞行器 | CN201210242345.9 | 2012-07-13 | CN102879602A | 2013-01-16 | J.费奥; F.雨果 |
| 用于确定飞行器空速的方法和装备有实施装置的飞行器。本发明的目的在于在基于关联测量的手段不适用的部分飞行场中，能够供给足够精确和可使用的飞行器的备选空速信息记录。为此，本发明利用由在所述飞行器的飞机高度下可在系统中工作的飞行器发动机供给的压力信息。飞行器装备有由至少一个吊舱和一个压缩机/涡轮机栓构成的发动机，飞行器包括至少一个数据处理单元以及在发动机水平下的至少一个系统。飞行器的至少一个发动机装备有至少一个被布置在所述吊舱下面的环境空气静压探头、被布置在发动机水平处的空气静压探头、一个位于压缩机输出端的压力探头、至少一个例如鼓风机的转速传感器、和位于空气输出端或在任何压缩点处的环境空气温度探头。 | ||||||
| 26 | 多功能便携式电子装置 | CN200910302060.8 | 2009-04-30 | CN101876662B | 2012-06-13 | 贾立进 |
| 本发明提供一种多功能便携式电子装置，具有移动电话的功能，其包括一本体，该本体内设有依次电性连接的电源模块、显示模块、信号处理器、模数转换器、风速传感器及控制模块。该本体上设有一显示屏，该显示屏与显示模块连接。该控制模块控制风速传感器的工作。该风速传感器用于感测风力，并产生一电压变化值。该模数转换器将该电压变化值转换成数字信号。所述信号处理器处理该数字信号并得出对应的风速值，并将该风速值传送至显示模块，显示模块驱动显示屏显示该风速值。该多功能便携式电子装置简化人们随身携带的物品，并可测量风速。 | ||||||
| 27 | 气液两相流的速度与气体含量的传感器 | CN201110208471.8 | 2011-07-25 | CN102411062A | 2012-04-11 | 路明 |
| 本发明公开了一种气液两相流的速度与气体含量的传感器。包括一个外形呈长圆柱形、测量端部呈圆锥台形状的测量探头、四个压力传感器、一个用于压力传感器的背压平衡器、三个导电电极、一个基于压力信号的电极对选择电路和数据采集管理系统。沿着测量探头中心轴线，在测量端有一个中心孔，沿着圆周方向均匀地分布着另外六个孔，中心孔和其中三个孔是压力孔，另外三个是电极孔。利用四个压力孔的压差值可以确定两相流体的三维流动速度和方向，同时利用导电电极可以测量两相流中气体的含量。 | ||||||
| 28 | 用于在地面上检测飞机的静压力传感器的压力测量嘴阻塞的方法和装置 | CN200680004695.4 | 2006-02-02 | CN100559139C | 2009-11-11 | L·方托瓦; S·弗赖西纳特 |
| 本发明涉及用于在地面上检测飞机的静压力传感器的压力测量嘴的障碍的方法及装置。装置(1)包括被设置用来测量探测器(4)内部压力的压力传感器(2)，压力传感器(2)具有用于加热探测器(4)的加热系统(9)；并且当加热系统(9)被激活时，传感器(2)完成至少一个参数的第一测量，所述参数与探测器(4)内部压力相关，并且在加热系统(9)激活之后的预定的持续时间内完成所述参数的第二测量。本发明的装置还包括至少一个中央处理器(11)，用于计算第一与第二测量值之间的差值，并把这个差值与预定值比较；并且本发明的装置包括报警装置(13)，用于如果差值大于所述预定值时发出指示检测到障碍的报警信号。 | ||||||
| 29 | 用于在地面上检测飞机的静压力传感器的压力测量嘴阻塞的方法和装置 | CN200680004695.4 | 2006-02-02 | CN101120238A | 2008-02-06 | L·方托瓦; S·弗赖西纳特 |
| 本发明涉及用于在地面上检测飞机的静压力传感器的压力测量嘴的障碍的方法及装置。装置(1)包括被设置用来测量探测器(4)内部压力的压力传感器(2)，压力传感器(2)具有用于加热探测器(4)的加热系统(9)；并且当加热系统(9)被激活时，传感器(2)完成至少一个参数的第一测量，所述参数与探测器(4)内部压力相关，并且在加热系统(9)激活之后的预定的持续时间内完成所述参数的第二测量。本发明的装置还包括至少一个中央处理器(11)，用于计算第一与第二测量值之间的差值，并把这个差值与预定值比较；并且本发明的装置包括报警装置(13)，用于如果差值大于所述预定值时发出指示检测到障碍的报警信号。 | ||||||
| 30 | 风速指示设备 | CN94119489.2 | 1994-12-13 | CN1062659C | 2001-02-28 | 诸星博; 增田裕一; 黑木保雄 |
| 一种风速指示设备，具有：风速测量单元，用于测量风速；方位测量单元，用于测量方位；显示单元，用于显示在各个方位上测量的风速；以及显示控制单元，用于根据方位测量单元和风速测量单元的测量结果控制显示单元显示在各个方位上测量的风速。从而，风的吹向可由该方位指示设备指示。 | ||||||
| 31 | 能指示风向的装配在风速计上的方位指示器 | CN94119489.2 | 1994-12-13 | CN1113317A | 1995-12-13 | 诸星博; 增田裕一; 黑木保雄 |
| 一种方向指示设备，具有：风速测量单元，用于测量风速；方位测量单元，用于测量方位；显示单元，用于显示在各个方位上测量的风速；以及显示控制单元，用于根据方位测量单元和风速测量单元的测量结果控制显示单元显示在各个方位上测量的风速。从而，风的吹向可由该方位指示设备指示。 | ||||||
| 32 | 전달력이 향상된 도로용 스피커를 이용한 도로 정보 방송 시스템 | KR1020170067162 | 2017-05-30 | KR1020170087838A | 2017-07-31 | 제영호; 임용묵 |
| 본발명은전달력이향상된도로용스피커를이용한도로정보방송시스템에관한것으로, 더욱상세하게는음향출력을위한혼을갖고, 상기혼의일면부가평평하게형성되며, 도로를따라일정간격으로설치되는복수의도로용스피커, 음향신호를증폭시키는앰프, 및상기도로이동차량의진행방향을따라배열된각 도로용스피커들을지연출력시키는메인제어부,를포함한다. 상기와같은본 발명에의하면, 복수의도로용스피커를이용하여이동하는차량을향해정보를음향으로지연출력함에따라, 차량내부에서정보를명확하게확인할수 있게하여상황파악은물론, 신속하게대처할수 있다. | ||||||
| 33 | 회전 블레이드용의 블레이드-장착식 전압 프로브 | KR1020007005826 | 1998-12-04 | KR1020010032580A | 2001-04-25 | 잭슨마이클이. |
| 로터블레이드용의블레이드-장착식전압(BMTP) 프로브는베이스부분및 입구부분으로구성된다. 상기베이스부분은, 로터블레이드와결합하는상기 BMTP 프로브를착탈가능하게장착시키기위하여로터블레이드의공기역학면과상보적인평면형태를갖는경계면, 이경계면과인접하며앞쪽모서리, 제 1 및제 2 유동면을포함하는공기역학적으로유선형을갖는본체및, 이공기역학적으로유선형을갖는본체및 상기경계면을통과하여신장하는유체연통구멍을포함한다. 상기입구부분은, 공기역학적으로유선형을갖는상기본체와인접하는하부벽, 이하부벽과인접하는대향측벽및, 이대향측벽과인접하는상부벽에의해형성되는입구를포함한다. 상기입구부분은또한상기하부벽, 대향측벽, 및상부벽과인접하는후방벽을포함하며, 상기후방벽, 하부벽, 대향측벽및, 상부벽은서로결합하여입구부분내에수집챔버를형성한다. 유체연통구멍은이 하부벽을통과하여상기베이스부분의유체연통구멍과정렬관계에있도록신장한다. 배출포트는메인로터블레이드의회전중심으로부터상기대향측벽의말단부를통과하도록형성된다. | ||||||
| 34 | 풍속계를 위한 시스템 및 방법 | KR1020160010382 | 2016-01-28 | KR1020160094312A | 2016-08-09 | 프로에멜안드레아스; 마르세츠발데마르 |
| 소정의실시예에따르면, 풍속을측정하는방법은케이스내부에배열되고바람으로부터차폐된제1 압력센서에서대기압을측정하고, 케이스내의개구에배열된제2 압력센서에서공기압을측정하고, 대기압및 공기압을측정하는것에기초하여케이스내의개구에서풍속을결정하는것을포함한다. | ||||||
| 35 | 내부 공기 유동을 이용한 이중배관 밀폐 손상 탐지 장치 | KR2020140008049 | 2014-11-05 | KR2020160001590U | 2016-05-13 | 윤준영; 김태훈; 이순기; 이재봉 |
| 본고안은내부공간에수소등과같은피수송기체가유통하는내관과, 상기내관을둘러싸고외부공간에불활성가스가유통하는외관을포함하며, 상기외관의일측에위치하며유체의압력차를측정할수 있는센서가설치된벤츄리를더 포함함으로서, 일정한양의공기유량이항상내관과외관사이를지날수 있도록하며, 사이에흐르는공기유동의유속을이용해유량변화를탐지함으로서, 유량이증가하면내관의밀폐상태가손상되어내관내부의물질이외관으로누출이발생한것으로판단하고, 유량이감소하면외관의밀폐상태가손상되어외관에서외기로공기가누출된것으로판단되므로내관뿐만아니라외관의손상애대한탐지도가능한효과를도모할수 있는내부공기유동을이용한이중배관밀폐손상탐지장치에관한것이다. | ||||||
| 36 | 허니콤 입구를 갖는 벤츄리 구조의 풍속계 | KR1020140122901 | 2014-09-16 | KR1020160032583A | 2016-03-24 | 김성훈 |
| 본발명에따른허니콤입구를갖는벤츄리구조의풍속계벤츄리관내부를통과하는바람의압력정보를측정하여베르누이방정식에의해벤츄리관으로유입되는바람의속도(풍속)을산출하도록하고, 특히바람이유입되는부위가허니콤구조로이루어져벤츄리관내부에서의바람속도구배가균일해지도록하여풍속계측오차를최소화시키면서계측정밀도를향상시키게된다. 본발명에따른허니콤입구를갖는벤츄리구조의풍속계는전후방향으로개방되고, 개방된전면으로부터바람이유입되도록하는바람유입관; 바람유입관의후면으로부터후측으로연장형성되되상기바람유입관보다작은크기로이루어지며, 전후방향으로개방되어바람유입관을거친바람이통과하게되는연결관; 연결관의후면으로부터후측으로연장형성되되상기연결관보다큰 크기로이루어지며, 전후방향으로개방되어연결관을거친바람이통과하여외부로배출되는바람배출관; 바람유입관, 연결관의압력정보를측정하는압력계및; 압력계와연결되어바람유입관, 연결관의압력정보를전달받고, 바람유입관과연결관의형상정보와치수정보가저장되어있으며, 바람유입관과연결관의형상정보와치수정보및 바람유입관, 연결관의압력정보으로부터바람유입관으로유입되는바람의풍속을산출하는컨트롤러를포함하는구성으로이루어진다. | ||||||
| 37 | 기압 변화를 이용한 속도센서 | KR1020120151111 | 2012-12-21 | KR101384588B1 | 2014-04-11 | 윤종채; 이상열 |
| The present invention relates to a speed sensor which uses an atmospheric pressure which detects a speed according to atmospheric pressure changes by using Bernoulli′s equation. The present invention measures an atmospheric pressure change according to speed changes of sport equipment by being installed in the sport equipment to measure a speed and outputs the measured change to the outside by converting the measured change into a speed by including: a substrate part on which an electronic circuit is printed; a barometer which is installed in the front side of the substrate part, measures an atmospheric change, and provides the atmospheric change as an electrical signal; a control part which receives an atmospheric pressure signal by being electrically connected with the barometer and outputs an electrical signal by converting the atmospheric pressure signal into a speed from a built-in pressure/speed converting table; a digital display window which is mounted in the rear surface of the substrate part and displays a speed-related electrical signal which is provided from the control part to the outside as a number; a power supply part which is installed in the substrate part and includes an electric condenser which supplies power to the control part; and a power switch which is installed in the rear surface of the substrate part and enables a user to selectively operate a sensor by turning on/off the power supply of the power supply part. According to the present invention, not only user convenience but also improved excellent effects are obtained to contribute to the improvement of sports ability by immediately measuring the speed of sport equipment in case of a swing of the sport equipment by being installed in the sport equipment including a badminton racket, a golf club, or a baseball bat. | ||||||
| 38 | 자동 수트블로워가 구비된 선박의 에코노마이저 | KR1020090109331 | 2009-11-12 | KR1020110052341A | 2011-05-18 | 오정한; 배진우 |
| PURPOSE: An economizer of a ship with an automatic soot blower is provided to enhance the heat efficiency since a soot blower periodically operates automatically to remove soot. CONSTITUTION: An economizer of a ship comprises a heat exchanger(10), a soot blower(20), an opening/closing valve(30), a temperature sensor(40), a pressure difference sensor(50), and a controller(60). The heat exchanger is installed on the flow path of waste gas and absorbs heat from the waste gas. The soot blower is installed on one side of the heat exchanger and sprays steam to the heat exchanger. The opening/closing valve controls the passing of air supplied to the soot blower. The temperature sensors are respectively installed on the entrance and exit of the heat exchanger. The pressure difference sensor is installed on one side of the heat exchange and senses the pressure difference between the entrance and exit of the heat exchanger. | ||||||
| 39 | VENTURI OMEGA DEVICE | PCT/IB2012000561 | 2012-03-20 | WO2013140194A3 | 2014-05-15 | ORTEGA BELTRAN MARCO ANTONIO |
| Venturi Omega is a hydro-pneumatic-device made up of two principal elements and aggregate. The aggregate may be a single element or a composed whole of many items. The two principal elements are 1 the membrane and a closing element or flow-stopper: 2 the ball, sphere or stopper. Some of the performances of the device are the following: The self-closing of the device The displacement of the ball and or the membrane which allows further actions. The displacement is originated by changes in the pressures relationship between the pressures on both sides of the membrane, the inner- and outer-side The increasing closing-force whit bigger softness of the ball The easy opening of the device and the easy handling of the flow-control, flow-monitoring and flow-measure, particularly pressure- and differential-pressure-measures. The Venturi Omega is a versatile elastic-dynamic-device. Till jet we have developed among others the following useful devices: A safety-valve whit all the working elements or machinery lying in the outer side of the membrane thus not contaminating the fluid and not being corroded and wearing away by the flow. An airplane-speedometer A barometer or atmospheric-pressure-monitoring-device A pneumatic "no hands" tap A top-level-control-device Several pressure- and differential-pressure-measure- and monitoring-devices The Venturi Omega balloons. The WC tube rinse devises. | ||||||
| 40 | AIR DATA SYSTEM AND METHOD FOR ROTARY AIRCRAFT | PCT/US2005024559 | 2005-07-12 | WO2006093520A9 | 2007-02-15 | ROUSE GORDON F; THOMAS STEVEN H; ELGERSMA MICHAEL R |
| An air data system and method for a rotary aircraft is described. The air data system includes a plurality of flush ports (202) connected via tubing (304) to a plurality of air flow sensors (302) that can measure air flow speeds as low as approximately 0.02 knots. The flush ports are arranged around a main rotor shaft (108) and below a rotor hub (310) of the rotary aircraft to help reduce the impact of rotor downwash. The flush ports and tubing permit air to flow into the air flow sensors, which allows the plurality of air flow sensors to measure speed and direction of cross-wind components of air flow surrounding the rotary aircraft. | ||||||
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