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1. 发明专利

CZ8193U1 Capacitance position sensor 未知
公开(公告)号：CZ8193U1
公开(公告)日：1999-03-17
申请号：CZ859898
申请日：1998-10-22
申请人： HAJIC JAN ING , PETRAK JAN
发明人： HAJIC JAN ING , PETRAK JAN
IPC分类号： G01P13/00 , G01P013/00

2. 发明专利

CZ4409U1 Device for indication of deflection from vertical 未知
公开(公告)号：CZ4409U1
公开(公告)日：1996-04-17
申请号：CZ478395
申请日：1995-12-15
申请人： OSTROJ HANSEN REINDERS SPOL S
发明人： BOKIS RADIM , RUNTAK JAROSLAV , SVOBODA ROMAN ING
IPC分类号： G01P13/00 , G01P013/00

3. 发明申请

US20040129071A1 Thermal Finder 审中-公开
标题翻译：热探测器
公开(公告)号：US20040129071A1
公开(公告)日：2004-07-08
申请号：US10248315
申请日：2003-01-08
发明人： Jerzy Plaszowiecki
IPC分类号： G01W001/00 , G01P013/00
CPC分类号： G01W1/10
摘要： An object of the present invention is to provide a system helping glider pilots locate thermals in the air by constructing a database of places on the ground that are likely to generate thermals, and then, given the current weather conditions, showing the projected position of thermals in the air on a graphical display in the cockpit of the flying aircraft. The present invention achieves its objects by utilizing the two following methods: 1. Analyzing past flights from a given geographical area, extracting from them weather conditions during the flight, and places on the ground that have generated thermals in these weather conditions. 2. Analyzing the shape of terrain above which the flight is taking place to find places on the ground that receive the biggest amount of solar energy and wind energy, and therefore are most likely to generate thermals.
摘要翻译：本发明的一个目的是提供一种帮助滑翔机飞行员通过构造可能产生热量的地面数据库来定位热空气的系统的系统，然后，鉴于当前的天气条件，显示出热量的投影位置在空中飞行飞机驾驶舱的图形显示。本发明通过利用以下两种方法实现其目的：1.分析从给定地理区域过去的航班，从飞行中提取天气条件以及在这些天气条件下产生热量的地面。 2.分析飞行发生地形的地形，找到接收最大量太阳能和风能的地面，因此最有可能产生热量。

4. 发明申请

US20040239311A1 Bearing equipped with magnetic encoder and sensor including aligned sensing elements 审中-公开
标题翻译：轴承装有磁性编码器和传感器，包括对准的传感元件
公开(公告)号：US20040239311A1
公开(公告)日：2004-12-02
申请号：US10790624
申请日：2004-03-01
发明人： Alfred John Santos , Mark E. LaCroix , Pascal Desbiolles
IPC分类号： G01B007/30 , G01P013/00 , G01P003/52
CPC分类号： G01P3/443 , F16C41/007 , G01D5/145
摘要： The invention relates to a bearing provided with an annular means generating magnetic pulses and with a device for detecting these pulses, wherein the detection device comprises a plurality of aligned sensitive elements.
摘要翻译：本发明涉及一种具有产生磁脉冲的环形装置和用于检测这些脉冲的装置的轴承，其中检测装置包括多个对准的敏感元件。

5. 发明申请

US20040129094A1 Micromovement measuring device and method of movement process conversion to an electric signal 有权
标题翻译：微动测量装置和移动过程转换为电信号的方法
公开(公告)号：US20040129094A1
公开(公告)日：2004-07-08
申请号：US10474788
申请日：2004-03-01
发明人： Leonids Bekers , Bonifatijs Lubgins , Jehezkelis Finkelshteins , Juris Nurovs , Alexandra Piorunskis
IPC分类号： G01P013/00 , G01D005/12 , G01B007/00
CPC分类号： G01B7/16
摘要： The invention relates to the field of micromovement measuring and can be used for recording creeping and dynamic infraprocesses both of natural and artificial origin, for example, seismic processes or infrasound and gravitation waves. The object of the invention is to raise sensitivity of measuring in a wide dynamic range. The micromovement measuring device consists of measuring element (2) and sensitive element (1), membrane (10), signal conditioner (6), the output of which is connected to the winding og the fixing electromagnet (4). According to the invention, the device is additionally provided with the pulling electromagnet (5), which interacts with the measuring element (2), the winding og the pulling electromagnet being connected to the second inverse output of the signal conditioner (6). The pulling electromagnet shall be preferably located on the membrane (10) that increases the range of the measurable movements. In addition, the prevention of formation of the oxide or similar films at the working surfaces of the measuring (2) and sensitive (1) elements can be provided by their hermetic sealing in space formed by the device housing (11) and the membrane (10). The method of converting movement to electric signal is embodied in said device; this method consists in the fact that the electronic field emission current is taken as a characteristic according to which quantization is made. The proposed approach permits the movements to be recorded in the range of Angstrom units.
摘要翻译：本发明涉及微运动测量领域，可用于记录天然和人造起源的蠕变和动态下拉法，例如地震过程或次声和引力波。本发明的目的是提高在宽动态范围内测量的灵敏度。微动测量装置由测量元件（2）和敏感元件（1），膜（10），信号调节器（6）组成，其输出端连接到固定电磁铁（4）的绕组上。根据本发明，该装置另外设置有与测量元件（2）相互作用的牵引电磁体（5），牵引电磁体与信号调节器（6）的第二反向输出端连接的绕组。牵引电磁体应优选位于膜（10）上，其增加可测量运动的范围。另外，在测量（2）和敏感（1）元件的工作表面上防止氧化物或类似膜的形成可以通过它们由装置壳体（11）和膜（ 10）。将移动转换为电信号的方法体现在所述装置中; 该方法的特征在于，将电场发射电流作为进行量化的特性。所提出的方法允许将运动记录在埃的单位范围内。

6. 发明申请

US20020166375A1 Sideslip correction for a multi-function three probe air data system 有权
标题翻译：多功能三探头空气数据系统的侧滑修正
公开(公告)号：US20020166375A1
公开(公告)日：2002-11-14
申请号：US09850796
申请日：2001-05-08
发明人： Dennis J. Cronin , Thomas D. Amerson
IPC分类号： G01W001/00 , G01P013/00 , A63B053/00
CPC分类号： G01P3/62 , G01C5/06 , G01P5/165 , G01P13/025
摘要： A multi-function probe system that provides redundancy for measurements and compensates for effects of sideslip of an aircraft includes at least two probes that are symmetrically located on the opposite sides of the aircraft, and a third probe mounted on the centerline of the aircraft positioned to directly measure local sideslip with ports that are positioned on opposite sides of the center plane of the aircraft. Each of the probes includes self contained instrumentation for providing signals indicating various pressures. The local angle of sideslip sensed by the third probe is used as a compensation for pressure readings at either of the other probes for determining actual angle of attack, and static pressure.
摘要翻译：提供用于测量并补偿飞行器侧滑的影响的多功能探测系统包括对称地位于飞行器的相对侧上的至少两个探针，以及安装在飞行器的中心线上的第三探针，其位于用位于飞机中心平面对面的端口直接测量局部侧滑。每个探头包括用于提供指示各种压力的信号的自包含仪器。由第三个探头感测到的侧滑的局部角度被用作补偿任何一个其他探头中的压力读数，用于确定实际的迎角和静压。

7. 发明申请

US20040177683A1 Total air temperature probe providing a secondary sensor measurement chamber 审中-公开
标题翻译：提供次级传感器测量室的总气温探头
公开(公告)号：US20040177683A1
公开(公告)日：2004-09-16
申请号：US10387625
申请日：2003-03-13
发明人： Paul A. Ice
IPC分类号： G01W001/00 , G01P013/00
CPC分类号： G01K13/028 , G01K13/02
摘要： A total air temperature sensor probe samples the air stream surrounding an aircraft in flight, and includes a duct carrying a fluid flow a portion of which is diverted to a primary chamber mounting a total air temperature sensor. A secondary chamber has a secondary sensor for sensing a different property of a sampled air stream. The secondary chamber is open to receive air flow from passageways in the total air temperature probe.
摘要翻译：总空气温度传感器探头对飞行中的飞行器周围的空气流进行采样，并且包括承载流体流的管道，其一部分被转移到安装总空气温度传感器的主室。次级室具有用于感测采样空气流的不同性质的次级传感器。二级室打开以接收来自总空气温度探头中的通道的气流。

8. 发明申请

US20040070388A1 Detecting rotational direction of a rotating article 审中-公开
标题翻译：检测旋转物品的旋转方向
公开(公告)号：US20040070388A1
公开(公告)日：2004-04-15
申请号：US10461273
申请日：2003-06-13
发明人： Thomas Hong Chuang , Stephen Gregory Horning
IPC分类号： G01P013/00
CPC分类号： G01P13/04 , G11B5/00813 , G11B27/13 , G11B2005/001 , G11B2220/20
摘要： Method and apparatus for determining the rotational direction of a rotatable article, such as a spindle motor used in a data storage device to rotate a data recording disc. The article includes an index mark which is detected by an index sensor to identify an index reference position on the article. The index sensor and index mark are further used to detect the direction of rotation of the article. In some embodiments, a second sensor is provided so that first and second timing pulses are generated from the index mark by the index sensor and the second sensor. In other embodiments, a second (detection) mark is added to the article so that first and second timing pulses are generated by the index sensor. In either case, a rotational direction detection circuit determines the rotational direction of the article in relation to the first and second timing pulses.
摘要翻译：用于确定旋转物品的旋转方向的方法和装置，例如在数据存储装置中使用的用于旋转数据记录盘的主轴电机。该物品包括由索引传感器检测以识别物品上的索引参考位置的索引标记。索引传感器和索引标记进一步用于检测物品的旋转方向。在一些实施例中，提供第二传感器，使得通过索引传感器和第二传感器从索引标记产生第一和第二定时脉冲。在其他实施例中，将第二（检测）标记添加到物品中，使得第一和第二定时脉冲由索引传感器产生。在任一情况下，旋转方向检测电路确定物品相对于第一和第二定时脉冲的旋转方向。

9. 发明申请

US20030205998A1 Sensor assembly using differential sensing elements for detecting direction of motion of a rotating object 失效
标题翻译：使用用于检测旋转物体的运动方向的差动传感元件的传感器组件
公开(公告)号：US20030205998A1
公开(公告)日：2003-11-06
申请号：US10453041
申请日：2003-06-03
发明人： Joseph Pierre Heremans , Bruno P. B. Lequesne , Thaddeus Schroeder , Avoki M. Omekanda
IPC分类号： G01P013/00
CPC分类号： G01D5/147 , G01P3/488 , G01P13/04
摘要： A target wheel sensor assembly includes a target wheel, a magnet, and two or more sensing elements placed therebetween. The magnet and the sensing elements are configured so that as the target wheel rotates each of the sensing elements outputs a respective asymmetric signal relative to the direction of rotation of the target wheel or an object mechanically connected to the wheel. Each of these asymmetric signals is differentially combined with one another to determine the direction of motion of the target wheel, and, if optionally desired, the position of the target wheel.
摘要翻译：目标轮传感器组件包括目标轮，磁体和放置在它们之间的两个或更多个传感元件。磁体和感测元件构造成使得当目标轮旋转每个感测元件时，相对于目标轮或机械地连接到车轮的物体的旋转方向输出相应的不对称信号。这些不对称信号中的每一个彼此差分地组合以确定目标车轮的运动方向，并且如果可选地，确定目标车轮的位置。

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