SAMPLE STORAGE AND MONITORING SYSTEM
    51.
    发明公开
    SAMPLE STORAGE AND MONITORING SYSTEM 审中-公开
    PROBENLAGERUNGS- UNDÜBERWACHUNGSSYSTEM

    公开(公告)号:EP2509412A1

    公开(公告)日:2012-10-17

    申请号:EP10835290.7

    申请日:2010-12-07

    申请人: Bluechiip Pty Ltd

    摘要: A system for storing and monitoring samples in a temperature-controlled storage environment, including one or more containers each housing one of the samples; a machine readable tag associated with each container, wherein each tag includes a plurality of resonant members encoding an identification code, at least one of the resonant members having temperature-dependant characteristic; an interrogator for reading the identification code and the temperature-dependant characteristic; and a controller and associated database for monitoring the thermal history of each container.

    摘要翻译: 提供了保存在温度控制的样品存储系统中的样品的热历史(369; 699)的方法。 该系统可以包括:一个或多个容器(218,220; 522),每个容器存储样品之一; 每个容纳一个或多个容器或其他存储对象的一个​​或多个存储对象(210-216,208; 510,516-518,520; 654-660,662) 限定温度控制的存储环境并容纳所述一个或多个存储对象的一个​​或多个结构(200-206; 512; 650) 机器可读标签(14),每个标签与单独的容器和存储对象相关联,每个标签编码识别码并具有温度依赖特性; 以及用于读取识别码和温度依赖特性的询问器(12)。

    Sensor Assembly And Methods Of Adjusting The Operation Of A Sensor
    52.
    发明公开
    Sensor Assembly And Methods Of Adjusting The Operation Of A Sensor 审中-公开
    Sensoranordnung und Verfahren zum Justieren des Betriebs eines Sensors

    公开(公告)号:EP2455730A1

    公开(公告)日:2012-05-23

    申请号:EP11189220.4

    申请日:2011-11-15

    IPC分类号: G01H11/06 H01Q9/27

    摘要: A microwave sensor probe (202) includes a probe housing (208), an emitter body (300) coupled to the probe housing, and an emitter (206) coupled to the emitter body. The emitter is configured to generate an electromagnetic field from at least one microwave signal. At least one electromagnetic absorbent member (302) is configured to absorb at least one of a current transmitted through the emitter and an electromagnetic radiation generated by the emitter.

    摘要翻译: 微波传感器探针(202)包括探针壳体(208),耦合到探针壳体的发射体(300)和耦合到发射器体的发射器(206)。 发射器被配置为从至少一个微波信号产生电磁场。 至少一个电磁吸收构件(302)被配置为吸收透射通过发射器的电流和由发射器产生的电磁辐射中的至少一个。

    Methods and apparatus for high cycle fatigue life test
    54.
    发明公开
    Methods and apparatus for high cycle fatigue life test 审中-公开
    的方法和装置高循环疲劳寿命试验

    公开(公告)号:EP1158284A3

    公开(公告)日:2009-05-27

    申请号:EP01304439.1

    申请日:2001-05-21

    IPC分类号: G01H11/06

    CPC分类号: G01H11/06

    摘要: A capacitance probe (10) measures and tracks frequency and amplitude changes of a component during a high cycle fatigue portion of a life test. The probe includes an internal oscillator (14), an adjustable receiver circuit (16), a product detector (18), and a pair of gain amplifiers (40, 42). The oscillator generates a single controlled frequency output. The receiver circuit receives the frequency and creates a DC voltage shift that nulls the capacitance bridge. The product detector detects an amplitude modulated product of the oscillator and rejects (92) undesirable frequencies. gain amplifiers detect (100) a DC voltage shift and permit the capacitance effect to be easily nulled.

    ELECTRET CAPACITOR TYPE COMPOSITE SENSOR
    55.
    发明公开
    ELECTRET CAPACITOR TYPE COMPOSITE SENSOR 审中-公开
    ELEKTRETKONDENSATOR-ARTIGER VERBUNDSENSOR

    公开(公告)号:EP1990611A1

    公开(公告)日:2008-11-12

    申请号:EP07737538.4

    申请日:2007-02-28

    IPC分类号: G01D21/02 G01H11/06 H04R19/01

    摘要: To provide a small, thin and light-weighted composite sensor which can also detect light together with sound, vibration, pressure or acceleration by a single sensor.
    An electret capacitor type composite sensor is constituted by a casing 11, an electrode 12, a hole portion (which is a sound hole and also a light introduction hole) 22, a spacer 31, a vibration plate 41 having light transmissibility, a vibration plate ring 42, a printed board 6 and a semiconductor element 61. Further, a photoelectric conversion portion having a function of photoelectric effect is provided at a portion of the surface of the semiconductor element 61, light is conducted to the photoelectric conversion portion via the hole portion 22 and the vibration plate 41 having light transmissibility, and an electric signal generated by the photoelectromotive force is taken out independently from an electric signal generated by the change of the electrostatic capacitance of the electret capacitor.

    摘要翻译: 提供一个小型,薄型和轻型复合传感器,它还可以通过单个传感器检测声音,振动,压力或加速度。 驻极体电容器型复合传感器由壳体11,电极12,孔部(声孔,导光孔)22,间隔件31,透光性振动板41,振动板 环42,印刷电路板6和半导体元件61.此外,在半导体元件61的表面的一部分设置具有光电效应功能的光电转换部,通过该孔向光电转换部导通光 部分22和具有透光性的振动板41和由光电动势产生的电信号被独立于由驻极体电容器的静电电容的变化产生的电信号取出。

    PROCEDE POUR REGLER AU MOINS UN ROTOR DEFICIENT D'UN GIRAVION
    56.
    发明授权
    PROCEDE POUR REGLER AU MOINS UN ROTOR DEFICIENT D'UN GIRAVION 有权
    方法调整旋翼机的至少一个BROKEN转子

    公开(公告)号:EP1754031B1

    公开(公告)日:2008-02-06

    申请号:EP05775275.0

    申请日:2005-06-02

    申请人: EUROCOPTER

    IPC分类号: G01H1/00 G01H11/06 B64C27/00

    CPC分类号: B64C27/008

    摘要: The invention relates to a method of adjusting at least one faulty rotor of a rotorcraft, regardless of whether it is the main rotor or an anti-torque rotor. The inventive method makes use of a neural network which displays the relations between: (i) accelerations that are representative of vibrations generated on at least part of a reference rotorcraft, and (ii) adjustment parameters and defects. According to the invention, once the faulty rotor defects have been determined, an adjustment value a for at least one of the adjustment parameters is defined, advantageously minimising the following adjustment relation: formula (I).

    Acceleration sensor
    59.
    发明公开
    Acceleration sensor 审中-公开
    加速度传感器

    公开(公告)号:EP1635179A1

    公开(公告)日:2006-03-15

    申请号:EP05019509.8

    申请日:2005-09-08

    摘要: A three-axis acceleration sensor having a simple construction is provided for improving shock resistance without lowering sensor sensitivity.
    An acceleration sensor for detecting acceleration in three orthogonal directions includes an electrode substrate (5) having fixed electrodes corresponding to three axes, respectively, a diaphragm (2) having one surface thereof opposed to the fixed electrodes acting as a movable electrode, and a weight (1) mounted centrally of the other surface of the diaphragm.
    Acceleration is detected based on variations in capacitance between the fixed electrodes and diaphragm (2).
    The electrode substrate (5) has an electret layer (4) formed to cover surfaces of the fixed electrodes.

    摘要翻译: 提供一种结构简单的三轴加速度传感器,用于在不降低传感器灵敏度的情况下提高抗震性。 一种用于检测三个正交方向上的加速度的加速度传感器包括:具有分别对应于三个轴的固定电极的电极基板(5);其一个表面与充当可动电极的固定电极相对的振动膜(2) (1)安装在隔膜另一表面的中央。 根据固定电极和隔膜(2)之间的电容变化来检测加速度。 电极基板(5)具有形成为覆盖固定电极表面的驻极体层(4)。

    PROCEDE ET DISPOSITIF POUR DETECTER DES DEFAUTS D'AU MOINS UN ROTOR D'UN AERONEF A VOILURE TOURNANTE
    60.
    发明公开
    PROCEDE ET DISPOSITIF POUR DETECTER DES DEFAUTS D'AU MOINS UN ROTOR D'UN AERONEF A VOILURE TOURNANTE 有权
    方法和设备,在一个飞行物体与旋转式机翼至少一个转子错误检测

    公开(公告)号:EP1485685A1

    公开(公告)日:2004-12-15

    申请号:EP02738244.9

    申请日:2002-05-15

    申请人: EUROCOPTER

    发明人: FERRER, Rogelio

    IPC分类号: G01H1/00 G01H11/06 B64C27/02

    摘要: The invention concerns a method and a device for detecting defects in at least one rotor of a rotary wing aircraft, in particular of a helicopter, and for adjusting said rotor. The method is characterized in that it consists, in a preliminary step, in using a reference aircraft corresponding to a particular type of aircraft, whereof the rotor (6, 10) is defect-free and is adjusted such that the vibratory level is minimal, in performing a series of measurements on the aircraft (1) and deducing therefrom a neural network illustrating the relationships between accelerations representing vibrations, and setting defects and parameters. Then, in a subsequent step, for a particular aircraft (1) of said similar type, in performing measurements on said particular aircraft (1), based on said measurements and on the neural network, in detecting possible defects and determining the values of setting parameters, which enable the vibratory level of the aircraft (1) to be reduced to a minimum, and applying them to the rotor (6, 10).

    摘要翻译: 一种用于检测旋转翼飞机的至少一个转子,尤其是直升机的缺陷,以调节转子的方法和装置。 在该方法中,在预备步骤中,一个参考飞行器被用于对应于特定类型的飞机和具有转子(6,10),而不缺损等调整,振动的DASS裸片级为最小,一系列的测量是 所采取的飞行器(1)上,和一个神经网络是从举例说明代表accelleration振动,和缺陷,和调整参数之间的关系推断出存在。 有后,在后面的步骤中,对于相同类型的一个特定的航空器(1),测量所采取的特定飞行器(1)上和所述测量的基础上和神经网络中,缺陷,如果任何的基础上 中,检测和用于调整参数的值是确定的开采thatwill使飞行器(1)的振动的电平最小化,哪些参数是施加到所述转子(6,10)。