IMPROVED METHOD AND APPARATUS FOR DETECTING CLEAR AIR TURBULENCES
    1.
    发明申请
    IMPROVED METHOD AND APPARATUS FOR DETECTING CLEAR AIR TURBULENCES 审中-公开
    用于检测清除空气涡轮的改进方法和装置

    公开(公告)号:WO1980000877A1

    公开(公告)日:1980-05-01

    申请号:PCT/US1979000882

    申请日:1979-10-12

    CPC classification number: G01W1/00 G01J5/602 G01W2001/003

    Abstract: An improved clear air turbulence (CAT) detector (100) sensing infrared radiation in the 27-33 micrometer range of the water vapor rotational wavelength band. The improved clear air turbulence detector (100) for use on an aircraft includes a forward looking and upwardly oriented between 8 to 12 optical assembly (300) having a thallium bromoiodide infrared lens (410), a 27-33 micrometer wavelength interference filter (420) and an infrared detector (430); a radiometer amplifier (320) for amplifying the output of the optical assembly (300) and for generating an analog voltage signal (330) related to the received infrared intensity, a processing unit (340) for analyzing the analog signal, and a display unit (360) for generating a first signal (370) when no clear air turbulence is detected, a second signal (380) when a moderate turbulence is detected, and a third signal (390) when extreme turbulence is detected. A method for determining the advance time for entering the clear air turbulence after detection is based upon the altitude of the aircraft.

    Abstract translation: 改进的清澈空气湍流(CAT)检测器,检测水蒸汽旋转波段的27-33微米范围内的红外辐射。 用于飞行器的改进的透明空气湍流探测器包括前视和向上定向在8°至12°光学组件之间,其具有铊溴碘化物红外透镜,27-33微米波长干涉滤光器和红外检测器; 辐射计放大器,用于放大光学组件的输出并产生与接收到的红外线强度相关的模拟电压信号;处理单元,用于分析模拟信号;以及显示单元,用于当没有检测到清晰的空气湍流时产生第一信号 ,当检测到中等湍流时的第二信号,以及当检测到极度​​湍流时的第三信号。 用于确定在检测之后进入清澈空气湍流的提前时间的方法基于飞行器的高度。

    AIR TURBULENCE DETECTION
    2.
    发明申请
    AIR TURBULENCE DETECTION 审中-公开
    空气湍流检测

    公开(公告)号:WO1990010203A1

    公开(公告)日:1990-09-07

    申请号:PCT/US1990000976

    申请日:1990-02-20

    CPC classification number: G01J5/602 G01J5/0014 G01J5/601 G01W2001/003

    Abstract: Air turbulence (windshear as well as clear air turbulence) in navigable airspace is detected by remotely sensing changes in the spatial temperature profile of an air column ahead of an aircraft by repeatedly sensing the intensity of the thermal radiation from the column of atmospheric air in at least two spectral peaks in the 4.17 to 4.2 νm region of the CO2 spectral emission band, and comparing the relative intensity of the spectral peaks over time. Apparatus which includes a tunable Fabry-Perot etalon is provided for the practice of the method.

    Abstract translation: 通过远程检测飞机前方的空气塔的空间温度曲线的变化来检测航行空域中的空气湍流(风切变以及清澈的空气湍流),通过反复感测来自大气中的热源的热辐射的强度 在二氧化碳光谱发射带的4.17至4.2μm的区域内至少有两个光谱峰,并比较光谱峰随时间的相对强度。 提供了包括可调法布里 - 珀罗标准具的装置,用于实施该方法。

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