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公开(公告)号：US06419186B1
公开(公告)日：2002-07-16
申请号：US09540142
申请日：2000-03-31
申请人： Thomas J. Bachinski , Timothy T. Golly , Robert G. Syring, Jr. , Ronald J. Petri , Douglas G. Conley
发明人： Thomas J. Bachinski , Timothy T. Golly , Robert G. Syring, Jr. , Ronald J. Petri , Douglas G. Conley
IPC分类号： B64C2700
CPC分类号： B64D43/02 , G01P5/165 , G01P13/025
摘要： A standoff arm and probe assembly for a helicopter has a standoff mounting arm that extends outwardly from the helicopter body in a selected direction, preferably forwardly. The standoff arm has an outer end that mounts a low lateral speed sensing probe that is positioned with an axis substantially parallel to the axis of a helicopter rotor, and within the downwash region of air movement causes by the rotor. The low lateral speed sensing probe has ports that are arranged annularly around the probe, and the pressures sensed at selected annular or peripheral locations on the probe are measured to determine low air speeds. Additionally, the standoff arm can mount a plurality of other sensors such as a pitot pressure probe extending forwardly from the arm, a lateral pressure sensing probe along a lateral side of the arm, and the arm can mount outside air temperature sensors, ice detectors, and total air temperature sensors, if desired.
摘要翻译： 用于直升机的支座臂和探针组件具有支架安装臂，该支架安装臂从直升机主体沿所选方向向外延伸，优选地向前延伸。 支架臂具有一个外端，该外端安装一个低侧速度传感探头，该探头的基本上平行于直升机转子轴线的轴线定位，并且在由转子引起的空气运动的下降区域内。 低横向速度感测探头具有围绕探针环形布置的端口，并且测量在探针上的选定环形或周边位置处感测到的压力以确定低空气速度。 此外，支架臂可以安装多个其它传感器，例如从臂向前延伸的皮托管压力探头，沿着臂的横向侧的侧向压力传感探头，并且臂可以安装在室外空气温度传感器，冰探测器， 和空气温度传感器。
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公开(公告)号：US06612166B2
公开(公告)日：2003-09-02
申请号：US10020839
申请日：2001-12-13
IPC分类号： G01P1300
CPC分类号： G01P13/025 , B64D43/02 , F16F9/535
摘要： An angle of attack sensor has a vane mounted on a rotating shaft that rotates in response to angle of attack. The shaft has a rotor at one end which is in a chamber in a housing supporting the shaft. The chamber includes a space around the rotor filled with either an electrorheological or magnetorheological fluid. A controller is used to provide an electrical signal, such as a signal controlling an electromagnet, to change the magnetic field affecting the fluid in response to various aircraft parameters to thereby control the viscosity of the electrorheological or magnetorheological fluid in the chamber and control the amount of damping of the rotating vane.
摘要翻译： 攻角传感器具有安装在旋转轴上的叶片，该旋转轴响应于迎角而旋转。 轴在一端处具有转子，该转子位于支撑轴的壳体中的室中。 该腔室包括一个充满电流变流体或磁流变流体的转子周围的空间。 控制器用于提供诸如控制电磁体的信号的电信号，以响应于各种飞行器参数改变影响流体的磁场，从而控制室内电流变或磁流变流体的粘度，并控制量 的旋转叶片的阻尼。
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公开(公告)号：USD463989S1
公开(公告)日：2002-10-08
申请号：US29141338
申请日：2001-05-03
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公开(公告)号：US06550344B2
公开(公告)日：2003-04-22
申请号：US09849271
申请日：2001-05-04
IPC分类号： G01P518
CPC分类号： G01P5/16 , G01P5/165 , G01P13/025
摘要： A semi-flush air data sensing probe is formed as an elongated bubble housing directly supported on an aircraft surface having a generally longitudinally extending rounded outer edge surface with a rounded contoured leading end. The housing has top and bottom wall surfaces extending from the supporting surface to the rounded outer surface. The trailing end of the housing is smaller than the leading end and is contoured to provide for smooth airflow past the housing. A central longitudinally extending plane that bisects the housing and which is perpendicular to the supporting surface, forms a reference. A forwardly facing port is at the leading end and centered on the central plane, and a pair of angle of attack sensing ports are on the leading end and are symmetrically located on opposite sides of the longitudinally extending plane. A static pressure sensing port also is provided on the housing at a position along the rounded outer edge surface and spaced downstream from the leading end.
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公开(公告)号：US08365591B2
公开(公告)日：2013-02-05
申请号：US12946192
申请日：2010-11-15
申请人： Timothy T. Golly
发明人： Timothy T. Golly
IPC分类号： A63B53/00
CPC分类号： G01P5/14 , G01P5/165 , G01P13/025
摘要： A static port apparatus for an aircraft having a static plate having inner and outer surfaces for fixture on the aircraft. The static plate including a first set of a plurality of port apertures and at least a second set of a plurality of port apertures. Each port aperture of the second set of port apertures is coaxially positioned with respect to each port aperture of the first set of port apertures.
摘要翻译： 一种用于飞行器的静态端口装置，具有具有用于飞机上的固定装置的内表面和外表面的静态板。 静态板包括第一组多个端口孔和至少第二组多个端口孔。 第二组端口孔的每个端口孔相对于第一组端口孔的每个端口孔同轴定位。
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公开(公告)号：US20120123704A1
公开(公告)日：2012-05-17
申请号：US12946359
申请日：2010-11-15
申请人： Timothy T. Golly , Jason Debo
发明人： Timothy T. Golly , Jason Debo
IPC分类号： G06F19/00
CPC分类号： G01P13/025 , G01P5/165 , G01P21/025
摘要： An avionics system and process for detecting pneumatic blockages having an air pressure measurement system including a first sensor positioned in association with the air inlet of an air probe component. The air pressure measurement system having a second sensor positioned in association with the air inlet for detecting air pressure in which the second sensor has a frequency response higher than that of the first sensor. An air data computer is coupled to each of the first and second sensors being configured and operable to calculate a first aircraft movement measurement using detected air pressure from the first sensor and is further operative to determine if the first sensor is faulty or if the air inlet is blocked in dependence upon the frequency content and amplitude of the output from the second sensor.
摘要翻译： 一种用于检测气动堵塞的航空电子系统和过程，其具有包括与空气探针部件的空气入口相关联的第一传感器的空气压力测量系统。 空气压力测量系统具有与进气口相关联的第二传感器，用于检测第二传感器的频率响应高于第一传感器的频率响应。 空气数据计算机耦合到第一和第二传感器中的每一个，其被配置和可操作以使用来自第一传感器的检测到的空气压力来计算第一飞行器运动测量，并进一步操作以确定第一传感器是否有故障，或者如果空气入口 根据来自第二传感器的输出的频率内容和振幅被阻挡。
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公开(公告)号：US08718955B2
公开(公告)日：2014-05-06
申请号：US12946359
申请日：2010-11-15
申请人： Timothy T. Golly , Jason Debo
发明人： Timothy T. Golly , Jason Debo
IPC分类号： G01L7/00
CPC分类号： G01P13/025 , G01P5/165 , G01P21/025
摘要： An avionics system and process for detecting pneumatic blockages having an air pressure measurement system including a first sensor positioned in association with the air inlet of an air probe component. The air pressure measurement system having a second sensor positioned in association with the air inlet for detecting air pressure in which the second sensor has a frequency response higher than that of the first sensor. An air data computer is coupled to each of the first and second sensors being configured and operable to calculate a first aircraft movement measurement using detected air pressure from the first sensor and is further operative to determine if the first sensor is faulty or if the air inlet is blocked in dependence upon the frequency content and amplitude of the output from the second sensor.
摘要翻译： 一种用于检测气动堵塞的航空电子系统和过程，其具有包括与空气探针部件的空气入口相关联的第一传感器的空气压力测量系统。 空气压力测量系统具有与进气口相关联的第二传感器，用于检测第二传感器的频率响应高于第一传感器的频率响应。 空气数据计算机耦合到第一和第二传感器中的每一个，其被配置和可操作以使用来自第一传感器的检测到的空气压力来计算第一飞行器运动测量，并进一步操作以确定第一传感器是否有故障，或者如果空气入口 根据来自第二传感器的输出的频率内容和振幅被阻挡。
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公开(公告)号：US08272261B2
公开(公告)日：2012-09-25
申请号：US12946192
申请日：2010-11-15
申请人： Timothy T. Golly
发明人： Timothy T. Golly
IPC分类号： A63B53/00
摘要： A static port apparatus for an aircraft having a static plate having inner and outer surfaces for fixture on the aircraft. The static plate including a first set of a plurality of port apertures and at least a second set of a plurality of port apertures. Each port aperture of the second set of port apertures is coaxially positioned with respect to each port aperture of the first set of port apertures.
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公开(公告)号：US20120118075A1
公开(公告)日：2012-05-17
申请号：US12946192
申请日：2010-11-15
申请人： Timothy T. Golly
发明人： Timothy T. Golly
IPC分类号： G01F1/34
CPC分类号： G01P5/14 , G01P5/165 , G01P13/025
摘要： A static port apparatus for an aircraft having a static plate having inner and outer surfaces for fixture on the aircraft. The static plate including a first set of a plurality of port apertures and at least a second set of a plurality of port apertures. Each port aperture of the second set of port apertures is coaxially positioned with respect to each port aperture of the first set of port apertures.
摘要翻译： 一种用于飞行器的静态端口装置，具有具有用于飞机上的固定装置的内表面和外表面的静态板。 静态板包括第一组多个端口孔和至少第二组多个端口孔。 第二组端口孔的每个端口孔相对于第一组端口孔的每个端口孔同轴定位。
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