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公开(公告)号：US3677086A
公开(公告)日：1972-07-18
申请号：US3677086D
申请日：1970-06-10
Applicant: SUNDSTRAND DATA CONTROL
Inventor： COREY VICTOR B
CPC classification number: G01P13/025 , F15C1/005 , G01F1/203 , G01P5/005 , Y10T137/2202
Abstract: An apparatus for determining a characteristic, as velocity or direction, of a fluid flow stream. Fluid sensors generate signals which are differentially compared to produce an error signal representative of the amount of movement, for the sensors or for a fluid stream generator, which is necessary to null the system. A servomechanism produces the nulling movement in response to the error signal. The amount of movement also generates a positional signal indicating the low frequency component or steady state characteristic of the fluid flow stream. A signal adder combines the positional signal with the error signal, containing a high frequency component, to provide an indication of the instantaneous fluid characteristic.
Abstract translation: 一种用于确定流体流动流的特性（如速度或方向）的装置。 流体传感器产生差分比较的信号，产生代表运动量的误差信号，传感器或流体流发生器，这是使系统失效所必需的。 伺服机构响应于误差信号产生归零运动。 移动量还产生指示流体流动流的低频分量或稳态特性的位置信号。 信号加法器将位置信号与包含高频分量的误差信号组合，以提供瞬时流体特性的指示。
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公开(公告)号：US3678746A
公开(公告)日：1972-07-25
申请号：US3678746D
申请日：1970-06-10
Applicant: SUNDSTRAND DATA CONTROL
Inventor： COREY VICTOR B
CPC classification number: G01F1/203 , G01P5/005 , Y10T137/2202
Abstract: A method and apparatus for determining the velocity of a fluid flow stream. A fluid jet source is disposed opposite a pair of fluid pressure detectors so that the jet stream equally intersects both detectors when the velocity of the fluid flow stream is zero. Means are provided for relatively laterally displacing the jet with respect to the detectors, and for sensing the pressure difference at the detectors, in order to indicate the velocity of the moving fluid flow stream.
Abstract translation: 一种用于确定流体流动流速度的方法和装置。 流体喷射源与一对流体压力检测器相对设置，使得当流体流动流的速度为零时，喷射流与两个检测器相等。 提供了用于相对于检测器相对地横向移位射流的装置，并且用于感测检测器处的压力差，以便指示运动流体流动流的速度。
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公开(公告)号：US3630169A
公开(公告)日：1971-12-28
申请号：US3630169D
申请日：1970-06-01
Applicant: SUNDSTRAND DATA CONTROL
Inventor： COREY VICTOR B
CPC classification number: B64D43/02
Abstract: A stall warning indicator having no moving parts is mounted on a leading edge of an aircraft wing, near the point of stagnation of airflow when a stall condition occurs. The indicator includes a transmitter emitting transmissions, as a continuous acoustic wave or a jet airstream, which are received by a pair of detectors connected to a differential sensor. When the stagnation point passes the axis of the transmissions, the differential sensor produces a signal to warn of an impending stall.
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