AIR DATA PROBE WITH OPTICAL PRESSURE INTEGRATION

An air data probe (12a-12n) includes a probe head (14, 26, 42, 64), a port (20, 22, 30, 48, 68) within the probe head (14, 26, 42, 64) in fluid communication with external airflow (A), and a pneumatic pressure sensor (28, 44, 66) mounted within the port (20...68).

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Bibliographische Detailangaben
Hauptverfasser:	MILLER, Mark Sherwood, SEIDEL, Greg Allen, CHILDRESS, Kimiko, NESNIDAL, Michael Paul
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT MEASURING MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUIDLEVEL METERING BY VOLUME PARACHUTES PERFORMING OPERATIONS PHYSICS TESTING TRANSPORTING
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Beschreibung
Zusammenfassung:	An air data probe (12a-12n) includes a probe head (14, 26, 42, 64), a port (20, 22, 30, 48, 68) within the probe head (14, 26, 42, 64) in fluid communication with external airflow (A), and a pneumatic pressure sensor (28, 44, 66) mounted within the port (20...68).