SYSTEM AND COMPUTER-READABLE STORAGE MEDIUM FOR VARIABLE ALIGNMENT AERODYNAMIC PROBES

A variable alignment aerodynamic probe (200; 300; 400) may comprise a probe body (218; 318; 402) having a leading edge (230) and extending radially into a vane case (202), a sensor element proximate the leading edge, and a bearing (224) coupled to the probe body (218; 318; 402) and the vane case (20...

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Bibliographische Detailangaben
Hauptverfasser:	SWAGGER, Adam, BOUDREAU, Daniel J, WARREN, Eli Cole, SMITH, Ryan C, HACKETT, Bryan J
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT LIGHTING MEASURING MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER,MECHANICAL EFFICIENCY, OR FLUID PRESSURE MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUIDLEVEL MECHANICAL ENGINEERING METERING BY VOLUME PHYSICS TESTING WEAPONS
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Beschreibung
Zusammenfassung:	A variable alignment aerodynamic probe (200; 300; 400) may comprise a probe body (218; 318; 402) having a leading edge (230) and extending radially into a vane case (202), a sensor element proximate the leading edge, and a bearing (224) coupled to the probe body (218; 318; 402) and the vane case (202). The probe body (218; 318; 402) may be configured to rotate in response to a turned flow within the vane case (202). The rotation of the probe body (218; 318; 402) may be configured to maintain an angle of attack of the leading edge (230) with respect to the turned flow between 0° and 15°.