HULL-MOUNTED IMPACT PRESSURE TUBE

Since, as a rule, there are several such PSTs on an aircraft, this results in a marked reduction in weight and aerodynamic drag, and savings in the required electric power in conjunction with a simultaneous increase in the accuracy of measurement of the angle of attack. All this permits a substantia...

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Bibliographische Detailangaben
Hauptverfasser:	EFREMOV ANDREI ALEKSANDROVICH, KOEHLER HEINZ-GERHARD, GUSKOV VALENTIN IVANOVICH, GOLOVKIN MIKHAIL ALEKSEEVICH, GOLOVKIN VLADIMIR ALEKSEEVICH, VOZHDAEV YEVGENY SEMENOVICH, NIKOLSKY ALEKSANDR ALEKSANDROVICH
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT MEASURING MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER,MECHANICAL EFFICIENCY, OR FLUID PRESSURE MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION,OR SHOCK PERFORMING OPERATIONS PHYSICS TESTING TRANSPORTING
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Beschreibung
Zusammenfassung:	Since, as a rule, there are several such PSTs on an aircraft, this results in a marked reduction in weight and aerodynamic drag, and savings in the required electric power in conjunction with a simultaneous increase in the accuracy of measurement of the angle of attack. All this permits a substantial increase in the competitiveness of the proposed fuselage Pitot-static tube.