METHOD FOR MONITORING THE THRUST OF AN AIRCRAFT MICROJET

The proposed method for monitoring the thrust of an aircraft microjet consists in measuring the thrust, inlet gas pressure, outlet gas pressure, and inlet gas temperature at the jet nozzle at different gas pressures, including the rated pressure, in testing the jet at a stand, and determining the ch...

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Bibliographische Detailangaben
Hauptverfasser:	DUPLISCHEVA OLGA MYKHAILIVNA, PORUBAIMEKH VOLODYMYR ILLICH, DEMCHENKO SERHII ANDRIIOVYCH
Format:	Patent
Sprache:	eng
Schlagworte:	MEASURING MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER,MECHANICAL EFFICIENCY, OR FLUID PRESSURE PHYSICS TESTING
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Beschreibung
Zusammenfassung:	The proposed method for monitoring the thrust of an aircraft microjet consists in measuring the thrust, inlet gas pressure, outlet gas pressure, and inlet gas temperature at the jet nozzle at different gas pressures, including the rated pressure, in testing the jet at a stand, and determining the characteristics that define the dependence of the jet thrust on the inlet gas temperature and the inlet and outlet gas pressure at the jet nozzle. The obtained characteristics are used for determining the thrust of the jet installed at an aircraft by the data on gas temperature and pressure. The present invention provides a possibility to monitor the thrust of a microjet installed at an aircraft by the data obtained in measuring the performance parameters of the jet.