METHOD TO CONTROL BYPASS OF AIR IN COMPRESSOR OF TWO-SHAFT BY-PASS GAS-TURBINE ENGINE

FIELD: mechanical engineering; gas-turbine engines. SUBSTANCE: invention provides faultless surgeless operation of engine owing to by-passing of air from inner circuit of engine into outer circuit in of mismatching of programmed and actual angles of positions of vanes of compressor inlet guide vane...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	KNJAZEVA N.R, SAZHENKOV A.N, TRUBNIKOV JU.A, SAVENKOV JU.S
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	BLASTING HEATING LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS WEAPONS
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Beschreibung
Zusammenfassung:	FIELD: mechanical engineering; gas-turbine engines. SUBSTANCE: invention provides faultless surgeless operation of engine owing to by-passing of air from inner circuit of engine into outer circuit in of mismatching of programmed and actual angles of positions of vanes of compressor inlet guide vane assembly exceeding maximum tolerable value. For this purpose actual angle of position of vanes of compressor inlet guide vane assembly alphaigais compared with corresponding programmed value alphaprogiga and value of mismatch Deltaalphaiga = alphaprogiga-alphaiga is determined, after which value Deltaalphaiga is compared with limited tolerable value Deltaalphalimiga and if Deltaalphaiga>Deltaalphalimiga, signal l6 is formed to open air bypass valves and command to open air bypass valves is sent signal l6 is received, irrespective of presence of signal l5. EFFECT: provision of trouble-free operation without surges. 7 cl, 1 dwg