FIELD: aircraft engineering.
SUBSTANCE: proposed process consists in adjustment of compressor distributor angles setting For this two or more compressor distributor angles setting adjustment programs are generated depending on compressor rpm For each said programs measured are thrust and fuel flow rate to define adjustment program of minimum flow rate for a given thrust range Changeover of programs in engine controller proceeds subject to flight mode.
EFFECT: fuel saving, increased range and time in flight.
2 dwg, 1 tbl
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