FIELD: control of gas turbine engines. SUBSTANCE: signal inducting that high-pressure rotor has gained speed at which acceleration control unit starts functioning is shaped; upon the arrival of this signal gas flow from high-pressure turbine is shut off up to the moment of engine running at low gas condition and gas flow from low-pressure turbine is admitted. EFFECT: improved reliability of control. 4 dwg
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Authors
Dates
1994-05-30—Published
1991-03-04—Filed