FIELD: engine building.
SUBSTANCE: group of inventions relates to a method for the control of fuel supply to a combustion chamber of a gas turbine engine, a fuel supply circuit and a gas turbine engine. The method for the control of fuel injection of a gas turbine engine is carried out using fuel supply circuit (100). In this case, fuel supply circuit (100) contains pre-injection line (141) and main injection line (142). During the supply distribution transition between pre-injection line (141) and main injection line (142), the method includes following stages: a) determination of at least the minimum value to be maintained relatively to the pressure value; b) determination of at least one hydraulic value of the fuel supply circuit; c) based on the determined hydraulic value in the fuel supply circuit, the calculated value of the fuel supply distribution corresponding to the minimum value to be maintained is calculated; and the fuel supply distribution is switched to the calculated value of the fuel supply distribution.
EFFECT: obtaining a method for the control of fuel supply to a combustion chamber of a gas turbine engine.
12 cl, 9 dwg
Title | Year | Author | Number |
---|---|---|---|
GAS-TURBINE FUEL DELIVERY CONTROL METHOD | 2006 |
|
RU2322601C1 |
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GAS-TURBINE ENGINE FUEL-FEED CONTROL METHOD | 1997 |
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|
RU2786969C1 |
Authors
Dates
2022-06-06—Published
2018-12-21—Filed