FIELD: engines and pumps.
SUBSTANCE: there is a way of target value adjustment of at least one parameter that affect on a draft of a gas-turbine engine that sets in motion an air vehicle during the air vehicle flight stage. It comprises: a stage at which one obtains a current value of at least one engine target variable, a stage at which one derives a decrement value for the at least one noted parameter from the predetermined table; the noted parameter is connected with the current value of at a minimum one mentioned engine target variable. The method also comprises a stage at which one regulates target value of at least one noted parameter by virtue of applying the decrement value to this parameter. The decrement value is derived from the table. Besides, the appliance for the gas-turbine engine draft control is presented. It sets in motion an air vehicle during the flight stage. The appliance also regulates the target value for at least one parameter that affect on the noted draft which is regulated with the aid of the claimed adjustment method.
EFFECT: invention allows to reduce the air vehicle draft by simultaneous numerous target values adjustment without being limited to one particular engine type.
9 cl, 4 dwg
Title |
Year |
Author |
Number |
METHOD AND DEVICE FOR DETECTING CONDITIONS CONDUCIVE TO OCCURRENCE OF SURGING TO PROTECT COMPRESSOR OF AIRCRAFT GAS TURBINE ENGINE |
2018 |
- Eburderie, Emmanuel, Mickael
|
RU2764225C2 |
METHOD TO CONTROL AIRCRAFT TURBOJET ENGINE THRUST DISTURBANCE |
2013 |
|
RU2638417C2 |
HYBRIDISATION OF TURBOJET ENGINE COMPRESSORS |
2015 |
- Robic, Bernard
- Obrecht, Thierry, Jean-Jacques
- Renault, Baptiste, Jean, Marie
|
RU2708492C2 |
METHOD FOR AUTOMATIC PROTECTION OF A GAS TURBINE ENGINE AGAINST SURGE |
2022 |
- Sazhenkov Aleksei Nikolaevich
- Savenkov Iurii Semenovich
|
RU2789806C1 |
METHOD AND DEVICE FOR GENERATING FUEL FLOW RATE COMMAND FOR INJECTING TO COMBUSTION CHAMBER OF TURBINE ENGINE |
2014 |
|
RU2654552C2 |
CONTROL METHOD OF GAS TURBINE ENGINE REVERSING DEVICE DURING AIRCRAFT LANDING AND INTERRUPTED TAKEOFF |
2019 |
- Savenkov Yurij Semenovich
- Sazhenkov Aleksej Nikolaevich
|
RU2730731C1 |
METHOD FOR PROTECTING A GAS TURBINE ENGINE FROM COMPRESSOR SURGE |
2023 |
- Sazhenkov Aleksej Nikolaevich
- Savenkov Yurij Semenovich
- Yakushev Aleksej Pavlovich
|
RU2801768C1 |
METHOD FOR CONTROL OF ELECTRICITY GENERATION, USED FOR AIRCRAFT GAS TURBINE, AND APPARATUS FOR APPLYING SAID METHOD |
2011 |
|
RU2598476C2 |
LP SPOOL POWER TAKE-OFF AND DEBRIS REMOVAL SYSTEM |
2020 |
- De Blois, Nicolas, Bertrand, Georges
- Dupays, Clement
|
RU2795890C2 |
METHOD FOR RENDERING ASSISTANCE TO PILOT OF SINGLE-ENGINE ROTARY-WING AIRCRAFT IN AUTOROTATION MODE |
2013 |
- Konnol'T Matt'E
- Mers'E Kristian
- Mariotto Dam'En
|
RU2556055C2 |