FIELD: energy.
SUBSTANCE: invention relates to power engineering. Method of turbo unit starting containing a gas turbine engine including at least one rotor and starter configured to drive the rotor rotation, is executed by an electronic module. Proposed method comprises: stage of obtaining instruction to start the turbo unit and start in response to receiving this instruction; stage of primary acceleration, when starter works to increase the rotor rotation speed; stage of heat homogenization, when starter works to maintain constant rotor rotation speed or reduce it untill specified conditions are satisfied; after specified conditions are satisfied secondary acceleration stage takes place, when starter works to increase rotor rotation speed; and stage of ignition E6) when an instruction for engine ignition is recieved.
EFFECT: invention allows to increase turbo unit start efficiency.
8 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD AND SYSTEM OF STARTING A GAS TURBINE ENGINE OF AN AIRCRAFT | 2013 |
|
RU2646521C2 |
| METHOD FOR MANAGING GAS TURBINE ASSEMBLY AT LOW SPEED ROTATION | 2015 |
|
RU2668299C2 |
| METHOD AND DEVICE FOR DETECTING CONDITIONS CONDUCIVE TO OCCURRENCE OF SURGING TO PROTECT COMPRESSOR OF AIRCRAFT GAS TURBINE ENGINE | 2018 |
|
RU2764225C2 |
| DEVICE AND METHOD FOR STARTING ENGINE OF MILD HYBRID VEHICLE | 2015 |
|
RU2670581C2 |
| COOLANT FLOW RATE CONTROL | 2009 |
|
RU2503831C2 |
| METHOD OF IMPROVED OPERATION OF THE ENGINE FOR ISG VEHICLE | 2015 |
|
RU2677636C2 |
| OPERATION OF VEHICLE WITH HYBRID DRIVE (VERSIONS) | 2014 |
|
RU2581993C2 |
| GAS TURBINE ENGINE STARTER-GENERATOR AND METHOD OF ITS CONTROL | 2010 |
|
RU2528950C2 |
| SYSTEM AND METHOD FOR VEHICLE DRIVING STYLE | 2010 |
|
RU2549598C2 |
| METHOD OF GAS TURBINE ENGINE START-UP | 2011 |
|
RU2467192C1 |
