FIELD: mechanical engineering; engine.
SUBSTANCE: invention relates to drive of auxiliary equipment, such as fuel pump or oil pump in gas-turbine engine. Proposed drive contains electric motor and air turbine 22 coupled with electric motor. Said air turbine is designed to supply gas-turbine engine with air flow from compressor and it takes part in setting indicated auxiliary equipment into operation. Drive contains also flow rate control valve of air taken from compressor, said valve being closed at starting phase of gas-turbine engine.
EFFECT: reliability of drive.
11 cl, 9 dwg
Title | Year | Author | Number |
---|---|---|---|
TURBINE MACHINE WITH BUILT-IN STARTER-GENERATOR | 2003 |
|
RU2321755C2 |
TURBOGENERATOR | 2006 |
|
RU2323344C1 |
TURBINE GENERATOR | 2023 |
|
RU2821119C1 |
AIRCRAFT PROPFAN ENGINE | 2007 |
|
RU2379523C2 |
LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE | 2016 |
|
RU2614709C1 |
DESIGN OF A CROSS-FLOW DIGITALLY CONTROLLED GAS TURBINE ENGINE | 2022 |
|
RU2784789C1 |
HELICAL FAN AVIATION GAS-TURBINE ENGINE | 2007 |
|
RU2358138C1 |
IMPROVED METHOD OF TURBINE COMPRESSOR CHARACTERISTICS | 2017 |
|
RU2741172C2 |
LOW-PRESSURE COMPRESSOR OF GAS TURBINE ENGINE OF AVIATION TYPE | 2016 |
|
RU2614708C1 |
BIROTATING COMPRESSOR | 2016 |
|
RU2614421C1 |
Authors
Dates
2008-04-10—Published
2003-07-15—Filed