FIELD: engines and pumps.
SUBSTANCE: jet-turbine engine includes a high-pressure housing, a low-pressure housing, a nacelle and an electric generator. The low-pressure housing brings into rotation the fan located in a fixed casing being a part of the nacelle. Electric generator is located in the fan and takes power from it. Electric generator includes a rotor built into a fan and includes constant magnets fixed on the fan blades. Besides, the electric generator includes a stator built into the fan casing and a deflector installed in the fan casing for cooling of the above stator.
EFFECT: possibility of avoiding problems with operation of an engine in an idle mode and conversion of mechanical power to electric power with increased efficiency; simpler plant and maintenance of an electric generator.
Title |
Year |
Author |
Number |
TURBINE MACHINE WITH BUILT-IN STARTER-GENERATOR |
2003 |
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|
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METHOD AND SYSTEM FOR ADJUSTMENT OF CLEARANCE AT TURBINE ROTOR BLADE EDGES |
2011 |
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- Denes Frank Rozhe Deni
- Golli Brjuno Rober
|
RU2566510C2 |
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2005 |
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|
RU2424435C2 |
TURBOJET COMPRISING CURRENT GENERATOR MOUNTED IN ENGINE FAN AND METHOD OF INSTALLING SAID GENERATOR IN SAID FAN |
2008 |
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|
RU2485328C2 |
HELICAL FAN AVIATION ENGINE |
2007 |
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|
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STATOR OF AIRCRAFT GAS TURBINE ENGINE AND AIRCRAFT GAS TURBINE ENGINE |
2015 |
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|
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2017 |
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|
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|
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PROPULSION UNIT OF AIRCRAFT, AND AIRCRAFT DRIVEN BY SUCH A PROPULSION UNIT BUILT IN REAR PART OF FUSELAGE OF AIRCRAFT |
2019 |
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|
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COMBUSTION CHAMBER FOR TURBOJET THREE-CIRCUIT ENGINE WITH TWO HIGH PRESSURE TURBINES |
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|
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