FIELD: mechanical engineering; engines. SUBSTANCE: proposed double-flow gas turbofan engine contains fan, high-speed compressor, combustion chamber, two-stage turbine setting compressor and fan into rotation, reaction nozzle and steam-water heater (steam generator). Engine is furnished also with air-hydrogen-nitrogen-oxygen heat-mass exchanger, reheat unit and multiplicator. Fan is made coaxial, double-row, sixteen-blade, variable pitch, with diameter of 3-3.4 m. Two-stage turbine is of combination impulse-reaction type, with de Laval nozzle fitted at its outlet. Higher-speed compressor is made with pressure ratio of Pc = 40, and speed of 6000-7600 rpm. Thrust of engine is 100 ton, air flow rate through first contour being 400 kg/s and through second contour, 1000 kg/s and gas temperature before turbine equal to 1800 K. EFFECT: increased efficiency of engine. 8 cl
Title |
Year |
Author |
Number |
GAS-TURBINE TURBOFAN ENGINE |
2003 |
- Agafonov Jurij Mikhajlovich
- Brusov Vladimir Alekseevich
- Brusova Tat'Jana Sergeevna
- Agafonov Nikolaj Jur'Evich
- Ablaeva Ekaterina Jakovlevna
- Balymov Aleksandr Fedorovich
- Bobrov Rauf Kajumovich
- Belomestnov Ehduard Nikolaevich
- Burlakov Lev Ivanovich
- Bogdanov Aleksandr Ivanovich
- Velikanova Nina Petrovna
- Golushchenko Anatolij Romanovich
- Zakiev Farit Kavievich
- Zazerskij Vladimir Dmitrievich
- Kadyrov Raif Jasaveevich
- Kornaukhov Aleksandr Anatol'Evich
- Kolomytseva Elena Evgen'Evna
- Kuznetsov Nikolaj Il'Ich
- Kozhin Viktor Georgievich
- Larjukhin Sergej Anatol'Evich
- Lysova Valentina Petrovna
- Margulis Stanislav Gershevich
- Mal'Tseva Tat'Jana Ivanovna
- Miftakhov Il'Giz Insarovich
- Mokshanov Aleksandr Pavlovich
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- Simkin Ehduard L'Vovich
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- Khamitov Rafaehl' Makhmutovich
- Il'Jushkin Vasilij Vasil'Evich
- Korobova Nadezhda Vasil'Evna
- Tonkikh Svetlana Jur'Evna
|
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2006 |
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|
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