AIR-JET ENGINE Russian patent published in 2007 - IPC F02K3/02 

Abstract RU 2305200 C2

FIELD: aircraft industry.

SUBSTANCE: proposed air-jet engine has turbocompressor part with compressor, combustion chamber and turbine, chamber arranged before exit nozzle having at least one port gates installed for movement relative to port, thus forming channel communicating with chamber to provide getting of atmospheric air. Engine is furnished also with nozzle assembly installed after turbine and before chamber, made for rotation around its axis and provided with at least two inner channels. Each inner channel hydraulically communicates with turbine by inlet, and with chamber, by outlet and it has exit sections made in form of nozzles. At afterburning, port of chamber is closed by gates and chamber operates as afterburner.

EFFECT: increased fuel economy of engine at cruising speeds of flight.

11 dwg

Similar patents RU2305200C2

Title Year Author Number
TURBOJET ENGINE 2019
  • Kulikov Vladimir Dmitrievich
RU2727532C1
TURBO-EJECTOR ENGINE 1999
  • Pis'Mennyj V.L.
RU2190772C2
TWO-SPOOL TURBOJET ENGINE 0
  • Vorontsov Aleksandr Vasilevich
  • Dembo Nikolaj Samuilovich
  • Lyulka Arkhip Mikhajlovich
SU1809145A1
GAS-TURBINE ENGINE 2013
  • Artjukhov Aleksandr Viktorovich
  • Erichev Dmitrij Jur'Evich
  • Efimov Andrej Sergeevich
  • Ivanov Igor' Nikolaevich
  • Kirjukhin Vladimir Valentinovich
  • Kuprik Viktor Viktorovich
  • Kotel'Nikov Andrej Rostislavovich
  • Manapov Irik Usmanovich
  • Marchukov Evgenij Juvenal'Evich
  • Simonov Sergej Anatol'Evich
  • Selivanov Vadim Nikolaevich
RU2555933C2
JET TURBINE ENGINE 2013
  • Artjukhov Aleksandr Viktorovich
  • Beresneva Tat'Jana Aleksandrovna
  • Erichev Dmitrij Jur'Evich
  • Kondrashov Igor' Aleksandrovich
  • Kuprik Viktor Viktorovich
  • Manapov Irik Usmanovich
  • Marchukov Evgenij Juvenal'Evich
  • Poljakov Konstantin Sergeevich
  • Simonov Sergej Anatol'Evich
  • Selivanov Nikolaj Pavlovich
RU2555939C2
AVIATION BYPASS TURBOJET ENGINE 2007
  • Alekseev Jurij Sergeevich
  • Ivakh Aleksandr Fedorovich
RU2353790C1
TURBO-JET ENGINE AND CONTROL METHOD THEREOF 2016
  • Pismennyj Vladimir Leonidovich
RU2645373C1
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
  • Semenova Tamara Anatol'Evna
  • Simkin Ehduard L'Vovich
  • Shamsutdinov Marat Il'Darovich
  • Shustov Viktor Alekseevich
  • Khamitov Rafaehl' Makhmutovich
  • Il'Jushkin Vasilij Vasil'Evich
  • Korobova Nadezhda Vasil'Evna
  • Tonkikh Svetlana Jur'Evna
RU2271460C2
TWO-SPOOL TURBOJET ENGINE 0
  • Dembo Nikolaj Samuilovich
SU1809147A1
JET TURBINE ENGINE 2013
  • Artjukhov Aleksandr Viktorovich
  • Erichev Dmitrij Jur'Evich
  • Kirjukhin Vladimir Valentinovich
  • Kondrashov Igor' Aleksandrovich
  • Kononov Nikolaj Aleksandrovich
  • Kuprik Viktor Viktorovich
  • Manapov Irik Usmanovich
  • Marchukov Evgenij Juvenal'Evich
  • Poljakov Konstantin Sergeevich
  • Simonov Sergej Anatol'Evich
  • Selivanov Nikolaj Pavlovich
RU2555950C2

RU 2 305 200 C2

Authors

Gol'Dinskij Ehmmanuil Izrailevich

Eliseev Jurij Sergeevich

Ovchinnikov Aleksandr Anatol'Evich

Poklad Valerij Aleksandrovich

Jakubovskij Konstantin Jakovlevich

Dates

2007-08-27Published

2005-05-18Filed