RU92006859A - JET ENGINE - Google Patents

JET ENGINE

Info

Publication number
RU92006859A
RU92006859A RU92006859/06A RU92006859A RU92006859A RU 92006859 A RU92006859 A RU 92006859A RU 92006859/06 A RU92006859/06 A RU 92006859/06A RU 92006859 A RU92006859 A RU 92006859A RU 92006859 A RU92006859 A RU 92006859A
Authority
RU
Russia
Prior art keywords
pressure inlet
jet engine
compressor
ejector
afterburner
Prior art date
Application number
RU92006859/06A
Other languages
Russian (ru)
Other versions
RU2066777C1 (en
Inventor
В.Ф. Шевцов
Original Assignee
В.Ф. Шевцов
Filing date
Publication date
Application filed by В.Ф. Шевцов filed Critical В.Ф. Шевцов
Priority to RU92006859A priority Critical patent/RU2066777C1/en
Priority claimed from RU92006859A external-priority patent/RU2066777C1/en
Publication of RU92006859A publication Critical patent/RU92006859A/en
Application granted granted Critical
Publication of RU2066777C1 publication Critical patent/RU2066777C1/en

Links

Claims (1)

Изобретение относится к авиационной и космической технике, а после выработки летного ресурса может быть использовано в качестве привода газовой турбины для выработки механической или электрической энергии для нужд народного хозяйства. Сущность изобретения: реактивный двигатель содержит компрессор, камеры сгорания, турбины, сопла, а также эжекторный компрессор, входной патрубок высокого давления к камере сгорания. Дополнительный эжектор предназначен для дожатия воздуха перед соплом, и его входной патрубок низкого давления соединен с воздухозаборником, а входной патрубок высокого давления через форсажную камеру с выходом турбины.The invention relates to aviation and space technology, and after the development of the flight resource can be used as a gas turbine drive for the generation of mechanical or electrical energy for the needs of the national economy. The inventive jet engine includes a compressor, combustion chambers, turbines, nozzles, as well as an ejector compressor, high-pressure inlet to the combustion chamber. An additional ejector is designed for air pressure before the nozzle, and its low pressure inlet is connected to the air intake, and the high pressure inlet is through the afterburner with the turbine outlet.
RU92006859A 1992-11-17 1992-11-17 Engine RU2066777C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU92006859A RU2066777C1 (en) 1992-11-17 1992-11-17 Engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU92006859A RU2066777C1 (en) 1992-11-17 1992-11-17 Engine

Publications (2)

Publication Number Publication Date
RU92006859A true RU92006859A (en) 1995-01-20
RU2066777C1 RU2066777C1 (en) 1996-09-20

Family

ID=20132207

Family Applications (1)

Application Number Title Priority Date Filing Date
RU92006859A RU2066777C1 (en) 1992-11-17 1992-11-17 Engine

Country Status (1)

Country Link
RU (1) RU2066777C1 (en)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2913063B1 (en) * 2007-02-27 2012-03-16 Snecma AIRCRAFT ENGINE EQUIPPED WITH THERMAL EXCHANGE MEANS.
RU2531110C2 (en) * 2010-06-29 2014-10-20 Дженерал Электрик Компани Gas-turbine unit and unit with injector vanes (versions)
RU2485330C1 (en) * 2011-11-16 2013-06-20 Федеральное государственное бюджетное учреждение "Национальный исследовательский центр "Курчатовский институт" Method of energy generation
RU2488709C1 (en) * 2012-04-11 2013-07-27 Открытое акционерное общество "Авиадвигатель" Aircraft power plant
RU2561764C1 (en) * 2014-01-10 2015-09-10 Николай Борисович Болотин Hydrogen gas turbine engine
RU2554392C1 (en) * 2014-01-10 2015-06-27 Николай Борисович Болотин Hydrogen gas turbine engine
RU2561772C1 (en) * 2014-01-14 2015-09-10 Николай Борисович Болотин Air-jet engine
RU2561757C1 (en) * 2014-01-14 2015-09-10 Николай Борисович Болотин Three-component air-jet engine
RU2553052C1 (en) * 2014-01-29 2015-06-10 Николай Борисович Болотин Hydrogen air-jet engine
RU2593573C1 (en) * 2015-01-12 2016-08-10 Николай Борисович Болотин Engine of hypersonic aircraft
RU2594091C1 (en) * 2015-01-12 2016-08-10 Николай Борисович Болотин Engine of hypersonic aircraft
RU2591361C1 (en) * 2015-01-13 2016-07-20 Николай Борисович Болотин Engine of hypersonic aircraft
RU2594828C1 (en) * 2015-01-19 2016-08-20 Николай Борисович Болотин Propulsion engine of supersonic aircraft
RU2645373C1 (en) * 2016-05-17 2018-02-21 Владимир Леонидович Письменный Turbo-jet engine and control method thereof

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