RU2015155123A - GAS-TURBINE ENGINE WITH STEAM INJECTORS - Google Patents

GAS-TURBINE ENGINE WITH STEAM INJECTORS Download PDF

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Publication number
RU2015155123A
RU2015155123A RU2015155123A RU2015155123A RU2015155123A RU 2015155123 A RU2015155123 A RU 2015155123A RU 2015155123 A RU2015155123 A RU 2015155123A RU 2015155123 A RU2015155123 A RU 2015155123A RU 2015155123 A RU2015155123 A RU 2015155123A
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RU
Russia
Prior art keywords
cavitator
combustion chamber
gas
housing
electrolyzer
Prior art date
Application number
RU2015155123A
Other languages
Russian (ru)
Other versions
RU2629305C2 (en
Inventor
Владислав Николаевич Ковальногов
Руслан Владимирович Федоров
Дмитрий Александрович Генералов
Александр Николаевич Золотов
Мария Игоревна Корнилова
Original Assignee
Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Ульяновский государственный технический университет"
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Application filed by Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Ульяновский государственный технический университет" filed Critical Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Ульяновский государственный технический университет"
Priority to RU2015155123A priority Critical patent/RU2629305C2/en
Publication of RU2015155123A publication Critical patent/RU2015155123A/en
Application granted granted Critical
Publication of RU2629305C2 publication Critical patent/RU2629305C2/en

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones

Landscapes

  • Engine Equipment That Uses Special Cycles (AREA)

Claims (1)

Газотурбинный двигатель с паровыми форсунками, содержащий корпус и герметизирующую вход в корпус крышку, компрессор, камеру сгорания, систему подачи электролита через форсунку с кавитатором, воспламеняющее устройство, турбину и электролизер, герметизирующая вход в корпус крышка выполнена с возможностью регулируемого забора воздуха в двигатель, система подачи электролита выполнена с возможностью подачи электролита через форсунку с кавитатором в поток забираемого в двигатель воздуха и с возможностью подачи топлива в камеру сгорания, электролизер при этом выполнен в виде кавитатора с центральным телом путем подводки постоянного электрического тока от источника питания к элементам кавитатора и установлен в обособленном корпусе, герметично соединенном с камерой сгорания, с возможностью подачи газовой смеси под давлением за компрессором через этот электролизер-кавитатор с центральным телом в камеру сгорания, трубу Леонтьева для разделения потока газа из камеры сгорания на дозвуковую и сверхзвуковую составляющие, канал рециркуляции дозвукового потока, отличающийся тем, что перед трубой Леонтьева установлена паровая форсунка, впрыскивающая пар в дозвуковой и сверхзвуковой потоки газа.A gas turbine engine with steam nozzles, comprising a housing and a cover sealing the entrance to the housing, a compressor, a combustion chamber, an electrolyte supply system through a nozzle with a cavitator, an ignition device, a turbine and an electrolyzer, a sealing entrance to the housing; the cover is configured to take air into the engine, the system the electrolyte supply is configured to supply electrolyte through a nozzle with a cavitator into the flow of air taken into the engine and with the possibility of supplying fuel to the combustion chamber, e The electrolyzer in this case is made in the form of a cavitator with a central body by applying a constant electric current from the power source to the elements of the cavitator and installed in a separate housing hermetically connected to the combustion chamber, with the possibility of supplying the gas mixture under pressure behind the compressor through this electrolyzer-cavitator with the central body into the combustion chamber, a Leontief pipe for separating the gas flow from the combustion chamber into subsonic and supersonic components, a subsonic flow recirculation channel, characterized by We note that a steam nozzle is installed in front of the Leontief pipe, which injects steam into the subsonic and supersonic gas flows.
RU2015155123A 2015-12-22 2015-12-22 Gas turbine engine with steam nozzles RU2629305C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2015155123A RU2629305C2 (en) 2015-12-22 2015-12-22 Gas turbine engine with steam nozzles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2015155123A RU2629305C2 (en) 2015-12-22 2015-12-22 Gas turbine engine with steam nozzles

Publications (2)

Publication Number Publication Date
RU2015155123A true RU2015155123A (en) 2017-06-28
RU2629305C2 RU2629305C2 (en) 2017-08-28

Family

ID=59309238

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2015155123A RU2629305C2 (en) 2015-12-22 2015-12-22 Gas turbine engine with steam nozzles

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RU (1) RU2629305C2 (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH248309A (en) * 1945-04-17 1947-04-30 Sulzer Ag Method for operating gas turbine plants and device for carrying out the method.
BE1010251A4 (en) * 1995-10-20 1998-04-07 Oxipar Sprl Method for partial oxidation catalyst on fuel gas turbine in combined energy systems and device for its implementation.
RU2163323C1 (en) * 1999-06-18 2001-02-20 Научно-производственное предприятие "Саров" Method of nonheated pressure reduction of main-line natural gas and device for its embodiment
RU2324831C1 (en) * 2006-09-05 2008-05-20 Михаил Иванович Весенгириев Gas turbine engine
RU2334178C1 (en) * 2007-03-09 2008-09-20 Государственное образовательное учреждение высшего профессионального образования "Ульяновский государственный технический университет" Supersonic tube of temperature stratification
RU2557793C1 (en) * 2014-03-14 2015-07-27 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Ульяновский государственный технический университет" Gas turbine engine

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Publication number Publication date
RU2629305C2 (en) 2017-08-28

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20171223