RU2014129234A - METHOD FOR FORCING A TWO-CIRCUIT TURBOREACTIVE ENGINE - Google Patents

METHOD FOR FORCING A TWO-CIRCUIT TURBOREACTIVE ENGINE Download PDF

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Publication number
RU2014129234A
RU2014129234A RU2014129234A RU2014129234A RU2014129234A RU 2014129234 A RU2014129234 A RU 2014129234A RU 2014129234 A RU2014129234 A RU 2014129234A RU 2014129234 A RU2014129234 A RU 2014129234A RU 2014129234 A RU2014129234 A RU 2014129234A
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RU
Russia
Prior art keywords
forcing
circuit
dual
combustion chamber
main combustion
Prior art date
Application number
RU2014129234A
Other languages
Russian (ru)
Other versions
RU2578941C2 (en
Inventor
Владимир Леонидович Письменный
Original Assignee
Владимир Леонидович Письменный
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Application filed by Владимир Леонидович Письменный filed Critical Владимир Леонидович Письменный
Priority to RU2014129234/06A priority Critical patent/RU2578941C2/en
Publication of RU2014129234A publication Critical patent/RU2014129234A/en
Application granted granted Critical
Publication of RU2578941C2 publication Critical patent/RU2578941C2/en

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Supercharger (AREA)

Abstract

1. Способ форсирования двухконтурного турбореактивного двигателя, заключающийся в подаче в основную камеру сгорания форсажного топлива, отличающийся тем, что коллектор форсажного топлива расположен в зоне вторичного воздуха основной камеры сгорания.2. Способ форсирования двухконтурного турбореактивного двигателя по п. 1, отличающийся тем, что частота вращения ротора (роторов) двигателя и перепад давлений на турбинах поддерживаются постоянными.1. A method of forcing a dual-circuit turbojet engine, which consists in supplying afterburner fuel to the main combustion chamber, characterized in that the afterburner manifold is located in the secondary air zone of the main combustion chamber. The method of forcing a dual-circuit turbojet engine according to claim 1, characterized in that the rotational speed of the rotor (s) of the engine and the pressure drop across the turbines are kept constant.

Claims (2)

1. Способ форсирования двухконтурного турбореактивного двигателя, заключающийся в подаче в основную камеру сгорания форсажного топлива, отличающийся тем, что коллектор форсажного топлива расположен в зоне вторичного воздуха основной камеры сгорания.1. The method of forcing a dual-circuit turbojet engine, which consists in supplying afterburner fuel to the main combustion chamber, characterized in that the afterburner manifold is located in the secondary air zone of the main combustion chamber. 2. Способ форсирования двухконтурного турбореактивного двигателя по п. 1, отличающийся тем, что частота вращения ротора (роторов) двигателя и перепад давлений на турбинах поддерживаются постоянными. 2. The method of forcing a dual-circuit turbojet engine according to claim 1, characterized in that the rotational speed of the rotor (s) of the engine and the pressure drop across the turbines are kept constant.
RU2014129234/06A 2014-07-15 2014-07-15 Method of boosting bypass turbojet engine RU2578941C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2014129234/06A RU2578941C2 (en) 2014-07-15 2014-07-15 Method of boosting bypass turbojet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2014129234/06A RU2578941C2 (en) 2014-07-15 2014-07-15 Method of boosting bypass turbojet engine

Publications (2)

Publication Number Publication Date
RU2014129234A true RU2014129234A (en) 2016-02-10
RU2578941C2 RU2578941C2 (en) 2016-03-27

Family

ID=55313118

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2014129234/06A RU2578941C2 (en) 2014-07-15 2014-07-15 Method of boosting bypass turbojet engine

Country Status (1)

Country Link
RU (1) RU2578941C2 (en)

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2413507A1 (en) * 1974-03-20 1975-10-02 Motoren Turbinen Union GAS TURBINE FOR CRYOGENIC FUEL
RU2248456C1 (en) * 2003-07-01 2005-03-20 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" By-pass engine afterburner
RU2419035C2 (en) * 2008-12-23 2011-05-20 Николай Евгеньевич Староверов Three-zone engine (versions)
RU2474718C2 (en) * 2011-01-25 2013-02-10 Николай Евгеньевич Староверов Method of turbojet afterburning and engine to this end (versions)

Also Published As

Publication number Publication date
RU2578941C2 (en) 2016-03-27

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