RU2012103791A - METHOD FOR SUBMITTING FUEL TO A GAS-TURBINE ENGINE - Google Patents

METHOD FOR SUBMITTING FUEL TO A GAS-TURBINE ENGINE Download PDF

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Publication number
RU2012103791A
RU2012103791A RU2012103791/06A RU2012103791A RU2012103791A RU 2012103791 A RU2012103791 A RU 2012103791A RU 2012103791/06 A RU2012103791/06 A RU 2012103791/06A RU 2012103791 A RU2012103791 A RU 2012103791A RU 2012103791 A RU2012103791 A RU 2012103791A
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RU
Russia
Prior art keywords
fuel
heated
turbine engine
ice formation
temperature
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RU2012103791/06A
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Russian (ru)
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RU2514522C2 (en
Inventor
Владимир Викторович Черниченко
Павел Анатольевич Солженикин
Владимир Григорьевич Стогней
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Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет"
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Priority to RU2012103791/06A priority Critical patent/RU2514522C2/en
Publication of RU2012103791A publication Critical patent/RU2012103791A/en
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Publication of RU2514522C2 publication Critical patent/RU2514522C2/en

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  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Feeding And Controlling Fuel (AREA)

Abstract

1. Способ подачи топлива в газотурбинный двигатель при запуске после длительного пребывания при низких температурах, заключающийся в подогреве топлива перед подачей его в топливный фильтр, причем перед подогревом отделяют от топлива льдообразования, которые подогревают до таяния, после чего воду, полученную при таянии льдообразовании, соединяют с подогретым топливом, отличающийся тем, что упомянутую воду дополнительно подогревают до температуры не ниже температуры подогретого топлива, предпочтительно, до температуры, близкой к температуре кипения.2. Способ по п.1, отличающийся тем, что подогрев льдообразовании осуществляют отбираемым от компрессора газотурбинного двигателя воздухом.1. The method of supplying fuel to a gas turbine engine when starting after a long stay at low temperatures, which consists in heating the fuel before feeding it into the fuel filter, and before heating, ice formation is separated from the fuel, which is heated until it melts, after which the water obtained by melting ice formation, combined with heated fuel, characterized in that the said water is additionally heated to a temperature not lower than the temperature of the heated fuel, preferably to a temperature close to tamper kipeniya.2 round. The method according to claim 1, characterized in that the ice formation is heated by air taken from the compressor of the gas turbine engine.

Claims (2)

1. Способ подачи топлива в газотурбинный двигатель при запуске после длительного пребывания при низких температурах, заключающийся в подогреве топлива перед подачей его в топливный фильтр, причем перед подогревом отделяют от топлива льдообразования, которые подогревают до таяния, после чего воду, полученную при таянии льдообразовании, соединяют с подогретым топливом, отличающийся тем, что упомянутую воду дополнительно подогревают до температуры не ниже температуры подогретого топлива, предпочтительно, до температуры, близкой к температуре кипения.1. The method of supplying fuel to a gas turbine engine when starting after a long stay at low temperatures, which consists in heating the fuel before feeding it into the fuel filter, and before heating, ice formation is separated from the fuel, which is heated until it melts, after which the water obtained by melting ice formation, combined with heated fuel, characterized in that the said water is additionally heated to a temperature not lower than the temperature of the heated fuel, preferably to a temperature close to tamper Boiling round. 2. Способ по п.1, отличающийся тем, что подогрев льдообразовании осуществляют отбираемым от компрессора газотурбинного двигателя воздухом. 2. The method according to claim 1, characterized in that the ice formation is heated by air taken from the compressor of the gas turbine engine.
RU2012103791/06A 2012-02-03 2012-02-03 Method of controlling fuel feed to gas turbine engine RU2514522C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2012103791/06A RU2514522C2 (en) 2012-02-03 2012-02-03 Method of controlling fuel feed to gas turbine engine

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Application Number Priority Date Filing Date Title
RU2012103791/06A RU2514522C2 (en) 2012-02-03 2012-02-03 Method of controlling fuel feed to gas turbine engine

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RU2012103791A true RU2012103791A (en) 2013-08-10
RU2514522C2 RU2514522C2 (en) 2014-04-27

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Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10703500B2 (en) 2018-07-10 2020-07-07 Hamilton Sundstrand Corporation Heated pipe for liquid flows

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1559828A (en) * 1975-09-12 1980-01-30 Rolls Royce Fuel system for gas turbine engines
GB2099509A (en) * 1981-05-21 1982-12-08 Dowty Fuel Syst Ltd Heating of aircraft fuel
US5867977A (en) * 1996-05-14 1999-02-09 The Dow Chemical Company Method and apparatus for achieving power augmentation in gas turbines via wet compression
RU2163978C2 (en) * 1999-03-22 2001-03-10 Центральный институт авиационного моторостроения (ЦИАМ) им. П.И. Баранова Method of fuel supply to gas turbine engine at its starting after long period of standing at low temperatures and fuel system of gas turbine engine
RU2194870C2 (en) * 2000-12-15 2002-12-20 Акчурин Харас Исхакович Method of operation and design of gas turbine plant with complex system of deep recovery of heat and production of harmful effluents

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Effective date: 20150204