UA16538A1 - Method and device for fuel burning in gas-turbine engine - Google Patents

Method and device for fuel burning in gas-turbine engine

Info

Publication number
UA16538A1
UA16538A1 UA4110954A UA4110954A UA16538A1 UA 16538 A1 UA16538 A1 UA 16538A1 UA 4110954 A UA4110954 A UA 4110954A UA 4110954 A UA4110954 A UA 4110954A UA 16538 A1 UA16538 A1 UA 16538A1
Authority
UA
Ukraine
Prior art keywords
burning
gas
turbine engine
catalytic element
gas mixture
Prior art date
Application number
UA4110954A
Other languages
Russian (ru)
Ukrainian (uk)
Inventor
Ігор Павлович Васильєв
Игорь Павлович Васильев
Петр Миколайович Гавриленко
Петр Николаевич Гавриленко
Фустє Гонсалєс Алєхандро
Фусте Гонсалес Алехандро
Гєррєро Вієро Алексіс
Герреро Виеро Алексис
Original Assignee
Ворошиловградський Машинобудівний Інститут
Ворошиловградский машиностроительный институт
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.)
Filing date
Publication date
Application filed by Ворошиловградський Машинобудівний Інститут, Ворошиловградский машиностроительный институт filed Critical Ворошиловградський Машинобудівний Інститут
Priority to UA4110954A priority Critical patent/UA16538A1/en
Publication of UA16538A1 publication Critical patent/UA16538A1/en

Links

Abstract

A method for fuel burning in gas-turbine engine is performed through separation of air flow to primary and secondary air flows, injection of fuel to primary air flow with formation of burning mix, its supply to catalytic element for combustion, mixing of burning products with secondary air, measurement of control parameter of gas mixture obtained and its change depending on value of flow rate of burning mixture supplied to the catalytic element for its burning. To decrease losses of total pressure in flow at permitted level of gas mixture toxicity the level of gas mixture toxicity is used as control parameter, and change of value of burning mixture flow rate is performed through its partial or complete passage through catalytic element.
UA4110954A 1986-09-01 1986-09-01 Method and device for fuel burning in gas-turbine engine UA16538A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
UA4110954A UA16538A1 (en) 1986-09-01 1986-09-01 Method and device for fuel burning in gas-turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
UA4110954A UA16538A1 (en) 1986-09-01 1986-09-01 Method and device for fuel burning in gas-turbine engine

Publications (1)

Publication Number Publication Date
UA16538A1 true UA16538A1 (en) 1997-08-29

Family

ID=74558417

Family Applications (1)

Application Number Title Priority Date Filing Date
UA4110954A UA16538A1 (en) 1986-09-01 1986-09-01 Method and device for fuel burning in gas-turbine engine

Country Status (1)

Country Link
UA (1) UA16538A1 (en)

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