RU2000117929A - FUEL AIR BURNER OF THE COMBUSTION CHAMBER OF A GAS-TURBINE ENGINE - Google Patents

FUEL AIR BURNER OF THE COMBUSTION CHAMBER OF A GAS-TURBINE ENGINE

Info

Publication number
RU2000117929A
RU2000117929A RU2000117929/06A RU2000117929A RU2000117929A RU 2000117929 A RU2000117929 A RU 2000117929A RU 2000117929/06 A RU2000117929/06 A RU 2000117929/06A RU 2000117929 A RU2000117929 A RU 2000117929A RU 2000117929 A RU2000117929 A RU 2000117929A
Authority
RU
Russia
Prior art keywords
combustion chamber
turbine engine
gas
air burner
fuel air
Prior art date
Application number
RU2000117929/06A
Other languages
Russian (ru)
Other versions
RU2199700C2 (en
Inventor
Петр Николаевич Касьминов
Андрей Владимирович Охлобыстин
Владимир Яковлевич Шинкарев
Валерий Григорьевич Ланин
Original Assignee
Открытое акционерное общество "Рыбинские моторы"
Filing date
Publication date
Application filed by Открытое акционерное общество "Рыбинские моторы" filed Critical Открытое акционерное общество "Рыбинские моторы"
Priority to RU2000117929A priority Critical patent/RU2199700C2/en
Priority claimed from RU2000117929A external-priority patent/RU2199700C2/en
Publication of RU2000117929A publication Critical patent/RU2000117929A/en
Application granted granted Critical
Publication of RU2199700C2 publication Critical patent/RU2199700C2/en

Links

Claims (1)

Топливовоздушная горелка камеры сгорания газотурбинного двигателя, содержащая двухъярусный завихритель, во внутреннем ярусе которого установлен осевой лопаточный завихритель с открытым выходным торцем, отличающаяся тем, что на входном торце осевого лопаточного завихрителя расположена перегородка, перекрывающая часть входного торца, выполненная, например, в виде кольца.A fuel-air burner of a combustion chamber of a gas turbine engine containing a two-tier swirl, in the inner tier of which an axial blade swirl with an open outlet end is installed, characterized in that a partition is located at the inlet end of the axial blade swirl, for example, made in the form of a ring.
RU2000117929A 2000-07-05 2000-07-05 Fuel-air furnace of gas-turbine engine combustion chamber RU2199700C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2000117929A RU2199700C2 (en) 2000-07-05 2000-07-05 Fuel-air furnace of gas-turbine engine combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2000117929A RU2199700C2 (en) 2000-07-05 2000-07-05 Fuel-air furnace of gas-turbine engine combustion chamber

Publications (2)

Publication Number Publication Date
RU2000117929A true RU2000117929A (en) 2002-09-10
RU2199700C2 RU2199700C2 (en) 2003-02-27

Family

ID=20237459

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2000117929A RU2199700C2 (en) 2000-07-05 2000-07-05 Fuel-air furnace of gas-turbine engine combustion chamber

Country Status (1)

Country Link
RU (1) RU2199700C2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2749434C1 (en) * 2020-08-25 2021-06-10 Федеральное государственное бюджетное образовательное учреждение высшего образования "Казанский национальный исследовательский технический университет им. А.Н. Туполева - КАИ" Air-fuel burner and frontal device of combustion chamber

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