SEAL OF INNER JOINT BETWEEN GAS TURBINE DISTRIBUTOR AND COMBUSTION CHAMBER Russian patent published in 2013 - IPC F02C7/28 

Abstract RU 2496017 C1

FIELD: engines and pumps.

SUBSTANCE: proposed seal comprises combustion chamber seal ring and distributor deflector. Said deflector is secured at distributor inner case. Combustion chamber seal ring guide part and distributor deflector make annular gap for feeding cooling air. Seal ring locking part has centering grooves to receive distributor deflector ledges and be centered over side mating surfaces. Annular gap "a" is formed between deflector outer surface and guide part inner surface. Fit with gal "b" is arranged between fire tube seal ring and distributor deflector ledges over side surfaces. For attachment of said deflector to distributor inner case bolts having variable clearance with deflector bores and gap "c" in meridian section. Said bolts make thread joint with distributor inner case bores to allow aforesaid said deflector to shift radially and axially relative to distributor inner case.

EFFECT: reduced vibratory loads, uniform distribution of cooling air in axial direction.

2 dwg

Similar patents RU2496017C1

Title Year Author Number
SEAL OF GAS TURBINE ENGINE COMBUSTION CHAMBER-TO-STATOR JOINT 2012
  • Khabibullin Midkhat Gubajdullovich
  • Zhil'Tsov Evgenij Izosimovich
  • Khusnullin Vjacheslav Khazievich
  • Merkushin Valentin Konstantinovich
  • Vil'Gemskaja Elena Viktorovna
RU2493388C1
DEVICE FOR ATTACHMENT OF FLAME TUBE IN BODY OF COMBUSTION CHAMBER 2001
  • Shajkhutdinov A.Z.
  • Vodbol'Skij I.Ju.
  • Vasin O.E.
  • Prokopets A.O.
  • Epejkin L.F.
  • Markushin A.N.
  • Vasil'Ev V.I.
  • Kanunnikov I.P.
  • Korotov M.V.
RU2223448C2
CONNECTION ASSEMBLY OF NOZZLE APPARATUS OF HIGH-PRESSURE TURBINE WITH END PART OF FLAME TUBE OF COMBUSTION CHAMBER OF GAS TURBINE ENGINE 2020
  • Kuzmin Maksim Vladimirovich
  • Khanin Aleksandr Anatolevich
RU2755453C1
TUBULAR-ANNULAR COMBUSTION CHAMBER OF GAS TURBINE ENGINE 1998
  • Khajrullin M.F.
  • Medvedev A.V.
  • Khrjashchikov M.S.
  • Kirievskij Ju.E.
  • Devjatkov V.V.
  • Verkholantsev S.V.
  • Vasil'Ev A.N.
RU2151961C1
LOW-PRESSURE TURBINE STATOR 2013
  • Sychev Vladimir Konstantinovich
  • Jazev Vladimir Mikhajlovich
  • Kuznetsov Valerij Alekseevich
RU2534669C1
TURBOMACHINE STATOR 2013
  • Sychev Vladimir Konstantinovich
  • Jazev Vladimir Mikhajlovich
  • Kuznetsov Valerij Alekseevich
RU2519677C1
DEVICE FOR MECHANICAL CONTROL OF RADIAL CLEARANCE BETWEEN ENDS OF ROTOR BLADES AND STATOR OF COMPRESSOR AND GAS TURBINE ENGINE TURBINE, METHOD OF CONTROLLING RADIAL CLEARANCE BETWEEN ENDS OF ROTOR BLADES AND STATOR OF COMPRESSOR AND GAS TURBINE ENGINE TURBINE 2017
  • Eskin Izold Davidovich
  • Startsev Nikolaj Ivanovich
  • Falaleev Sergej Viktorinovich
RU2702063C2
DEVICE FOR ATTACHMENT OF FLAME TUBE IN BODY OF COMBUSTION CHAMBER 2001
  • Shajkhutdinov A.Z.
  • Vodbol'Skij I.Ju.
  • Vasin O.E.
  • Prokopets A.O.
  • Epejkin L.F.
  • Markushin A.N.
  • Kanunnikov I.P.
  • Korotov M.V.
RU2223447C2
BYPASS GAS TURBINE ENGINE 2012
  • Bolotin Nikolaj Borisovich
RU2499894C1
YUGI'S TURBO-ROTOR ENGINE 2007
  • Il'Inykh Jurij Gavrilovich
RU2359140C2

RU 2 496 017 C1

Authors

Khabibullin Midkhat Gubajdullovich

Ivannikov Vladimir Fedorovich

Khusnullin Vjacheslav Khazievich

Dates

2013-10-20Published

2012-03-27Filed