[go: up one dir, main page]

RU2006100793A - DEVICE FOR CONNECTING TURBINE SHAFT AND GAS-TURBINE ENGINE COMPRESSOR - Google Patents

DEVICE FOR CONNECTING TURBINE SHAFT AND GAS-TURBINE ENGINE COMPRESSOR Download PDF

Info

Publication number
RU2006100793A
RU2006100793A RU2006100793/06A RU2006100793A RU2006100793A RU 2006100793 A RU2006100793 A RU 2006100793A RU 2006100793/06 A RU2006100793/06 A RU 2006100793/06A RU 2006100793 A RU2006100793 A RU 2006100793A RU 2006100793 A RU2006100793 A RU 2006100793A
Authority
RU
Russia
Prior art keywords
turbine
shaft
gas
engine compressor
turbine engine
Prior art date
Application number
RU2006100793/06A
Other languages
Russian (ru)
Other versions
RU2310088C2 (en
Inventor
Анатолий Иванович Тункин (RU)
Анатолий Иванович Тункин
Original Assignee
Открытое акционерное общество "Авиадвигатель" (RU)
Открытое акционерное общество "Авиадвигатель"
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 Открытое акционерное общество "Авиадвигатель" (RU), Открытое акционерное общество "Авиадвигатель" filed Critical Открытое акционерное общество "Авиадвигатель" (RU)
Priority to RU2006100793/06A priority Critical patent/RU2310088C2/en
Publication of RU2006100793A publication Critical patent/RU2006100793A/en
Application granted granted Critical
Publication of RU2310088C2 publication Critical patent/RU2310088C2/en

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)

Claims (1)

Устройство соединения валов турбины и компрессора газотурбинного двигателя, содержащее промежуточный вал, в задний хвостовик которого по шлицам через шлицевую муфту установлен вал турбины, а в передний хвостовик - вал компрессора, отличающийся тем, что на наружном диаметре шлиц вала турбины в кольцевую проточку заднего хвостовика промежуточного вала установлено центрирующее кольцо.A device for connecting the shafts of a turbine and a compressor of a gas turbine engine, comprising an intermediate shaft, a turbine shaft installed in the rear shank of the splines through a splined sleeve, and a compressor shaft in the front shank, characterized in that on the outer diameter of the turbine shaft splined into the annular groove of the rear shank of the intermediate the shaft has a centering ring.
RU2006100793/06A 2006-01-10 2006-01-10 Device for connecting shafts of turbine and compressor of gas-turbine engine RU2310088C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2006100793/06A RU2310088C2 (en) 2006-01-10 2006-01-10 Device for connecting shafts of turbine and compressor of gas-turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2006100793/06A RU2310088C2 (en) 2006-01-10 2006-01-10 Device for connecting shafts of turbine and compressor of gas-turbine engine

Publications (2)

Publication Number Publication Date
RU2006100793A true RU2006100793A (en) 2007-07-20
RU2310088C2 RU2310088C2 (en) 2007-11-10

Family

ID=38430864

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2006100793/06A RU2310088C2 (en) 2006-01-10 2006-01-10 Device for connecting shafts of turbine and compressor of gas-turbine engine

Country Status (1)

Country Link
RU (1) RU2310088C2 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8955230B2 (en) 2012-06-12 2015-02-17 Solar Turbines Inc. Shaft alignment tools and methods
US8997365B2 (en) 2012-06-12 2015-04-07 Solar Turbines Incorporated Shaft alignment tools and methods

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2405955C1 (en) * 2009-07-07 2010-12-10 Открытое акционерное общество "Научно-производственное объединение "Сатурн" (ОАО "НПО "Сатурн") Assembly of joint between gas turbine engine compressor and turbine rotors
US8689455B2 (en) 2012-02-29 2014-04-08 Solar Turbines Inc. Shaft alignment tool
RU2542656C1 (en) * 2014-03-06 2015-02-20 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Connecting assembly of rotors of compressor and turbine of gas turbine engine
RU2579286C1 (en) * 2014-12-05 2016-04-10 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Coupling assembly between compressor rotors and turbine of a gas turbine engine
RU2682462C1 (en) * 2018-04-11 2019-03-19 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Gas turbine engine low pressure rotor connection unit

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2738125A (en) * 1951-06-19 1956-03-13 United Aircraft Corp Locking means between compressor and turbine
US3900270A (en) * 1973-09-22 1975-08-19 Rolls Royce 1971 Ltd Shaft couplings
RU2003821C1 (en) * 1991-07-29 1993-11-30 Акционерное общество открытого типа "Авиадвигатель" Inter-shaft bearing unit of turbomachine
RU2190110C2 (en) * 2000-05-15 2002-09-27 Открытое акционерное общество "Авиадвигатель" Gas-turbine engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8955230B2 (en) 2012-06-12 2015-02-17 Solar Turbines Inc. Shaft alignment tools and methods
US8997365B2 (en) 2012-06-12 2015-04-07 Solar Turbines Incorporated Shaft alignment tools and methods

Also Published As

Publication number Publication date
RU2310088C2 (en) 2007-11-10

Similar Documents

Publication Publication Date Title
EP2148139A3 (en) Flow sleeve impingement cooling using a plenum ring
EP1719949A3 (en) Compliant metal support for ceramic combustor liner in a gas turbine engine
EP2148140A3 (en) Flow sleeve impingement cooling baffles
EP2395202A3 (en) A mounting assembly for a gearbox of gas turbine engine
WO2011080433A3 (en) Guiding of a spark plug into a turbine engine combustion chamber
WO2010007220A3 (en) Turbomachine structural casing
EP1921383A3 (en) Combustor dome and methods of assembling such
EP1850070A3 (en) Methods and system for reducing pressure losses in gas turbine engines
WO2006110124A3 (en) Ejector cooling of outer case for tip turbine engine
JP2013536910A5 (en)
EP2108787A3 (en) Methods for repairing a damaged variable vane shroud and corresponding vane shroud
WO2009051236A1 (en) Gas turbine
EP1439350A3 (en) Support assembly for a gas turbine engine combustor
EP2354491A3 (en) Gas turbine engine steam injection manifold
EP2208933A3 (en) Combustor assembly and cap for a turbine engine
ATE317060T1 (en) DEVICE FOR CENTERING A TUBE IN A TURBINE SHAFT
EP1862737A3 (en) Large diameter Mid-Zone air separation cone for expanding IRZ
RU2008100463A (en) TURBO-FAN ENGINE
WO2011033242A3 (en) Combustion chamber of an aeronautical turbine engine with combustion holes having different configurations.
JP5149596B2 (en) Combustor dome mixer holding means
CA2659823A1 (en) Thrust bearing housing for a gas turbine engine
WO2008146579A1 (en) Gas turbine engine
EP1394470A3 (en) Multiple-domes annular combustor for a gas turbine engine
RU2006100793A (en) DEVICE FOR CONNECTING TURBINE SHAFT AND GAS-TURBINE ENGINE COMPRESSOR
RU2000112276A (en) GAS TURBINE ENGINE

Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20130111