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SU1635645A1 - DRIVE OF GAS TURBINE INSTALLATION - Google Patents

DRIVE OF GAS TURBINE INSTALLATION

Info

Publication number
SU1635645A1
SU1635645A1 SU4623476/06A SU4623476A SU1635645A1 SU 1635645 A1 SU1635645 A1 SU 1635645A1 SU 4623476/06 A SU4623476/06 A SU 4623476/06A SU 4623476 A SU4623476 A SU 4623476A SU 1635645 A1 SU1635645 A1 SU 1635645A1
Authority
SU
USSR - Soviet Union
Prior art keywords
shaft
additional
turbine
drive
coupling
Prior art date
Application number
SU4623476/06A
Other languages
Russian (ru)
Inventor
А.А. Кохан
Original Assignee
А.А. Кохан
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 А.А. Кохан filed Critical А.А. Кохан
Priority to SU4623476/06A priority Critical patent/SU1635645A1/en
Application granted granted Critical
Publication of SU1635645A1 publication Critical patent/SU1635645A1/en

Links

Landscapes

  • Gear Transmission (AREA)
  • Structure Of Transmissions (AREA)

Abstract

Привод газотурбинной установки, содержащий валы турбины заднего хода и турбины переднего хода, вал отбора мощности для привода винта фиксированного шага, установленный в корпусе двухступенчатый редуктор, включающий ведущую и ведомую шестерни, разобщительную муфту, при этом вал турбины переднего хода соединен с ведущей шестерней, а вал отбора мощности соединен с валом ведомой шестерни посредством разобщительной муфты, отличающийся тем, что, с целью повышения надежности и маневренности привода, редуктор содержит дополнительную ведущую шестерню, установленную на валу турбины заднего хода, дополнительную ведомую шестерню, соединенную с валом отбора мощности, дополнительную промежуточную шестерню, установленную между дополнительными ведомой и ведущей шестернями, дополнительную разобщительную муфту и гидродинамическую муфту, при этом вал дополнительной ведомой шестерни соединен с валом обора мощности посредством дополнительной разобщительной муфты, а вал турбины переднего хода соединен с валом турбины заднего хода посредством гидродинамической муфты.The drive of the gas turbine unit, comprising the shafts of the back-up turbine and the forward-driven turbine, the power take-off shaft for driving the fixed-pitch propeller, a two-stage reducer mounted in the housing, including driving and driven gears, an uncoupling coupling, the forward drive turbine shaft and The power take-off shaft is connected to the driven gear shaft by means of a decoupling clutch, characterized in that, in order to improve the reliability and maneuverability of the drive, the gearbox contains an additional drive esternya, mounted on the shaft of the reverse turbine, additional driven gear connected to the power shaft, additional intermediate gear mounted between the additional driven and driving gears, additional disconnecting coupling and hydrodynamic coupling, while the shaft of the additional driven gear is connected to the shaft of the power output by additional disconnecting coupling, and the shaft of the forward turbine is connected to the shaft of the reverse turbine by means of a hydrodynamic coupling.

SU4623476/06A 1988-12-22 1988-12-22 DRIVE OF GAS TURBINE INSTALLATION SU1635645A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4623476/06A SU1635645A1 (en) 1988-12-22 1988-12-22 DRIVE OF GAS TURBINE INSTALLATION

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4623476/06A SU1635645A1 (en) 1988-12-22 1988-12-22 DRIVE OF GAS TURBINE INSTALLATION

Publications (1)

Publication Number Publication Date
SU1635645A1 true SU1635645A1 (en) 1999-08-10

Family

ID=60531564

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4623476/06A SU1635645A1 (en) 1988-12-22 1988-12-22 DRIVE OF GAS TURBINE INSTALLATION

Country Status (1)

Country Link
SU (1) SU1635645A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2204036C2 (en) * 2001-04-23 2003-05-10 Открытое акционерное общество "Авиадвигатель" Gas-turbine engine
RU2566173C1 (en) * 2014-06-17 2015-10-20 Юрий Фёдорович Ващенко Gas turbine engine multiplexer

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2204036C2 (en) * 2001-04-23 2003-05-10 Открытое акционерное общество "Авиадвигатель" Gas-turbine engine
RU2566173C1 (en) * 2014-06-17 2015-10-20 Юрий Фёдорович Ващенко Gas turbine engine multiplexer

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