RU2005129936A - TORQUE TRANSMISSION DEVICE FROM THE COMPRESSOR SHAFT TO THE GAS-TURBINE ENGINE DRIVE UNIT BOX - Google Patents

TORQUE TRANSMISSION DEVICE FROM THE COMPRESSOR SHAFT TO THE GAS-TURBINE ENGINE DRIVE UNIT BOX Download PDF

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Publication number
RU2005129936A
RU2005129936A RU2005129936/06A RU2005129936A RU2005129936A RU 2005129936 A RU2005129936 A RU 2005129936A RU 2005129936/06 A RU2005129936/06 A RU 2005129936/06A RU 2005129936 A RU2005129936 A RU 2005129936A RU 2005129936 A RU2005129936 A RU 2005129936A
Authority
RU
Russia
Prior art keywords
turbine engine
gas
drive unit
transmission device
compressor shaft
Prior art date
Application number
RU2005129936/06A
Other languages
Russian (ru)
Other versions
RU2302541C2 (en
Inventor
Александр Николаевич Семенов (RU)
Александр Николаевич Семенов
Юрий Абрамович Трубников (RU)
Юрий Абрамович Трубников
Виктор Павлович Герасимов (RU)
Виктор Павлович Герасимов
Александр Владимирович Мехоношин (RU)
Александр Владимирович Мехоношин
Алексей Викторович Микрюков (RU)
Алексей Викторович Микрюков
нов Владимир Алексеевич Ахмадз (RU)
Владимир Алексеевич Ахмадзянов
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 RU2005129936/06A priority Critical patent/RU2302541C2/en
Publication of RU2005129936A publication Critical patent/RU2005129936A/en
Application granted granted Critical
Publication of RU2302541C2 publication Critical patent/RU2302541C2/en

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  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Gear Transmission (AREA)

Claims (1)

Устройство передачи крутящего момента от вала компрессора к коробке приводных агрегатов газотурбинного двигателя, включающее прямозубое цилиндрическое колесо и коническую шестерню, отличающееся тем, что цилиндрическое колесо и коническая шестерня разнесены и соединены по посадочным поверхностям и шлицам, при этом коническая шестерня расположена на отдельной подшипниковой опоре, а во внутреннюю полость цилиндрического колеса установлен индуктор.A device for transmitting torque from the compressor shaft to the gearbox of the gas turbine engine, including a spur gear and bevel gear, characterized in that the cylindrical gear and bevel gear are spaced and connected along the seating surfaces and splines, while the bevel gear is located on a separate bearing support, and an inductor is installed in the inner cavity of the cylindrical wheel.
RU2005129936/06A 2005-09-26 2005-09-26 Device to transmit torque from compressor shaft to gas turbine engine auxiliaries RU2302541C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2005129936/06A RU2302541C2 (en) 2005-09-26 2005-09-26 Device to transmit torque from compressor shaft to gas turbine engine auxiliaries

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2005129936/06A RU2302541C2 (en) 2005-09-26 2005-09-26 Device to transmit torque from compressor shaft to gas turbine engine auxiliaries

Publications (2)

Publication Number Publication Date
RU2005129936A true RU2005129936A (en) 2007-04-10
RU2302541C2 RU2302541C2 (en) 2007-07-10

Family

ID=37999868

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2005129936/06A RU2302541C2 (en) 2005-09-26 2005-09-26 Device to transmit torque from compressor shaft to gas turbine engine auxiliaries

Country Status (1)

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RU (1) RU2302541C2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2920191B1 (en) * 2007-08-23 2013-11-22 Snecma GAS TURBINE ENGINE WITH DRIVING MEANS FOR THE ACCESSORIES HOUSING AND METHOD OF MOUNTING THE SAME
ITTO20130636A1 (en) 2013-07-29 2015-01-30 Avio Spa TRANSMISSION BOX, AND DISASSEMBLY METHOD TO DISCONNECT A DRIVE SHAFT IN SUCH A TRANSMISSION BOX
BR112016024852B1 (en) * 2014-04-29 2022-10-11 Safran Aircraft Engines MODULAR ASSEMBLY FOR A TURBO MACHINE

Also Published As

Publication number Publication date
RU2302541C2 (en) 2007-07-10

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

Effective date: 20090927