RU2004112290A - TURBOJET - Google Patents

TURBOJET Download PDF

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Publication number
RU2004112290A
RU2004112290A RU2004112290/06A RU2004112290A RU2004112290A RU 2004112290 A RU2004112290 A RU 2004112290A RU 2004112290/06 A RU2004112290/06 A RU 2004112290/06A RU 2004112290 A RU2004112290 A RU 2004112290A RU 2004112290 A RU2004112290 A RU 2004112290A
Authority
RU
Russia
Prior art keywords
gear
helical
reversing mechanism
compressor
rotors
Prior art date
Application number
RU2004112290/06A
Other languages
Russian (ru)
Other versions
RU2264553C1 (en
Inventor
Виктор Сергеевич Лугин (RU)
Виктор Сергеевич Лугиня
Софь Владимировна Маркова (RU)
Софья Владимировна Маркова
Александр Григорьевич Пайкин (RU)
Александр Григорьевич Пайкин
Александр Владимирович Белов (RU)
Александр Владимирович Белов
Николай Маркович Билык (RU)
Николай Маркович Билык
Николай Сергеевич Винокуров (RU)
Николай Сергеевич Винокуров
Владимир Анатольевич Никифоров (RU)
Владимир Анатольевич Никифоров
Original Assignee
ЗАО "Энергетика" (RU)
ЗАО "Энергетика"
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 ЗАО "Энергетика" (RU), ЗАО "Энергетика" filed Critical ЗАО "Энергетика" (RU)
Priority to RU2004112290/06A priority Critical patent/RU2264553C1/en
Publication of RU2004112290A publication Critical patent/RU2004112290A/en
Application granted granted Critical
Publication of RU2264553C1 publication Critical patent/RU2264553C1/en

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Claims (1)

Турбореактивный двигатель, содержащий соосно последовательно установленные в корпусе регулируемый воздухозаборник, осевой компрессор и газовую турбину, роторы которых укреплены на валах, связанных между собой зубчатым механизмом реверсирования, а также камеру сгорания и реактивное сопло, отличающийся тем, что зубчатый механизм реверсирования выполнен в виде планетарного редуктора, ведущее зубчатое колесо которого, закрепленное на валу турбины, связано косозубым зацеплением с автономно расположенными в неподвижных опорах сателитными шестернями, торцевая ступень которых кинематически замкнута с закрепленным на обойме вала компрессора ведомым зубчатым колесом внутреннего зацепления, образуя косозубую передачу противоположного направления вышеупомянутой косозубой передачи ведущее колесо - сателитные шестерни.A turbojet engine containing an adjustable air intake coaxially mounted in series in the housing, an axial compressor and a gas turbine, the rotors of which are mounted on shafts interconnected by a gear reversing mechanism, as well as a combustion chamber and a jet nozzle, characterized in that the gear reversing mechanism is made in the form of a planetary a gearbox, the drive gear of which is mounted on the turbine shaft, is connected by helical gearing with the satellite and gears, the end stage of which is closed with kinematically attached to cage compressor shaft driven gear with internal engagement, forming a helical direction of transmission opposite the aforementioned helical transfer drive wheel - gear SAT.
RU2004112290/06A 2004-04-23 2004-04-23 Turbojet engine RU2264553C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2004112290/06A RU2264553C1 (en) 2004-04-23 2004-04-23 Turbojet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2004112290/06A RU2264553C1 (en) 2004-04-23 2004-04-23 Turbojet engine

Publications (2)

Publication Number Publication Date
RU2004112290A true RU2004112290A (en) 2005-10-20
RU2264553C1 RU2264553C1 (en) 2005-11-20

Family

ID=35862886

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2004112290/06A RU2264553C1 (en) 2004-04-23 2004-04-23 Turbojet engine

Country Status (1)

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RU (1) RU2264553C1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7841165B2 (en) * 2006-10-31 2010-11-30 General Electric Company Gas turbine engine assembly and methods of assembling same
RU2582385C2 (en) * 2014-03-11 2016-04-27 Юрий Михайлович Финк Finca turboshaft engine

Also Published As

Publication number Publication date
RU2264553C1 (en) 2005-11-20

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Legal Events

Date Code Title Description
PD4A Correction of name of patent owner
PC41 Official registration of the transfer of exclusive right

Effective date: 20181225

MM4A The patent is invalid due to non-payment of fees

Effective date: 20200424