SU1453997A1 - TURBOCHARGER ENGINE - Google Patents

TURBOCHARGER ENGINE

Info

Publication number
SU1453997A1
SU1453997A1 SU4215286/06A SU4215286A SU1453997A1 SU 1453997 A1 SU1453997 A1 SU 1453997A1 SU 4215286/06 A SU4215286/06 A SU 4215286/06A SU 4215286 A SU4215286 A SU 4215286A SU 1453997 A1 SU1453997 A1 SU 1453997A1
Authority
SU
USSR - Soviet Union
Prior art keywords
air intake
additional
intake housing
fixed
drive shaft
Prior art date
Application number
SU4215286/06A
Other languages
Russian (ru)
Inventor
Б.Д. Фишбейн
Л.М. Гошев
Original Assignee
Б.Д. Фишбейн
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 Б.Д. Фишбейн filed Critical Б.Д. Фишбейн
Priority to SU4215286/06A priority Critical patent/SU1453997A1/en
Application granted granted Critical
Publication of SU1453997A1 publication Critical patent/SU1453997A1/en

Links

Landscapes

  • Supercharger (AREA)

Abstract

1. Турбовентиляторный двигатель, содержащий воздухозаборник, расположенные в нем входной обтекатель и два нагнетательных венца, один из которых закреплен на внутренней поверхности корпуса воздухозаборника, и приводной вал, соединенный через редуктор с винтовентилятором, закрепленным на корпусе воздухозаборника, отличающийся тем, что, с целью повышения КПД, он снабжен дополнительным валом, соединенным с приводным валом, и редуктором, посредством которого второй нагнетательный венец подсоединен к дополнительному валу.2. Двигатель по п.1, отличающийся тем, что он снабжен дополнительным нагнетательным венцом, расположенным перед вторым нагнетательным венцом и закрепленным на внутренней поверхности корпуса воздухозаборника и входном обтекателе.1. A turbofan engine containing an air intake, an inlet fairing located therein and two pressure rings, one of which is fixed to the inner surface of the air intake housing, and a drive shaft connected through a reducer to a fan drive mounted on the air intake housing, characterized in that increase efficiency, it is equipped with an additional shaft connected to the drive shaft, and a gearbox, through which the second discharge ring is connected to an additional shaft. The engine according to claim 1, characterized in that it is provided with an additional discharge ring located in front of the second injection ring and fixed to the inner surface of the air intake housing and the inlet fairing.

SU4215286/06A 1987-03-24 1987-03-24 TURBOCHARGER ENGINE SU1453997A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4215286/06A SU1453997A1 (en) 1987-03-24 1987-03-24 TURBOCHARGER ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4215286/06A SU1453997A1 (en) 1987-03-24 1987-03-24 TURBOCHARGER ENGINE

Publications (1)

Publication Number Publication Date
SU1453997A1 true SU1453997A1 (en) 2005-10-10

Family

ID=60536459

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4215286/06A SU1453997A1 (en) 1987-03-24 1987-03-24 TURBOCHARGER ENGINE

Country Status (1)

Country Link
SU (1) SU1453997A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2482311C1 (en) * 2011-12-14 2013-05-20 Открытое акционерное общество "Авиадвигатель" Gas turbine engine with aft location of open propeller fan

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2482311C1 (en) * 2011-12-14 2013-05-20 Открытое акционерное общество "Авиадвигатель" Gas turbine engine with aft location of open propeller fan

Similar Documents

Publication Publication Date Title
ES2006348A6 (en) Fuel pump for an internal combustion engine having two pump units
JPS6469716A (en) Supercharger
GB1497477A (en) Gas turbine engine
SE7607267L (en) GASTURBINE ENGINE
MY108711A (en) Rotary jet engine
DE68925977D1 (en) TURBOCHARGER
JPS5529094A (en) Oil pump
DE3880535D1 (en) GAS TURBINE SYSTEM FOR HELICOPTERS.
SE8406093D0 (en) ACCESSORY DRIVE FOR A TURBINE ENGINE
SU1453997A1 (en) TURBOCHARGER ENGINE
GB874902A (en) Improvements relating to power units
GB2014663A (en) Gas Turbine Ducted Fan Engine
JPS57159920A (en) Intake device for engine with turbocharger
SU708070A1 (en) Centrifugal fan
ES8507224A1 (en) Turbo composite engine device
RU93006617A (en) RING FLASH CHAMBER OF A GAS TURBINE ENGINE
GB1014870A (en) Improvements in air induction system for a gas turbine engine
JPS57191493A (en) Mechanical seal for water pump
JPS5746012A (en) Cooling device of supercharger for engine
SU1832859A1 (en) Rocket engine
RU96107452A (en) ADVANCED DIRECT ROTARY ENGINE
SU1827985A1 (en) COUPLING FRONT LOCATION
FR2434285A1 (en) COMPRESSOR SYSTEM FOR A TURBO-ENGINE AND TURBO-MACHINE COMPRISING SUCH A COMPRESSOR SYSTEM
SU1407186A1 (en) COMBUSTION CHAMBER OF A GAS TURBINE ENGINE
JPS5746026A (en) Motorcycle employing multicylinder engine with supercharger