SU1407153A1 - TURBOCHARGER ENGINE - Google Patents

TURBOCHARGER ENGINE

Info

Publication number
SU1407153A1
SU1407153A1 SU4045549/06A SU4045549A SU1407153A1 SU 1407153 A1 SU1407153 A1 SU 1407153A1 SU 4045549/06 A SU4045549/06 A SU 4045549/06A SU 4045549 A SU4045549 A SU 4045549A SU 1407153 A1 SU1407153 A1 SU 1407153A1
Authority
SU
USSR - Soviet Union
Prior art keywords
pillars
windows
compressor
motor fan
blades
Prior art date
Application number
SU4045549/06A
Other languages
Russian (ru)
Inventor
Г.М. Горелов
В.Е. Резник
А.А. Бобух
С.В. Михайлов
Л.М. Гошев
В.А. Чистяков
Original Assignee
Г.М. Горелов
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 Г.М. Горелов filed Critical Г.М. Горелов
Priority to SU4045549/06A priority Critical patent/SU1407153A1/en
Application granted granted Critical
Publication of SU1407153A1 publication Critical patent/SU1407153A1/en

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  • Supercharger (AREA)

Abstract

1. Турбовинтовентиляторный двигатель, содержащий газогенератор с компрессором, соосный винтовентилятор с лопастями, силовую турбину, статор который снабжен окнами для прохода выхлопных газов, а винтовентилятор - концентрично расположенными наружными и внутренними обечайками, образующими кольцевой канал, сообщенный с окнами, и соединенными между собой при помощи полых стоек, причем внутренние обечайки снабжены стекателем, отличающийся тем, что, с целью повышения надежности, стойки выполнены с продольной сквозной щелью, а полость стоек подключена к компрессору.2. Двигатель по п.1, отличающийся тем, что стойки выполнены в виде профиля рабочей лопатки турбины.1. Turbopropfan engine containing a gas generator with a compressor, a coaxial motor fan with blades, a power turbine, a stator which is provided with windows for the passage of exhaust gases, and a motor fan with concentrically arranged outer and internal shells forming an annular channel connected to the windows and interconnected with each other hollow pillars, the inner shells being provided with a steamer, characterized in that, in order to increase reliability, the pillars are made with a longitudinal through slot, and the cavity of the pillars Connected to compressor.2. The engine according to claim 1, characterized in that the rack is made in the form of the profile of the working blades of the turbine.

SU4045549/06A 1986-03-28 1986-03-28 TURBOCHARGER ENGINE SU1407153A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4045549/06A SU1407153A1 (en) 1986-03-28 1986-03-28 TURBOCHARGER ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4045549/06A SU1407153A1 (en) 1986-03-28 1986-03-28 TURBOCHARGER ENGINE

Publications (1)

Publication Number Publication Date
SU1407153A1 true SU1407153A1 (en) 2005-09-20

Family

ID=60535767

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4045549/06A SU1407153A1 (en) 1986-03-28 1986-03-28 TURBOCHARGER ENGINE

Country Status (1)

Country Link
SU (1) SU1407153A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2449154C2 (en) * 2010-06-25 2012-04-27 Открытое акционерное общество "Авиадвигатель" Gas turbine propfan engine
RU2482311C1 (en) * 2011-12-14 2013-05-20 Открытое акционерное общество "Авиадвигатель" Gas turbine engine with aft location of open propeller fan
RU2672349C1 (en) * 2017-12-19 2018-11-13 Акционерное общество "Лётно-исследовательский институт имени М.М. Громова" Fairing-supercharger at inlet to air intake of compressor of turboprop-fan engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2449154C2 (en) * 2010-06-25 2012-04-27 Открытое акционерное общество "Авиадвигатель" Gas turbine propfan engine
RU2482311C1 (en) * 2011-12-14 2013-05-20 Открытое акционерное общество "Авиадвигатель" Gas turbine engine with aft location of open propeller fan
RU2672349C1 (en) * 2017-12-19 2018-11-13 Акционерное общество "Лётно-исследовательский институт имени М.М. Громова" Fairing-supercharger at inlet to air intake of compressor of turboprop-fan engine

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