SU828586A1 - ENGINE PLANE INSTALLATION - Google Patents

ENGINE PLANE INSTALLATION

Info

Publication number
SU828586A1
SU828586A1 SU2873038/06A SU2873038A SU828586A1 SU 828586 A1 SU828586 A1 SU 828586A1 SU 2873038/06 A SU2873038/06 A SU 2873038/06A SU 2873038 A SU2873038 A SU 2873038A SU 828586 A1 SU828586 A1 SU 828586A1
Authority
SU
USSR - Soviet Union
Prior art keywords
engine
plane installation
cavity
gap
engine plane
Prior art date
Application number
SU2873038/06A
Other languages
Russian (ru)
Inventor
Е.М. Семенов
Г.М. Горелов
В.Е. Резник
В.П. Данильченко
М.М. Пирский
Г.А. Тетюшин
А.А. Бобух
Н.Б. Болотин
А.Э. Брейво
Б.Д. Фишбейн
E.M. Semenov
G.M. Gorelov
V.E. Reznik
V.P. Danil'chenko
M.M. Pirskij
G.A. Tetjushin
A.A. Bobukh
N.B. Bolotin
A.Eh. Brejvo
B.D. Fishbejn
Original Assignee
Е.М. Семенов
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 Е.М. Семенов filed Critical Е.М. Семенов
Priority to SU2873038/06A priority Critical patent/SU828586A1/en
Application granted granted Critical
Publication of SU828586A1 publication Critical patent/SU828586A1/en

Links

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Двигательная установка самолета, содержащая мотогондолу и размещенный в ней с образованием кольцевой полости двухконтурный турбореактивный двигатель, над корпусом турбины которого между его фланцами закреплен перфорированный кожух, образующий с корпусом кольцевой зазор, отличающаяся тем, что, с целью повышения надежности и экономичности, в наружном контуре двигателя установлены полые стойки, сообщенные с зазором и полостью и снабженные со стороны последней регулируемыми клапанами.The propulsion system of the aircraft, containing the engine nacelle and placed in it with the formation of the annular cavity, is a double-circuit turbojet engine, above the turbine casing of which between its flanges a perforated casing is fixed, forming an annular gap with the case, in order to increase reliability and efficiency, in the outer contour engine mounted hollow rack, communicated with a gap and cavity and provided with the last adjustable valves.

SU2873038/06A 1980-01-24 1980-01-24 ENGINE PLANE INSTALLATION SU828586A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2873038/06A SU828586A1 (en) 1980-01-24 1980-01-24 ENGINE PLANE INSTALLATION

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2873038/06A SU828586A1 (en) 1980-01-24 1980-01-24 ENGINE PLANE INSTALLATION

Publications (1)

Publication Number Publication Date
SU828586A1 true SU828586A1 (en) 2005-11-27

Family

ID=60525293

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2873038/06A SU828586A1 (en) 1980-01-24 1980-01-24 ENGINE PLANE INSTALLATION

Country Status (1)

Country Link
SU (1) SU828586A1 (en)

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