SU1635643A1 - COOLING DEVICE FOR LIQUID SYSTEMS OF A REACTIVE ENGINE - Google Patents

COOLING DEVICE FOR LIQUID SYSTEMS OF A REACTIVE ENGINE

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Publication number
SU1635643A1
SU1635643A1 SU4499879/23A SU4499879A SU1635643A1 SU 1635643 A1 SU1635643 A1 SU 1635643A1 SU 4499879/23 A SU4499879/23 A SU 4499879/23A SU 4499879 A SU4499879 A SU 4499879A SU 1635643 A1 SU1635643 A1 SU 1635643A1
Authority
SU
USSR - Soviet Union
Prior art keywords
heat exchanger
engine
cooling device
cochlea
liquid systems
Prior art date
Application number
SU4499879/23A
Other languages
Russian (ru)
Inventor
В.А. Карпенко
Е.Б. Ермилов
И.В. Путин
Г.А. Игнатенко
Original Assignee
В.А. Карпенко
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 В.А. Карпенко filed Critical В.А. Карпенко
Priority to SU4499879/23A priority Critical patent/SU1635643A1/en
Application granted granted Critical
Publication of SU1635643A1 publication Critical patent/SU1635643A1/en

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  • Jet Pumps And Other Pumps (AREA)

Abstract

Устройство для охлаждения жидкостных систем реактивного двигателя, включающее теплообменник, систему жидкостных коммуникаций, воздухозаборник, воздухоотводящий канал, выходной туннель теплообменника, отличающееся тем, что, с целью упрощения конструкции и повышения надежности устройства путем использования снижения статического давления в канале воздухозаборника двигателя на земле и скоростного напора в полете, участок канала воздухозаборника двигателя выполнен перфорированным и снабжен кольцевой камерой-улиткой, а выходной туннель теплообменника снабжен управляемой заслонкой и через патрубок соединен с кольцевой камерой-улиткой.Device for cooling liquid jet engine systems, including a heat exchanger, liquid communications system, air intake, air outlet channel, heat exchanger outlet tunnel, characterized in that, in order to simplify the design and increase the reliability of the device by using the reduction of static pressure in the engine air inlet channel on the ground and high-speed head in flight, the portion of the air intake channel of the engine is made perforated and provided with an annular chamber-cochlea, and the output tunnel The heat exchanger is equipped with a controlled damper and is connected to the annular cochlea through a nozzle.

SU4499879/23A 1988-10-31 1988-10-31 COOLING DEVICE FOR LIQUID SYSTEMS OF A REACTIVE ENGINE SU1635643A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4499879/23A SU1635643A1 (en) 1988-10-31 1988-10-31 COOLING DEVICE FOR LIQUID SYSTEMS OF A REACTIVE ENGINE

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4499879/23A SU1635643A1 (en) 1988-10-31 1988-10-31 COOLING DEVICE FOR LIQUID SYSTEMS OF A REACTIVE ENGINE

Publications (1)

Publication Number Publication Date
SU1635643A1 true SU1635643A1 (en) 2004-10-27

Family

ID=60530235

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4499879/23A SU1635643A1 (en) 1988-10-31 1988-10-31 COOLING DEVICE FOR LIQUID SYSTEMS OF A REACTIVE ENGINE

Country Status (1)

Country Link
SU (1) SU1635643A1 (en)

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