SU1804042A1 - Engine heat exchanger cooling system - Google Patents
Engine heat exchanger cooling systemInfo
- Publication number
- SU1804042A1 SU1804042A1 SU4922173/23A SU4922173A SU1804042A1 SU 1804042 A1 SU1804042 A1 SU 1804042A1 SU 4922173/23 A SU4922173/23 A SU 4922173/23A SU 4922173 A SU4922173 A SU 4922173A SU 1804042 A1 SU1804042 A1 SU 1804042A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- heat exchanger
- ejector
- stage
- cooling system
- cooling
- Prior art date
Links
Abstract
FIELD: aeronautical engineering. SUBSTANCE: heat exchanger cooling system consists of front inlet tunnel 1 and rear outlet tunnel 2 between which heat exchanger, adjusting gate and two-stage ejector are mounted. Ejector has first stage 7 and second stage 10. At high ambient temperature, for example during ground hold, air from engine compressor flows to ejector through branch pipe and causes intensified flow of cooling air through heat exchanger. During flight, heat exchanger is blown off due to velocity head. EFFECT: enhanced efficiency of cooling due to blowing of heat exchanger and reduced mass of device. 2 cl, 6 dwg
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4922173/23A SU1804042A1 (en) | 1991-03-28 | 1991-03-28 | Engine heat exchanger cooling system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4922173/23A SU1804042A1 (en) | 1991-03-28 | 1991-03-28 | Engine heat exchanger cooling system |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1804042A1 true SU1804042A1 (en) | 1994-01-15 |
Family
ID=60536843
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU4922173/23A SU1804042A1 (en) | 1991-03-28 | 1991-03-28 | Engine heat exchanger cooling system |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1804042A1 (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2470840C1 (en) * | 2008-10-07 | 2012-12-27 | Эрбюс Операсьон (Сас) | Aircraft air intake assembly |
RU2471682C2 (en) * | 2007-06-25 | 2013-01-10 | ЭРБЮС ОПЕРАСЬОН (сосьете пар аксьон семплифье) | Turbojet engine for airborne vehicle |
RU2587733C1 (en) * | 2015-01-13 | 2016-06-20 | Открытое акционерное общество "Научно-производственное предприятие "Аэросила" | Ejector oil cooling system in power plant |
RU2635001C2 (en) * | 2012-02-01 | 2017-11-08 | Турбомека | Method for discharging exhaust gases from gas turbine and exhaust system having optimised configuration |
RU2753385C1 (en) * | 2018-06-18 | 2021-08-13 | НУОВО ПИНЬОНЕ ТЕКНОЛОДЖИ - С.р.л. | Ventilation system for bearing oil cavity |
RU2753738C2 (en) * | 2014-11-25 | 2021-08-23 | Сафран Эркрафт Энджинз | Cooling device for turbomachine provided with unloading circuit |
-
1991
- 1991-03-28 SU SU4922173/23A patent/SU1804042A1/en active
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2471682C2 (en) * | 2007-06-25 | 2013-01-10 | ЭРБЮС ОПЕРАСЬОН (сосьете пар аксьон семплифье) | Turbojet engine for airborne vehicle |
RU2470840C1 (en) * | 2008-10-07 | 2012-12-27 | Эрбюс Операсьон (Сас) | Aircraft air intake assembly |
RU2635001C2 (en) * | 2012-02-01 | 2017-11-08 | Турбомека | Method for discharging exhaust gases from gas turbine and exhaust system having optimised configuration |
RU2753738C2 (en) * | 2014-11-25 | 2021-08-23 | Сафран Эркрафт Энджинз | Cooling device for turbomachine provided with unloading circuit |
RU2587733C1 (en) * | 2015-01-13 | 2016-06-20 | Открытое акционерное общество "Научно-производственное предприятие "Аэросила" | Ejector oil cooling system in power plant |
RU2753385C1 (en) * | 2018-06-18 | 2021-08-13 | НУОВО ПИНЬОНЕ ТЕКНОЛОДЖИ - С.р.л. | Ventilation system for bearing oil cavity |
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