FIELD: engines and pumps.
SUBSTANCE: turbo-jet plant for aircraft includes engine installed in nacelle and heat exchanger intended to cool the fluid medium used in power system of the engine. Heat exchanger is located on the level of outer wall of engine; at that, between outer engine wall and lower engine wall there left is intermediate space for air circulation.
EFFECT: reducing aerodynamic losses inside the engine path.
10 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TURBOJET ENGINE FOR AIRBORNE VEHICLE | 2008 |
|
RU2471682C2 |
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|
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| NACELLE FOR BYPASS TURBOJET ENGINE | 2007 |
|
RU2453477C2 |
| DEVICE TO COOL TWO-CIRCUIT TURBOJET ENGINE FIRST CIRCUIT | 2005 |
|
RU2397350C2 |
