FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed engine plat comprises turbojet engine 1 and heat exchanger 13 arranged above said engine to bleed cooling airflow 7 and hot airflow in turbojet engine. Cooling airflow and hot airflow bleed surfaces are oriented toward turbojet engine front part and feature normal lines (n1, n2) inclined to turbojet engine axis A. Aircraft incorporates above describe engine plant.
EFFECT: reduced overall dimensions.
8 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| POWER PLANT AND AIRCRAFT CONTAINING SUCH POWER PLANT | 2006 |
|
RU2413086C2 |
| AIRCRAFT POWER PLANT COMPRISING ENGINE AND ENGINE ATTACHMENT POST | 2006 |
|
RU2394730C2 |
| AIRCRAFT POWER PLANT WITH ENGINE AND ATTACHMENT STRUT | 2006 |
|
RU2420430C2 |
| AIRCRAFT TURBOJET ENGINE PYLON | 2006 |
|
RU2400401C2 |
| AIRCRAFT POWER PLANT COMPRISING ENGINE AND ENGINE PYLON | 2006 |
|
RU2401222C2 |
| AIRCRAFT ENGINE UNIT | 2008 |
|
RU2469917C2 |
| AIRCRAFT ENGINE ASSEMBLY UNIT | 2005 |
|
RU2381148C2 |
| TURBO-JET PLANT FOR AIRCRAFT | 2007 |
|
RU2436988C2 |
| TURBOJET HINGED TO AIRCRAFT PYLON | 2008 |
|
RU2487056C2 |
| AIRCRAFT ENGINE ASSEMBLY | 2005 |
|
RU2381149C2 |
