FIELD: transport.
SUBSTANCE: pod contains air inlet structure providing air flow direction to turbojet engine fan, and central structure including shroud (9) which encompasses the fan. The shroud encompasses the fan essentially up to its blades (8). The air inlet structure is connected with inner panel (41) using structural ring flange (15) made so that to provide holding of at least one blade in case when this blade breaks.
EFFECT: no sonic breaks and vibratory projections on the inner panel.
9 cl, 9 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TURBOJET NACELLE AIR INTAKE | 2009 |
|
RU2500585C2 |
| NACELLE AIR INTAKE WITH ACOUSTIC PANEL | 2020 |
|
RU2803661C2 |
| BEARING NACELLE | 2007 |
|
RU2424160C2 |
| NACELLE AIR INTAKE AND NACELLE CONTAINING SUCH AIR INTAKE | 2020 |
|
RU2801764C2 |
| NACELLE AIR INTAKE AND NACELLE CONTAINING SUCH AIR INTAKE | 2020 |
|
RU2804492C2 |
| AIR INTAKE HOUSING DESIGN | 2007 |
|
RU2433073C2 |
| GUIDE SYSTEM WITH LOCKING MEANS FOR NACELLE MOVING SECTION | 2008 |
|
RU2460674C2 |
| DETACHABLE AIR INTAKE FOR TURBOJET NACELLE | 2007 |
|
RU2451804C2 |
| AIR INTAKE FOR TURBOJET ENGINE NACELLE | 2020 |
|
RU2806229C2 |
| AIR-INTAKE STRUCTURE OF GONDOLA | 2009 |
|
RU2516899C2 |
