FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to aircraft air intake assembly. Proposed assy comprises air intake structure with air intake edge 7 and acoustic jacket 5 extending downward from said edge 7 that is intended for installation at fixed structural element 2. Said air intake structure can displace relative to fixed structural element 2 between working position whereat said edge 7 contacts with said jacket 5 and servicing position whereat said edge 7 is displaced upward from said jacket 5. Said assy includes rolling means 19 to center said edge 7 with respect to said jacket 5..
EFFECT: optimised clearance between air intake assy and other nacelle elements.
15 cl, 17 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TURBOJET NACELLE AIR INTAKE | 2009 |
|
RU2500585C2 |
| TURBOJET NACELLE | 2010 |
|
RU2524321C2 |
| AIR-INTAKE STRUCTURE OF GONDOLA | 2009 |
|
RU2516899C2 |
| THRUST REVERSER | 2010 |
|
RU2546132C2 |
| AIRCRAFT TURBOJET SUPPORT STRUT AND NACELLE WITH SUCH STRUT | 2009 |
|
RU2500584C2 |
| ATTACHMENT OF TURBOJET ENGINE GONDOLA STRUCTURAL ELEMENT USING REINFORCED CONNECTION OF "BLADE BEARING - GROOVE" TYPE | 2008 |
|
RU2463214C2 |
| AERODYNAMIC ELEMENT FOR AIRCRAFT NACELLE | 2011 |
|
RU2571981C2 |
| AIRCRAFT POWER PLANT AND ITS AIR INTAKE | 2009 |
|
RU2537998C2 |
| NACELLE AIR INTAKE AND NACELLE CONTAINING SUCH AIR INTAKE | 2020 |
|
RU2802275C2 |
| DEVICE TO CENTRE AIR INTAKE SECTION RELATIVE TO NACELLE MID SECTION | 2009 |
|
RU2500587C2 |
