FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to turbojet nacelle attachments. Proposed assembly comprises two ledges that make the parts of casing end upstream of fixed outer structure end and downstream of casing rear end. Said ledges are located to contact with each other. Retention assembly comprises also two half-rings composed by the wall that confines the recess. Shape of said recess allows feeding of said ledges therein when casing and fixed outer structure are located to abut on. Ledges in said recess are retained by thrust means.
EFFECT: accelerated servicing, ease of servicing, minimised number of components and costs.
24 cl, 31 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| REAR FRAME FOR THRUST REVERSER, AIRCRAFT THRUST REVERSER FOR AIRCRAFT NACELLE AND NACELLE, EQUIPPED WITH SUCH THRUST REVERSER | 2015 |
|
RU2717173C2 |
| CONTROL SYSTEM FOR AIRCRAFT NACELLE SERVICING | 2009 |
|
RU2494927C2 |
| NACELLE FOR BYPASS TURBOJET ENGINE | 2007 |
|
RU2453477C2 |
| AIR INTAKE FOR AIRCRAFT NACELLE | 2009 |
|
RU2480598C2 |
| FRONT FRAME FOR THRUST REVERSER WITH DEFLECTING CASCADES | 2010 |
|
RU2542165C2 |
| TURBO-JET PLANT FOR AIRCRAFT | 2007 |
|
RU2436988C2 |
| ACCESSORY GEARBOX FOR GAS TURBINE ENGINE AND GAS TURBINE ENGINE | 2015 |
|
RU2684865C2 |
| PERCUSSION TOOL | 2010 |
|
RU2563417C2 |
| THRUST REVERSER DEVICE FIXED STRUCTURE AND TURBOJET ENGINE NACELLE HAVING SUCH DEVICE | 2013 |
|
RU2650982C2 |
| DOUBLE-STAGE TURBOFAN ENGINE | 2005 |
|
RU2415287C2 |
