FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft tail. Aircraft tail comprises engine attachment structure 14 extending through fuselage first and second openings 18, 18'. Said structure comprises means to attach it to fuselage 6 and including first fasteners connecting the structure to first frame 50 making the first opening 18 and second fasteners to connect it to frame 50 to make second opening 18'. In compliance with this invention, every said fastener comprises said compression interlocking link 90, 92 to rest on frame 50, on one side, and in attachment structure 14, on opposite side.
EFFECT: simplified design, lower weight.
10 cl, 12 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT TAIL COMPRISING ENGINE ATTACHMENTS EXTENDING THROUGH FUSELAGE AND CONNECTED THEREWITH BY AT LEAST ONE LINK | 2009 |
|
RU2496684C2 |
| AIRCRAFT TAIL AND METHOD OF ITS ASSEMBLY | 2009 |
|
RU2501711C2 |
| AIRCRAFT WITH FOLDABLE REAR DOOR | 2015 |
|
RU2622518C1 |
| HELICOPTER FUSELAGE | 1993 |
|
RU2090450C1 |
| SEARCH-AND-RESCUE AIRCRAFT | 2007 |
|
RU2337855C1 |
| AIRCRAFT POWER PLANT COMPRISING ENGINE SUSPENSION ASSEMBLIES SHIFTED DOWNWARD AT BLOWER HOUSING | 2009 |
|
RU2487057C2 |
| FRAME OF OPENING MADE IN AIRCRAFT FUSELAGE | 2010 |
|
RU2532010C2 |
| FLIGHT VEHICLE (VERSIONS), FLIGHT VEHICLES PARTS, METHOD OF EXPLOITING FLIGHT VEHICLE AND ITS PARTS | 2010 |
|
RU2466061C2 |
| BENCH TO TEST AIRCRAFT HATCH | 2010 |
|
RU2444715C1 |
| AIRCRAFT POWER PLANT BUILT AROUND TURBOJET WITH REINFORCING STRUCTURES CONNECTING FAN CASE WITH CENTRAL HOUSING | 2009 |
|
RU2485022C2 |
