FIELD: transport.
SUBSTANCE: fuselage comprises front section 2 with cabin, central section 4 and rear section 6. Fuselage central section 4, on the side of front section 2, has first zone 10 the width of which measured in lengthwise axis increases to maximum in direction from front section to rear section, second zone 12 with width decreasing, and third zone 14 behind second zone 12 of invariable width. Fuselage central section height measured in normal is invariable.
EFFECT: optimised aircraft weight and balance and aerodynamics.
9 cl, 19 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT FRONT WHEEL NACELLE | 2007 |
|
RU2467918C2 |
| OPTIMISED AIRCRAFT PASSENGER CABIN SET-UP | 2008 |
|
RU2517624C2 |
| COMMERCIAL AIRCRAFT | 2005 |
|
RU2392184C2 |
| ARRANGEMENT OF UPPER PART OF AIRCRAFT CABIN | 2005 |
|
RU2385825C2 |
| AIRCRAFT CABIN INNER LAYOUT | 2004 |
|
RU2347721C2 |
| BULKHEAD IN COCKPIT | 2006 |
|
RU2403186C2 |
| AIRCRAFT WITH LOW NOISE AT TAKE-OFF AND LANDING | 2006 |
|
RU2388651C2 |
| LUGGAGE RACK AND AIRCRAFT WITH SAID RACK | 2007 |
|
RU2456176C2 |
| AIRCRAFT WITH REDUCED ENVIRONMENT IMPACT | 2006 |
|
RU2384479C2 |
| AIRCRAFT POWER PLANT WITH ENGINE AND ATTACHMENT STRUT | 2006 |
|
RU2420430C2 |
