FIELD: transport.
SUBSTANCE: aircraft freight compartment floor 2 comprises central rails 8 and side rails 5 arranged on both sides of said central rails. Central rails 8 are rigidly attached to traverse 9. Side rails are secured to aircraft bearing structure solely by vertical levers 15. Freight compartment floor panels 18 are arranged between each pair of adjacent rails. Aircraft section 1 is furnished with said freight compartment floor 2. Said floor 2 is sued at aircraft section that comprises two undercarriage compartments that accommodate undercarriage main legs.
EFFECT: transmission of crosswise forces from side rails toward central rails.
10 cl, 8 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT FREIGHT COMPARTMENT FLOOR, APPLICATION OF SAID FLOOR AND AIRCRAFT SECTION PROVIDED WITH SUCH FLOOR | 2007 |
|
RU2499729C2 |
| FLOOR PANEL AND DEVICE TO FIX ELEMENTS OF EQUIPMENT COMPRISING SUCH PANELS | 2006 |
|
RU2413652C2 |
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|
RU2445233C2 |
| FLOOR SYSTEM FOR AIRCRAFT FUSELAGE SECTION | 2009 |
|
RU2494916C2 |
| AIRCRAFT FLOOR LOAD BEARING SET | 2007 |
|
RU2417906C2 |
| AIRCRAFT FLOOR HEATING DEVICE AND METHOD | 2004 |
|
RU2385827C2 |
| INNER SAFETY DOOR FOR AIRCRAFT | 2005 |
|
RU2403188C2 |
| AIRCRAFT FUSELAGE FLOOR STRUCTURAL SET | 2007 |
|
RU2438922C2 |
| HELICOPTER FUSELAGE | 1993 |
|
RU2090450C1 |
| AIRCRAFT STRUCTURAL ASSEMBLY | 2011 |
|
RU2576647C2 |
