FIELD: transport.
SUBSTANCE: this invention relates to aircraft fuselage section 1 and to aircraft with said section. Fuselage section outer skin 4 comprises at least one door opening 5 divided vertically and at least one fuselage frame component 3 into multiple open areas 7. Cabin door may be fitted into door opening, flush with skin, to make fuselage load bearing element.
EFFECT: simplified design, wider door opening.
11 cl
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| AIRCRAFT FUSELAGE WITH CIRCULAR-ARC-OUTER CONTOUR | 2007 |
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RU2428351C2 |
| AIRCRAFT | 2000 |
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| AIRCRAFT | 2000 |
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| METHOD OF EMERGENCY EVACUATION OF PASSENGERS FROM AIRCRAFT | 2000 |
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RU2177441C2 |
| METHOD OF EMERGENCY EVACUATION OF PASSENGERS FROM AIRCRAFT | 2001 |
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RU2200688C2 |
| ACTIVE GLOVE BOX DOOR (EMBODIMENTS) AND INTERNAL STORAGE SYSTEM OF VEHICLE | 2016 |
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RU2710507C2 |
| AIRCRAFT | 1995 |
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RU2088477C1 |
| AIRCRAFT FUSELAGE | 2015 |
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RU2610151C1 |
| AIRCRAFT DOOR FRAME | 2007 |
|
RU2424945C2 |
