FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to landing gear compartment and aircraft with such landing gear. Proposed compartment 20 comprises carcass (2, 3, 4, 5, 7, 8, 9) for attachment and taking up forces from landing gear, and envelopment structure jointed to said carcass to take up supercharging forces.
EFFECT: optimised forces acting on landing gear compartment.
16 cl, 8 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| LANDING GEAR COMPARTMENT WITH BOX STRUCTURE | 2006 |
|
RU2406651C2 |
| CHASSIS WITH FUSELAGE INSTALLATION | 2012 |
|
RU2617295C2 |
| AIRFRAME OF MULTIMODE MONOPLANE | 1997 |
|
RU2173654C2 |
| AIRCRAFT UNDERCARRIAGE INCORPORATING DRIVE WITH BRACE, AND AIRCRAFT WITH SUCH UNDERCARRIAGE | 2006 |
|
RU2424948C2 |
| FUSELAGE OF AIRCRAFT | 2018 |
|
RU2701899C1 |
| AIRPLANE AND METHOD OF ITS CONVERSION IN PARKING POSITION | 1992 |
|
RU2005663C1 |
| MULTI-PURPOSE HIGHLY MANOEUVRABLE SUPERSONIC AIRCRAFT, ITS AIRFRAME, EQUIPMENT AND SYSTEMS | 1996 |
|
RU2207968C2 |
| AIRCRAFT OR SPACECRAFT FUSELAGE FROM HYBRID COMPOSITION OF CARBON FIBER-REINFORCED PLASTIC/METAL WITH METAL FRAME | 2008 |
|
RU2446076C2 |
| LANDING GEAR COMPARTMENT OF REDUCED OVERALL DIMENSIONS | 2008 |
|
RU2465171C2 |
| AIRCRAFT WITH FOLDING WING AND WING FOLDING DEVICE | 2019 |
|
RU2727896C1 |
