FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering. Design of the connection of console (1) wing with the fuselage is equipped with box-shaped beam (6) and contains a duct consisting of outer (7) and inner (8) longitudinal walls connected to upper (9) and lower (10) panels. Inside the box there are power frames (11). Each of spars (12) of console (1) of the wing is fixed (13) on power frame (11) of box girder (6), respectively. Ends (14, 15) of the box girder box are rigidly connected to power frames (16, 17) of the fuselage with the formation of a closed fuselage contour.
EFFECT: invention is aimed at increasing the functional space of the fuselage.
4 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRFRAME OF MULTIMODE MONOPLANE | 1997 |
|
RU2173654C2 |
FUSELAGE CENTRAL PART AND BEAM | 2010 |
|
RU2443599C1 |
AIRCRAFT WING, AIRCRAFT WINGS CAISSON, CENTER WING, SPAR (VERSIONS) | 2019 |
|
RU2709976C1 |
AIRCRAFT WING | 2014 |
|
RU2557638C1 |
HELICOPTER FUSELAGE | 2004 |
|
RU2278059C1 |
AIRCRAFT WING AND OUTER WING JOINT ASSEMBLY | 2012 |
|
RU2481243C1 |
AIRFRAME OF MULTIPURPOSE CLASS VI AIRCRAFT | 2010 |
|
RU2462395C2 |
MULTI-PURPOSE HIGHLY MANOEUVRABLE SUPERSONIC AIRCRAFT, ITS AIRFRAME, EQUIPMENT AND SYSTEMS | 1996 |
|
RU2207968C2 |
AIRCRAFT AIRFRAME | 2008 |
|
RU2391251C2 |
CONNECTION OF WING AND FUSELAGE | 1998 |
|
RU2154003C2 |
Authors
Dates
2019-03-20—Published
2018-02-15—Filed