FIELD: aircraft structural members.
SUBSTANCE: proposed aircraft structural member includes sheets of skin and several rigidity profiles connected with skin section by weld seam. Rigidity profiles have rigidity members formed by duplicating components made in form of I-profiles; each of them is located on sections of profile struts on at least one side. Rigidity members may be formed by tie rods mounted on sections of profile struts which have thickened areas of material with holes for introducing the tie rods.
EFFECT: enhanced residual strength; cut costs.
15 cl, 10 dwg
Title | Year | Author | Number |
---|---|---|---|
METAL STRUCTURAL MEMBER OF SKIN | 2000 |
|
RU2249538C2 |
SYSTEM OF AIRCRAFT FUSELAGE TWO SECTIONS AND CONNECTION STRUCTURE FOR FUSELAGE SKIN CONNECTION | 2008 |
|
RU2479466C2 |
CONNECTOR FOR CONNECTION OF FUSELAGE SECTION, COMBINATION OF CONNECTOR AND, AT LEAST, ONE FUSELAGE SECTION, AND METHOD OF MAKING SAID CONNECTOR | 2008 |
|
RU2480372C2 |
AIRFRAME OF MULTIMODE MONOPLANE | 1997 |
|
RU2173654C2 |
HYBRID AIRCRAFT FUSELAGE CELL STRUCTURE | 2010 |
|
RU2482995C1 |
JOINT BETWEEN AIRCRAFT FUSELAGE COMPARTMENTS AND ITS SEALED FRAME | 2011 |
|
RU2472671C1 |
FLYING VEHICLE FUSELAGE | 2004 |
|
RU2270135C2 |
JOINT BETWEEN AIRCRAFT FUSELAGE COMPARTMENTS AND ITS SEALED FRAME | 2011 |
|
RU2472670C1 |
AIRCRAFT OR SPACECRAFT STRUCTURAL COMPONENT AND AIRFRAME | 2008 |
|
RU2475411C2 |
AIRCRAFT BAGGAGE COMPARTMENT | 1992 |
|
RU2007330C1 |
Authors
Dates
2006-03-10—Published
2001-06-26—Filed