FIELD: physics.
SUBSTANCE: proposed device consists of additional structure with sections with U-shape in crosswise cross section. Ends of said sections are furnished with lengthwise flanges incorporating appliance to joint hull plating to added structure, as well as to apply and absorb correcting forces. Crosswise flanges are arranged on boundary of added structure to apply and absorb test forces in six degrees of freedom. Added structure is made up of soft module made from composite materials. Said U-shaped section consists of horizontal straight segment and two ellipsoidal segments adjoining on each side to form sections of U-shape additional structure.
EFFECT: efficient plating testing device.
19 cl, 11 dwg
Title | Year | Author | Number |
---|---|---|---|
CONNECTOR FOR CONNECTION OF FUSELAGE SECTION, COMBINATION OF CONNECTOR AND, AT LEAST, ONE FUSELAGE SECTION, AND METHOD OF MAKING SAID CONNECTOR | 2008 |
|
RU2480372C2 |
SYSTEM OF AIRCRAFT FUSELAGE TWO SECTIONS AND CONNECTION STRUCTURE FOR FUSELAGE SKIN CONNECTION | 2008 |
|
RU2479466C2 |
FUSELAGE OF AIRCRAFT | 2018 |
|
RU2701899C1 |
LARGE-SIZED AERODYNAMIC MODEL | 2015 |
|
RU2607675C1 |
AIRCRAFT PRESSURE BULKHEAD ASSEMBLY STRUCTURE | 2010 |
|
RU2522538C2 |
JOINT BETWEEN AIRCRAFT FUSELAGE COMPARTMENTS AND ITS SEALED FRAME | 2011 |
|
RU2472670C1 |
AERODYNAMIC MODEL OF AIRCRAFT WITH INTEGRATED AIR BREATHING ENGINE | 2008 |
|
RU2370744C1 |
AIRCRAFT WING, AIRCRAFT WINGS CAISSON, CENTER WING, SPAR (VERSIONS) | 2019 |
|
RU2709976C1 |
FUSELAGE FLOOR BEARING CARCASS AND ITS SUPPORT BEAM | 2010 |
|
RU2440278C1 |
JOINT BETWEEN AIRCRAFT FUSELAGE COMPARTMENTS AND ITS SEALED FRAME | 2011 |
|
RU2472671C1 |
Authors
Dates
2011-03-27—Published
2007-03-27—Filed