AIRPLANE
The invention provides a junction of metal/composite structures of an airplane where in a former (2) of the airplane fuselage (4) a girder (1) is seated and coupled, to which bearing elements of the airplane are mounted, such as wings or elements of flight controls of the airplane, in particular a s...
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| Format: | Patent |
| Sprache: | eng ; fre ; ger |
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| Zusammenfassung: | The invention provides a junction of metal/composite structures of an airplane where in a former (2) of the airplane fuselage (4) a girder (1) is seated and coupled, to which bearing elements of the airplane are mounted, such as wings or elements of flight controls of the airplane, in particular a small plane.A junction is characterized in that in the former (2) of the airplane fuselage (4) an insert (3) is positioned that has an outer shape that represents the inner shape of the former (2) of the fuselage (4) and its inner shape represents the outer shape of an end of the girder (1), where the height of the insert (3) as measured along an opening in the former (2) corresponds to at most a half od he depth of the opening in the former (2). |
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