Supporting wing structure for aircraft and aircraft having such supporting wing structure
The invention provides a wing group structure for an aircraft and the aircraft with the wing group structure. The invention also relates to a wing assembly (3) for an aircraft (1), in particular for acargo and/or passenger aircraft, preferably in the form of a vertical take-off and landing multi-rot...
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Format: | Patent |
Sprache: | chi ; eng |
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Zusammenfassung: | The invention provides a wing group structure for an aircraft and the aircraft with the wing group structure. The invention also relates to a wing assembly (3) for an aircraft (1), in particular for acargo and/or passenger aircraft, preferably in the form of a vertical take-off and landing multi-rotor aircraft having a plurality of distributed electric rotors (6), the wing group structure comprises a plurality of wing ribs (4, 4a, 4b), wherein the first number of ribs (4a) is arranged at least predominantly in a first direction (R1) and the second number of ribs (4b) is arranged at least predominantly in a second direction (R2) which is oriented orthogonally to the first direction (R1). The wing assembly (3) is characterized in that the cross-section of at least the second number of ribs(4b) has an aerodynamic profile, and/or the ribs (4, 4a, 4b) are connected to each other in pairs at least between adjacent ribs (4, 4a, 4b) by means of a connecting structure, preferably by means ofa separate connecting secti |
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