公开(公告)号：US20210016877A1

公开(公告)日：2021-01-21

申请号：US16979888

申请日：2019-02-20

Applicant: LENTOLA LOGISTICS OY

Inventor： Markus Hohenthal

IPC: B64C29/00 ,  B64C1/06 ,  B64C1/26 ,  B64D27/02 ,  B64C3/38 ,  B64C25/60 ,  B64D11/00 ,  B64D27/24 ,  B64D31/00

Abstract: A structure construction for an aircraft includes first and second fuselage portions and at least one wing. In addition, the structure construction includes a supporting structure for supporting the wing and the first fuselage portion. The supporting structure or the wing also includes at least one engine, Additionally, the supporting structure is configured to be hinged to the second fuselage portion so that the supporting structure allows turning of the wing and the first fuselage portion in relation to the second fuselage portion during take-off, landing positions and forward flying position.