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.

公开(公告)号：WO2019180304A1

公开(公告)日：2019-09-26

申请号：PCT/FI2019/050134

申请日：2019-02-20

Applicant: LENTOLA LOGISTICS OY

Inventor： HOHENTHAL, Markus

IPC: B64C29/02

Abstract: A structure construction (100) for an aircraft (200) comprises first (101) and second (102) fuselage portions and at least one wing (103). In addition the structure construction (100) comprises a supporting structure (104) for supporting the wing (103) and the first fuselage portion (101). T h e supporting structure (104) or the wing (103) comprises also at least one engine (105). Additionally, the supporting structure (104) is configured to be hinged (106) to the second fuselage portion (102) so that said supporting structure (104) allows turning of said wing (103) and said first fuselage portion (101) in relation to said second fuselage portion (102) to a take-off and landing positions and forward flying position.

公开(公告)号：FI20185256A1

公开(公告)日：2019-09-21

申请号：FI20185256

申请日：2018-03-20

Applicant: LENTOLA LOGISTICS OY

Inventor： HOHENTHAL MARKUS

IPC: B64C1/26 ,  B64C29/00 ,  B64C37/00

Abstract: A structure construction (100) for an aircraft (200) comprises first (101) and second (102) fuselage portions and at least one wing (103). In addition the structure construction (100) comprises a supporting structure (104) for supporting the wing (103) and the first fuselage portion (101). The supporting structure (104) or the wing (103) comprises also at least one engine (105). Additionally the supporting structure (104) is configured to be hinged (106) to the second fuselage portion (102) so that said supporting structure (104) allows turning of said wing (103) and said first fuselage portion (101) in relation to said second fuselage portion (102) to a take-off and landing positions and forward flying position.

公开(公告)号：EP3768592A1

公开(公告)日：2021-01-27

申请号：EP19709082.2

申请日：2019-02-20

Applicant: Lentola Logistics Oy

Inventor： HOHENTHAL, Markus

IPC: B64C29/02

公开(公告)号：EP3209559A4

公开(公告)日：2018-06-13

申请号：EP15851788

申请日：2015-10-20

Applicant: LENTOLA LOGISTICS OY

Inventor： HOHENTHAL MARKUS

IPC: B64C29/02 ,  B64C39/02 ,  B64D27/24

CPC classification number: B64C29/02 ,  B64C39/024 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/104 ,  B64D27/24

Abstract: An electrically powered vertical takeoff and vertical landing (VTOL) aircraft, which comprises at least two main propellers, wherein the main propellers are adapted to generate at least 70% of the aircraft propulsion. The aircraft also comprises at least one adjustment propeller, which has its propeller slipstream adapted to produce a torque relative to a first axis or the first and second axes with respect to a fuselage of the aircraft for turning the aircraft relative to said first axis or said first and second axes. In addition, not less than 35%, but not more than 85%, of the aircraft's mass is adapted to lie, during takeoff and/or landing, on a rear side of a propeller line of said main propellers with respect to a nose of the aircraft.