公开(公告)号：US10906664B2

公开(公告)日：2021-02-02

申请号：US15523244

申请日：2015-10-28

Applicant: ACC Innovation AB

Inventor： Anders Ljung

IPC: B64D35/04 ,  B64C39/02 ,  A63H27/00 ,  B64D37/00

Abstract: Multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″) comprising, at least a first, second and third rotor 10, 20, 30, each rotatable by a dedicated first second and third hydraulic motor 11, 21, 31, a power unit 2, at least a first, second and third hydraulic pump 12, 22, 32 dedicated to the respective first, second and third hydraulic motor 11, 21, 31, wherein each hydraulic pump 12, 22, 32 is arranged to provide pressurized fluid to each hydraulic motor 11, 21, 31 for powering the hydraulic motor 11, 21, 31 and thereby rotating the respective rotor 10, 20, 30, a control unit 6 for controlling the operation of the multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″), wherein the control of the multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″) is arranged to be performed by altering the flow of pressurized fluid distributed to each respective hydraulic motor 11, 21, 31, wherein, wherein the flow of pressurized fluid provided to each hydraulic motor 11, 21, 31 is individually controllable by means of at least one control valve 13, 23, 33 configured to control the flow of pressurized fluid from each hydraulic pump 12, 22, 32 to its dedicated hydraulic motor 11, 21, 31.

公开(公告)号：US20180016022A1

公开(公告)日：2018-01-18

申请号：US15523244

申请日：2015-10-28

Applicant: ACC Innovation AB

Inventor： Anders Ljung

IPC: B64D35/04 ,  B64D37/00 ,  B64C39/02

CPC classification number: B64D35/04 ,  A63H27/12 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/04 ,  B64C2201/06 ,  B64C2201/108 ,  B64C2201/146 ,  B64C2201/148 ,  B64D37/00

Abstract: Multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″) comprising, at least a first, second and third rotor 10, 20, 30, each rotatable by a dedicated first second and third hydraulic motor 11, 21, 31, a power unit 2, at least a first, second and third hydraulic pump 12, 22, 32 dedicated to the respective first, second and third hydraulic motor 11, 21, 31, wherein each hydraulic pump 12, 22, 32 is arranged to provide pressurized fluid to each hydraulic motor 11, 21, 31 for powering the hydraulic motor 11, 21, 31 and thereby rotating the respective rotor 10, 20, 30, a control unit 6 for controlling the operation of the multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″), wherein the control of the multi-rotor aerial vehicle (1, 1′, 1″, 1′″, 1″″, 1″″′, 1″″″) is arranged to be performed by altering the flow of pressurized fluid distributed to each respective hydraulic motor 11, 21, 31, wherein, wherein the flow of pressurized fluid provided to each hydraulic motor 11, 21, 31 is individually controllable by means of at least one control valve 13, 23, 33 configured to control the flow of pressurized fluid from each hydraulic pump 12, 22, 32 to its dedicated hydraulic motor 11, 21, 31.

公开(公告)号：US12091165B2

公开(公告)日：2024-09-17

申请号：US16626226

申请日：2017-06-26

Applicant: ACC Innovation AB

Inventor： Anders Ljung

IPC: B64C27/14 ,  B64C27/08 ,  B64D35/04 ,  B64U10/10 ,  B64U30/20 ,  F16H7/02 ,  B64C39/02

CPC classification number: B64C27/14 ,  B64C27/08 ,  B64D35/04 ,  F16H7/02 ,  B64C39/024 ,  B64U10/10 ,  B64U30/20

Abstract: Rotor flight vehicle includes a first rotor, a power unit, a transmission from the power unit to the first rotor, wherein said transmission comprises at least one belt, a group of rotational axes, at least one power output axle connected to the power unit and at least one rotor axle connected to said first rotor, the belt is applied to the power output axle, the power output axle is concentric with a rotational axis, the belt transmits power to the rotor axle, the rotor axle is concentric with a rotational axis, wherein consecutive rotational axes of the group of rotational axes extend in a relation to each other such that the angle between them is in the range of 80-100 degrees, wherein the belt has a maximal torsion of 80-100 degrees, in the belt's transition between two respective consecutive rotational axes of the group of rotational axes.

公开(公告)号：US20240425175A1

公开(公告)日：2024-12-26

申请号：US18828933

申请日：2024-09-09

Applicant: ACC Innovation AB

Inventor： Anders Ljung

IPC: B64C27/14 ,  B64C27/08 ,  B64C39/02 ,  B64D35/04 ,  B64U10/10 ,  B64U10/13 ,  B64U30/20 ,  B64U30/24 ,  B64U50/19 ,  F16H7/02

Abstract: Rotor flight vehicle includes a first rotor, a power unit, a transmission from the power unit to the first rotor, wherein said transmission comprises at least one belt, a group of rotational axes, at least one power output axle connected to the power unit and at least one rotor axle connected to said first rotor, the belt is applied to the power output axle, the power output axle is concentric with a rotational axis, the belt transmits power to the rotor axle, the rotor axle is concentric with a rotational axis, wherein consecutive rotational axes of the group of rotational axes extend in a relation to each other such that the angle between them is in the range of 80-100 degrees, wherein the belt has a maximal torsion of 80-100 degrees, in the belt's transition between two respective consecutive rotational axes of the group of rotational axes.

公开(公告)号：USD920160S1

公开(公告)日：2021-05-25

申请号：US35507763

申请日：2019-04-17

Applicant: ACC Innovation AB

Designer： Anders Ljung