公开(公告)号：US20120160955A1

公开(公告)日：2012-06-28

申请号：US13332460

申请日：2011-12-21

Applicant: Jost SEIFERT

Inventor： Jost SEIFERT

IPC: B64C39/00 ,  B64C27/00

CPC classification number: B64C39/005

Abstract: A hybrid rotor for an aircraft includes a Magnus rotor rotatable around a Magnus rotor axis and a transverse flow rotor that is kept rotating around an axis of rotation and has a number of axially extending rotor blades that are actuatable to rotate around the axis of rotation and are configured stationary relative to the tangential angle position. The Magnus rotor is located within the transverse flow rotor and has an axis extending in the direction of the axis of rotation. The guide mechanism has a housing segment partially surrounding the transverse flow rotor in the circumferential direction. The housing segment has an adjustment mechanism and is deflectable relative to the Magnus rotor axis. The housing segment is aligned such that the transverse flow rotor generates a propulsion force and causes a transverse flow onto the Magnus rotor to generate lifting force by way of a Magnus effect.

Abstract translation: 用于飞行器的混合转子包括可围绕马格努斯转子轴线旋转的马格努斯转子和沿着旋转轴线保持旋转的横向流动转子，并且具有若干可轴向延伸的转子叶片，该转子叶片可致动以围绕旋转轴线旋转， 相对于切向角位置固定。 Magnus转子位于横向流动转子内，并具有沿旋转轴线方向延伸的轴线。 引导机构具有沿圆周方向部分地围绕横向流动转子的壳体段。 壳体段具有调节机构，并且相对于Magnus转子轴线是可偏转的。 壳体段被对准使得横向流动转子产生推进力并且使横向流动到马格努斯转子上以通过马格努斯效应产生提升力。

公开(公告)号：US20120161447A1

公开(公告)日：2012-06-28

申请号：US13333174

申请日：2011-12-21

Applicant: Jost SEIFERT

Inventor： Jost SEIFERT

IPC: F03D9/00 ,  F03D7/00 ,  F03D3/04

CPC classification number: F03D3/007 ,  F03D3/002 ,  F03D3/005 ,  F03D3/02 ,  F03D3/04 ,  F03D9/00 ,  F03D9/25 ,  F05B2240/201 ,  F05B2240/212 ,  F05B2240/214 ,  Y02B10/30 ,  Y02E10/74

Abstract: A wind power hybrid rotor of a wind power plant for converting wind energy into drive energy is provided. For a utilization of the wind energy in a manner as efficient as possible, a wind power hybrid rotor is provided with a cross-flow rotor, a guide device and a Magnus rotor. The cross-flow rotor is supported so as to be rotatable about a rotational axis and has a plurality of axially extending rotor blades. The guide device has a housing segment partially enclosing the cross-flow rotor in the circumferential direction in such a manner that the cross-flow rotor can be driven by inflowing wind. The Magnus rotor axis is arranged within the cross-flow rotor, and the Magnus rotor axis extends in the direction of the rotational axis. The Magnus rotor has a closed lateral surface and is rotatably driven about the Magnus rotor axis by a drive device.

Abstract translation: 提供了一种用于将风能转换为驱动能量的风力发电厂的风力混合转子。 为了以尽可能高效率的方式利用风能，风力混合式转子设置有横流转子，引导装置和马格努斯转子。 横流转子被支撑成能够围绕旋转轴线旋转并且具有多个轴向延伸的转子叶片。 引导装置具有在圆周方向上部分地包围横流转子的壳体段，使得横流转子可以通过流入的风来驱动。 Magnus转子轴线设置在横流转子内，Magnus转子轴线沿旋转轴线方向延伸。 Magnus转子具有封闭的侧面，并通过驱动装置围绕Magnus转子轴旋转。

公开(公告)号：US20120138740A1

公开(公告)日：2012-06-07

申请号：US13310141

申请日：2011-12-02

Applicant: Jost SEIFERT

Inventor： Jost SEIFERT

IPC: B64C13/24 ,  F16H21/10

CPC classification number: F16H21/44 ,  B64C13/42 ,  B64C13/503 ,  Y10T74/18992

Abstract: A control force transmission arrangement for an aircraft is provided. A transmission device has a first and a second force transmission point, and a coupling unit disposed between them. The coupling unit has a first and a second side element and a connecting element. The first and the second side elements are each connected to the first force transmission point and to the connecting element. At least the first side element has an element for altering the length of the side element. The second force transmission point is provided on the connecting element and is adjustable at least between a first and a second position.

Abstract translation: 提供了一种用于飞机的控制力传递装置。 传动装置具有第一和第二力传递点，以及设置在它们之间的联接单元。 联接单元具有第一和第二侧面元件和连接元件。 第一和第二侧面元件各自连接到第一力传递点和连接元件。 至少第一侧元件具有用于改变侧元件的长度的元件。 第二力传递点设置在连接元件上，并且至少在第一位置和第二位置之间是可调节的。