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1. 发明申请

US20120160955A1 Hybrid Rotor 有权
标题翻译：混合转子
公开(公告)号：US20120160955A1
公开(公告)日：2012-06-28
申请号：US13332460
申请日：2011-12-21
申请人： Jost SEIFERT
发明人： Jost SEIFERT
IPC分类号： B64C39/00 , B64C27/00
CPC分类号： B64C39/005
摘要： 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.
摘要翻译：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。

2. 发明授权

US09863398B2 Wind-powered rotor and energy generation method using said rotor 有权
公开(公告)号：US09863398B2
公开(公告)日：2018-01-09
申请号：US13996651
申请日：2011-08-01
申请人： Jost Seifert
发明人： Jost Seifert
IPC分类号： F03D3/02 , F03D3/00 , F03D3/04 , F03D9/00 , F03D9/25
CPC分类号： F03D3/007 , F03D3/002 , F03D3/005 , F03D3/02 , F03D3/04 , F03D9/00 , F03D9/25 , F05B2240/201 , F05B2240/212 , F05B2240/214 , Y02B10/30 , Y02E10/74
摘要： A wind power rotor has a first and second rotor device. The first rotor device rotates about a first axis of rotation and has at least two rotor blades moving on a peripheral track about the first axis of rotation. The rotor blades are such that they describe a virtual first shell surface of a virtual first rotating body upon rotation about the first axis of rotation. The second rotor device rotates about a second axis of rotation and has a second rotating body with a closed second shell surface. The second rotating body is arranged at least partially inside of the virtual first rotating body. The first rotor device can be driven by wind in a first direction of rotation and the second rotor device has a drive device, and can be driven in a second direction of rotation which is opposite that of the first direction of rotation.

3. 发明授权

US08757538B2 Aircraft having a variable geometry 有权
标题翻译：具有可变几何形状的飞机
公开(公告)号：US08757538B2
公开(公告)日：2014-06-24
申请号：US13269946
申请日：2011-10-10
申请人： Jost Seifert
发明人： Jost Seifert
IPC分类号： B64C3/38
CPC分类号： B64C3/42 , B64C3/10 , B64C3/16 , B64C3/546 , B64C3/56 , B64C39/068 , Y02T50/12 , Y02T50/14
摘要： An aircraft having a variable geometry for adapting the flight characteristics to different flight situations includes a fuselage with a pair of wings projecting on both sides of the fuselage in the transverse direction (y), each of which wings has an inner wing section arranged stationarily with respect to the fuselage and an outer wing section adjacent thereto and pivotable about a pivot axis. The pivot axis is oriented in a direction deviating from the longitudinal direction (x) of the aircraft by a maximum of 40°.
摘要翻译：具有用于将飞行特性适应于不同飞行情况的可变几何形状的飞机包括具有在横向（y）上在机身两侧突出的一对翼的机身，每个翼具有内侧翼段，相对于机身和与其相邻并且可围绕枢转轴线枢转的外翼部分。枢转轴线沿着飞行器的纵向方向（x）偏离最多40°的方向。

4. 发明授权

US07120538B2 Vehicle guidance system for automatic vehicle guidance 失效
标题翻译：汽车引导系统
公开(公告)号：US07120538B2
公开(公告)日：2006-10-10
申请号：US10483578
申请日：2002-07-12
申请人： Jost Seifert
发明人： Jost Seifert
IPC分类号： G01C21/00 , G06G7/70
CPC分类号： G05D1/101
摘要： A track guidance system for guiding a vehicle with reference to pre-specified desired values of at least one application phase, includes a script development function (3) for developing an application script that defines pre-specified desired values of application phases according to which the vehicle is to be guided, at least one track regulator (12; 12a, 12b, 12c) for guiding the vehicle with reference to the pre-specified desired values, an input function (2) for the user to develop a regulator matrix that allocates track regulators to the application phases, an application control (4) for controlling the time sequence of the application phases on the basis of the corresponding pre-specified desired values, a regulator control (10) for activating the respective track regulator relevant in the respective application phase, whereby the respectively active track regulator (12; 12a, 12b, 12c) transfers its status for control or monitoring to the regulator control (10).
摘要翻译：参考至少一个应用阶段的预先指定的期望值来引导车辆的轨道引导系统包括脚本开发功能（3），用于开发定义应用阶段的预定的期望值的应用脚本，根据该指令，用于引导车辆的至少一个轨道调节器（12; 12a，12b，12c），用于参照预先指定的期望值引导车辆;用于使用者开发调节器的输入功能（2）矩阵，其将轨道调节器分配到应用阶段;应用控制（4），用于基于相应的预先指定的期望值来控制应用阶段的时间顺序;调节器控制（10），用于激活相应的轨道调节器相关在相应的应用阶段中，由此分别有效的轨道调节器（12; 12a，12b，12c）将其用于控制或监视的状态传送到调节器控制器（10）。

5. 发明授权

US08618690B2 Wind power turbine combining a cross-flow rotor and a magnus rotor 有权
标题翻译：风力发电机组合了一个横流转子和一个大转子
公开(公告)号：US08618690B2
公开(公告)日：2013-12-31
申请号：US13333174
申请日：2011-12-21
申请人： Jost Seifert
发明人： Jost Seifert
IPC分类号： F03D11/04
CPC分类号： F03D3/007 , F03D3/002 , F03D3/005 , F03D3/02 , F03D3/04 , F03D9/00 , F03D9/25 , F05B2240/201 , F05B2240/212 , F05B2240/214 , Y02B10/30 , Y02E10/74
摘要： 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.
摘要翻译：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。

6. 发明申请

US20130328320A1 Wind-Powered Rotor and Energy Generation Method Using Said Rotor 有权
标题翻译：使用所述转子的风力转子和能量产生方法
公开(公告)号：US20130328320A1
公开(公告)日：2013-12-12
申请号：US13996651
申请日：2011-08-01
申请人： Jost Seifert
发明人： Jost Seifert
IPC分类号： F03D3/02 , F03D9/00 , F03D3/04
CPC分类号： F03D3/007 , F03D3/002 , F03D3/005 , F03D3/02 , F03D3/04 , F03D9/00 , F03D9/25 , F05B2240/201 , F05B2240/212 , F05B2240/214 , Y02B10/30 , Y02E10/74
摘要： A wind power rotor has a first and second rotor device. The first rotor device rotates about a first axis of rotation and has at least two rotor blades moving on a peripheral track about the first axis of rotation. The rotor blades are such that they describe a virtual first shell surface of a virtual first rotating body upon rotation about the first axis of rotation. The second rotor device rotates about a second axis of rotation and has a second rotating body with a closed second shell surface. The second rotating body is arranged at least partially inside of the virtual first rotating body. The first rotor device can be driven by wind in a first direction of rotation and the second rotor device has a drive device, and can be driven in a second direction of rotation which is opposite that of the first direction of rotation.
摘要翻译：风力转子具有第一和第二转子装置。第一转子装置围绕第一旋转轴线旋转并且具有围绕第一旋转轴线在周边轨道上移动的至少两个转子叶片。转子叶片使得它们描述了围绕第一旋转轴线旋转时虚拟的第一旋转体的虚拟的第一壳体表面。第二转子装置围绕第二旋转轴线旋转并且具有带有封闭的第二壳体表面的第二旋转体。第二旋转体至少部分地布置在虚拟第一旋转体的内部。第一转子装置可以在第一旋转方向上由风驱动，并且第二转子装置具有驱动装置，并且可以在与第一旋转方向相反的第二旋转方向上被驱动。

7. 发明申请

US20120085858A1 Aircraft Having a Variable Geometry 有权
标题翻译：具有可变几何的飞机
公开(公告)号：US20120085858A1
公开(公告)日：2012-04-12
申请号：US13269946
申请日：2011-10-10
申请人： Jost Seifert
发明人： Jost Seifert
IPC分类号： B64C3/42
CPC分类号： B64C3/42 , B64C3/10 , B64C3/16 , B64C3/546 , B64C3/56 , B64C39/068 , Y02T50/12 , Y02T50/14
摘要： An aircraft having a variable geometry for adapting the flight characteristics to different flight situations includes a fuselage with a pair of wings projecting on both sides of the fuselage in the transverse direction (y), each of which wings has an inner wing section arranged stationarily with respect to the fuselage and an outer wing section adjacent thereto and pivotable about a pivot axis. The pivot axis is oriented in a direction deviating from the longitudinal direction (x) of the aircraft by a maximum of 40°.
摘要翻译：具有用于将飞行特性适应于不同飞行情况的可变几何形状的飞机包括具有在横向（y）上在机身两侧突出的一对翼的机身，每个翼具有内侧翼段，相对于机身和与其相邻并且可围绕枢转轴线枢转的外翼部分。枢转轴线沿着飞行器的纵向方向（x）偏离最多40°的方向。

8. 发明授权

US08944371B2 Transmission of a control force 有权
标题翻译：控制力传递
公开(公告)号：US08944371B2
公开(公告)日：2015-02-03
申请号：US13310141
申请日：2011-12-02
申请人： Jost Seifert
发明人： Jost Seifert
IPC分类号： B64C13/24 , B64C13/42 , B64C13/50
CPC分类号： F16H21/44 , B64C13/42 , B64C13/503 , Y10T74/18992
摘要： 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.
摘要翻译：提供了一种用于飞行器的控制力传递装置。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。

9. 发明授权

US06931368B1 Flight control display for use in an aircraft cockpit and in aircraft simulation systems 有权
标题翻译：用于飞机驾驶舱和飞机模拟系统的飞行控制显示
公开(公告)号：US06931368B1
公开(公告)日：2005-08-16
申请号：US09715070
申请日：2000-11-20
申请人： Jost Seifert
发明人： Jost Seifert
IPC分类号： G01C23/00 , G06F17/50 , G09B19/16
CPC分类号： G01C23/005
摘要： A flight control display shows a representation of terrain, the horizon, an aircraft with a fuselage and aircraft wings, and a gamma ladder. The observer has a viewing direction at least in a predefined attitude range, which viewing direction is directed along the momentary flight path. The aircraft is therefore rotated depending on its momentary angle of incidence and angle of yaw with respect to the observer's viewing direction. The representation of the terrain is obtained from the relative position of a geodetic system of coordinates XG, YG, ZG and an aerodynamic system of axes of the airplane, in which case a reference line of the gamma ladder coincides with the horizon.
摘要翻译：飞行控制显示屏显示地形，地平线，飞机机身和飞机机翼以及伽玛梯。观察者至少在预定的姿态范围内具有观察方向，该观察方向是沿着瞬时飞行路线引导的。因此，飞机根据其相对于观察者观察方向的瞬时入射角和偏航角度而旋转。地形的表示是从坐标系X，Y，G，Z，G的大地测量系统的相对位置和空气动力学系统在这种情况下，伽马梯的参考线与地平线重合。

10. 发明授权

US08528855B2 Magnus and transverse flow hybrid rotor 有权
标题翻译：马格努斯和横向流动混合转子
公开(公告)号：US08528855B2
公开(公告)日：2013-09-10
申请号：US13332460
申请日：2011-12-21
申请人： Jost Seifert
发明人： Jost Seifert
IPC分类号： B64C39/00
CPC分类号： B64C39/005
摘要： 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.
摘要翻译：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。

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