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1. 发明授权

US09555878B2 Rotor blade control device 有权
标题翻译：转子叶片控制装置
公开(公告)号：US09555878B2
公开(公告)日：2017-01-31
申请号：US14345615
申请日：2012-08-02
申请人： Uwe Arnold , Carsten Wintjen , Andre Hausberg
发明人： Uwe Arnold , Carsten Wintjen , Andre Hausberg
IPC分类号： B64C11/06 , B64C27/04 , B64C27/605
CPC分类号： B64C27/04 , B64C27/605
摘要： The present disclosure provides a rotor blade control device for a helicopter. The rotor blade control device may include a swash plate disk with a non-rotating component coupled to the helicopter. At least three actuators may be arranged around a rotor shaft axis of the helicopter, and a coupling element may be located between each actuator and the non-rotating component. The coupling element can be adjusted to change the position of a crosspoint at the non-rotating component of the swash plate disk alongside the rotor shaft axis in order to adjust the rotor blades. The actuators may be arranged onto the non-rotating component and may be able to pivot around a respective swivel axis. A radial distance of the first crosspoint to the rotor shaft axis may change with the swivel movement of an actuator around the swivel axis.
摘要翻译：本公开提供了一种用于直升机的转子叶片控制装置。转子叶片控制装置可以包括具有联接到直升机的非旋转部件的斜盘盘。至少三个致动器可以布置在直升机的转子轴轴线周围，并且耦合元件可以位于每个致动器和非旋转部件之间。为了调整转子叶片，可以调整联接元件以改变旋转盘盘的非旋转部件处的转子轴线的交叉点的位置。致动器可以布置在非旋转部件上并且可以围绕相应的旋转轴线枢转。第一交叉点与转子轴轴线的径向距离可以随着致动器围绕旋转轴线的旋转运动而改变。

2. 发明授权

US06533549B1 Helicopter 失效
标题翻译：直升机
公开(公告)号：US06533549B1
公开(公告)日：2003-03-18
申请号：US09936008
申请日：2001-09-06
申请人： Thomas Schreiber , Carsten Wintjen , Torsten Röhn
发明人： Thomas Schreiber , Carsten Wintjen , Torsten Röhn
IPC分类号： B63H300
CPC分类号： B64C27/58 , B64C27/32
摘要： A helicopter with rotor blades rotatably connected to a rotor head. The rotor head is non-rotatably connected with a rotor mast (1) pivoted in a transmission housing and driven by a transmission via at least one driving mechanism. A pitch of the rotor blades, relative to a plane of rotation of the rotor blades, is controlled via a swash plate, control rods (12) and via individual actuators (9) allocated to each individual rotor blade. The control rods (12) and the actuators (9) are mounted in the rotor mast (1) and the rotor head and those components act, via a mixing lever (11) and a control rod (8), upon a pivoted arm (7) which adjusts the pitch of the rotor blade. The control devices of the rotor blades do not interfere with the air flow, are affected only to a limited extent by centrifugal forces and additional stresses, and are also protected against influences of the weather.
摘要翻译：具有可旋转地连接到转子头的转子叶片的直升机。转子头不可旋转地连接于在变速器壳体中枢转并通过至少一个驱动机构由变速器驱动的转子桅杆（1）。相对于转子叶片的旋转平面，转子叶片的间距通过旋转斜盘，控制杆（12）和分配给每个单独的转子叶片的各个致动器（9）来控制。控制杆（12）和致动器（9）安装在转子桅杆（1）中，并且转子头部和那些部件通过混合杆（11）和控制棒（8）作用在枢转臂 7）调节转子叶片的间距。转子叶片的控制装置不会干扰空气流动，仅通过离心力和附加应力在有限的程度上受到影响，并且也可以防止天气的影响。

3. 发明申请

US20140377068A1 ROTOR BLADE CONTROL DEVICE 有权
标题翻译：转子叶片控制装置
公开(公告)号：US20140377068A1
公开(公告)日：2014-12-25
申请号：US14345615
申请日：2012-08-02
申请人： Uwe Arnold , Carsten Wintjen , Andre Hausberg
发明人： Uwe Arnold , Carsten Wintjen , Andre Hausberg
IPC分类号： B64C27/04
CPC分类号： B64C27/04 , B64C27/605
摘要： Rotor blade control device for a helicopter, consisting of a swash plate disk, the swash plate disk consisting of a non-rotating part of the swash plate disk, which is stationary stationarily coupled to the helicopter, a rotating part of the swash plate disk, at least three actuators which are arranged around a rotor shaft axis of the helicopter, a coupling element between actuator and the non-rotating part of the swash plate disk. The coupling element can be adjusted in its tilt, in order to change the position of the crosspoint at the non-rotating part of the swash plate disk alongside the rotor shaft axis by means of the actuator through a control shaft, in order to adjust the rotor blades. Here, the coupling element is made up in a rigid way, and the actuators are arranged onto the stationary component being able to pivot around a respective swivel axis. Further, the first crosspoint has a radial distance to the swivel axis, whereby the control axis and the swivel axis are arranged in such a way toward each other, that the radial distance of the first crosspoint to rotor shaft axis changes with the swivel movement of actuator around swivel axis.
摘要翻译：一种用于直升机的转子叶片控制装置，包括斜盘盘，由旋转斜盘盘的非旋转部分组成的旋转盘盘，其固定地联接到直升机，旋转盘旋转部分，围绕直升机的转子轴轴线布置的至少三个致动器，在致动器和旋转盘盘的非旋转部分之间的联接元件。联接元件可以在其倾斜度中进行调整，以便通过致动器通过控制轴来改变旋转斜盘盘的非旋转部分与转子轴线一起的交叉点的位置，以便调节转子叶片。这里，联接元件以刚性的方式制成，并且致动器被布置在能够围绕相应的旋转轴线枢转的固定部件上。此外，第一交叉点具有到旋转轴线的径向距离，由此控制轴线和旋转轴线以彼此相对的方式布置，第一交叉点与转子轴线的径向距离随着旋转轴线的旋转运动而改变执行器围绕旋转轴。

4. 发明授权

US08878466B2 Electromechanical linear actuator 有权
标题翻译：机电线性执行机构
公开(公告)号：US08878466B2
公开(公告)日：2014-11-04
申请号：US13380566
申请日：2010-06-30
申请人： Andre Hausberg , Carsten Wintjen , Werner Pfluegen
发明人： Andre Hausberg , Carsten Wintjen , Werner Pfluegen
IPC分类号： H02K41/00 , F16H25/20 , H02K7/06 , F16H25/24 , H02K7/102 , H02K16/00
CPC分类号： F16H25/205 , F16H25/2454 , F16H2025/2059 , H02K7/06 , H02K7/1021 , H02K16/00 , Y10T74/1459 , Y10T74/1465 , Y10T74/18568 , Y10T74/19637 , Y10T74/2195
摘要： An electro-mechanical linear actuator unit comprising an actuator housing that accommodates at least two electric drives, each of which, when actuated by a control device, sets an associated drive of a respective spindle drive into rotation for adjusting linear movement of the associated spindle drive in order to produce relative linear adjustment of a control rod. The two electric drives are located in the actuator housing in such manner that relative adjustment can be produced by simultaneous actuation of the two electric drives, as the sum of the adjustment movements of the associated spindle drives, or by actuating a single electric drive, as the adjustment movement of the associated spindle drive. A respective brake is provided, in an area of each of the two electric drives, which can be selectively actuated by the control device to then prevent the adjustment movement of the respective associated spindle drive.
摘要翻译：一种电机械线性致动器单元，其包括容纳至少两个电驱动器的致动器壳体，每个电驱动器由控制装置致动时将相应主轴驱动器的相关联的驱动设置为旋转，以调节相关联的主轴驱动器的线性运动以便产生控制棒的相对线性调节。两个电动驱动器位于致动器壳体中，使得可以通过同时致动两个电动驱动器来产生相关调整，作为相关主轴驱动器的调节运动的总和，或通过致动单个电驱动器，如相关主轴驱动器的调整运动。在两个电动驱动器的每一个的区域中设置有相应的制动器，该制动器可由控制装置选择性地致动，从而防止各自相关主轴驱动器的调节运动。

5. 发明申请

US20120137799A1 ELECTROMECHANICAL LINEAR ACTUATOR 有权
标题翻译：电动线性执行器
公开(公告)号：US20120137799A1
公开(公告)日：2012-06-07
申请号：US13380566
申请日：2010-06-30
申请人： Andre Hausberg , Carsten Wintjen , Werner Pfluegen
发明人： Andre Hausberg , Carsten Wintjen , Werner Pfluegen
IPC分类号： F16H25/18 , G06F19/00
CPC分类号： F16H25/205 , F16H25/2454 , F16H2025/2059 , H02K7/06 , H02K7/1021 , H02K16/00 , Y10T74/1459 , Y10T74/1465 , Y10T74/18568 , Y10T74/19637 , Y10T74/2195
摘要： An electro-mechanical linear actuator unit comprising an actuator housing that accommodates at least two electric drives, each of which, when actuated by a control device, sets an associated drive of a respective spindle drive into rotation for adjusting linear movement of the associated spindle drive in order to produce relative linear adjustment of a control rod. The two electric drives are located in the actuator housing in such manner that relative adjustment can be produced by simultaneous actuation of the two electric drives, as the sum of the adjustment movements of the associated spindle drives, or by actuating a single electric drive, as the adjustment movement of the associated spindle drive. A respective brake is provided, in an area of each of the two electric drives, which can be selectively actuated by the control device to then prevent the adjustment movement of the respective associated spindle drive.
摘要翻译：一种电机械线性致动器单元，其包括容纳至少两个电驱动器的致动器壳体，每个电驱动器由控制装置致动时将相应主轴驱动器的相关联的驱动设置为旋转，以调节相关联的主轴驱动器的线性运动以便产生控制棒的相对线性调节。两个电动驱动器位于致动器壳体中，使得可以通过同时致动两个电动驱动器来产生相关调整，作为相关主轴驱动器的调节运动的总和，或通过致动单个电驱动器，如相关主轴驱动器的调整运动。在两个电动驱动器的每一个的区域中设置有相应的制动器，该制动器可由控制装置选择性地致动，从而防止各自相关主轴驱动器的调节运动。

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