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88 条记录 (耗时 0.028 秒)

    Rotor, especially for rotary wing aircraft
    31.
    发明授权
    Rotor, especially for rotary wing aircraft 失效
    转子，特别适用于旋翼飞机

    公开(公告)号：US4786236A

    公开(公告)日：1988-11-22

    申请号：US107241

    申请日：1987-10-09

    申请人： Michael Hahn ,  Gerald Kuntze-Fechner

    发明人： Michael Hahn ,  Gerald Kuntze-Fechner

    IPC分类号： B64C27/50

    CPC分类号： B64C27/50

    摘要： A helicopter rotor with foldable blades has, in the hub and blade roots, holes for mounting the blade roots to the rotor hub with connecting bolts passing through these holes in the operating position of the blades. Additionally, at least one blade of two blades and the hub have aligned holes for holding the respective foldable blade in a folded position, whereby one of the regular connecting bolts passes through the aligned holes, which are located as close as possible to the pivoting point connecting a pitch angle control rod to a pitch angle control sleeve.

    摘要翻译： 具有可折叠刀片的直升机转子在轮毂和叶片根部具有用于将叶片根部安装到转子毂上的孔，其中连接螺栓在叶片的操作位置通过这些孔。 另外，两个叶片的至少一个叶片和轮毂具有对准的孔，用于将相应的可折叠刀片保持在折叠位置，由此一个规则连接螺栓穿过对准的孔，其尽可能靠近枢转点 将俯仰角控制杆连接到俯仰角控制套筒。

    Rotor blade, especially for a rotary wing aircraft
    32.
    发明授权
    Rotor blade, especially for a rotary wing aircraft 失效
    转子叶片，特别适用于旋翼飞机

    公开(公告)号：US4592701A

    公开(公告)日：1986-06-03

    申请号：US686472

    申请日：1984-12-26

    申请人： Michael Hahn ,  Otmar Friedberger ,  Gerhard Singer

    发明人： Michael Hahn ,  Otmar Friedberger ,  Gerhard Singer

    IPC分类号： B64C27/28 ,  B64C27/33

    CPC分类号： B64C27/28 ,  B64C27/33

    摘要： A rotor blade, for example for a rotary wing aircraft, has a wing section d a root section interconnected by a neck section surrounded by a blade angle adjustment sleeve which is stiff against torque moments for transmitting blade angle adjustment movements through the sleeve to the wing section. The trailing edge of the sleeve is provided with a gap which extends, at least partially, alongside the rear edge of the neck section for visually inspecting the neck section inside the sleeve even when the root section is connected to a rotor hub. A reflecting mirror may be used for inspecting all sides of the neck section through the gap.

    摘要翻译： 例如用于旋转飞行器的转子叶片具有翼部分和根部，其通过由叶片角度调节套筒包围的颈部部分相互连接，该叶片角度调节套筒刚性地抵抗用于将叶片角度调节运动通过套筒传递到翼部的扭矩 部分。 套筒的后缘设置有间隙，其至少部分地延伸到颈部部分的后边缘，用于目视检查套管内的颈部部分，即使当根部连接到转子毂时也是如此。 反射镜可用于通过间隙检查颈部的所有侧面。

    Wing mounting for a rotary wing aircraft
    33.
    发明授权
    Wing mounting for a rotary wing aircraft 失效
    机翼安装用于旋翼飞机

    公开(公告)号：US4547127A

    公开(公告)日：1985-10-15

    申请号：US544563

    申请日：1983-10-24

    申请人： Hubert Frommlet ,  Michael Hahn

    发明人： Hubert Frommlet ,  Michael Hahn

    IPC分类号： B64C27/32 ,  B64C27/33 ,  B64C27/48 ,  B64C27/37

    CPC分类号： B64C27/33 ,  B64C27/32 ,  B64C27/48

    摘要： A flexible blade neck of a helicopter rotor blade is bridged by a torsion gid sleeve for the blade angle adjustments. The radially outer end of the blade neck and sleeve are rigidly connected to the wing section of the blade. The radially inner end of the blade neck forms a blade root which is secure to the rotor head or hub. Additionally, the radially inner ends of the blade root and of the sleeve are interconnected by a ball and socket arrangement permitting a universal movement between the sleeve and the blade neck, thereby decoupling sleeve movements from the blade neck and vice versa.

    摘要翻译： 直升机转子叶片的柔性叶片颈部由扭转刚性套筒桥接，用于叶片角度调整。 叶片颈部和套筒的径向外端刚性地连接到叶片的翼部。 叶片颈部的径向内端形成叶片根部，叶片根部固定到转子头部或轮毂上。 此外，叶片根部和套筒的径向内端部通过允许套筒和叶片颈部之间的通用运动的球窝装置相互连接，从而使套筒运动与叶片颈部脱离，反之亦然。

    Aerosol generator
    34.
    发明授权
    Aerosol generator 有权

    公开(公告)号：US09975136B2

    公开(公告)日：2018-05-22

    申请号：US14123634

    申请日：2012-06-04

    申请人： Harald Schulz ,  Philipp Holzmann ,  Dominique Mutschmann ,  Michael Hahn

    发明人： Harald Schulz ,  Philipp Holzmann ,  Dominique Mutschmann ,  Michael Hahn

    IPC分类号： B05B17/00 ,  A61M11/00 ,  A61M15/00

    CPC分类号： B05B17/0646 ,  A61M11/005 ,  A61M15/00 ,  A61M15/0015 ,  A61M15/0018 ,  A61M15/0085

    摘要： An aerosol generator for generating an aerosol from a fluid, comprising: a vibratable membrane (22) having a first side (24) for being in contact with the fluid and an opposite second side (25), the membrane having a plurality of through holes (26) penetrating the membrane in an extension direction (E) from the first side to the second side, whereby the fluid passes the through holes from the first side to the second side when the membrane is vibrated for generating the aerosol at the second side, each through hole (26) having along its extension direction (E) a smallest diameter (Ds), a larger diameter (DL) that is larger than the smallest diameter and defined by that diameter that is closest to triple, preferably twice said smallest diameter, each through hole having a nozzle portion (32) defined by that continuous portion of the through hole in the extension direction comprising the smallest diameter of the through hole and bordered by the larger diameter of the through hole, characterized in that the ratio of the total length of each through hole (26) in the extension direction to the length of a respective one of said nozzle portions (32) in the extension direction is at least (4), preferably at least (4.5) and most preferred equal to or larger than (5).

    ASSEMBLY COMPRISING A FIRST CAM CARRIER
    35.
    发明申请
    ASSEMBLY COMPRISING A FIRST CAM CARRIER 有权
    组装包括第一个CAM载体

    公开(公告)号：US20140318304A1

    公开(公告)日：2014-10-30

    申请号：US14349813

    申请日：2012-08-16

    申请人： Michael Hahn ,  Martin Fleischer

    发明人： Michael Hahn ,  Martin Fleischer

    IPC分类号： B62D1/184

    CPC分类号： B62D1/184 ,  F16H25/186

    摘要： An assembly includes a first cam carrier and at least one other cam carrier for a securing device for an adjustable steering column of a motor vehicle. Each of the cam carriers has at least one cam, and the carriers are located opposite one another so that they can rotate against one another about a rotational axis. When the first cam carrier rotates against the other cam carrier through a rotational angle about the rotational axis, the cam of the first cam carrier rests on and glides along the cam of the other cam carrier on a contact path. The contact path runs at a radial distance from the rotational axis, and the distance altering depends on the rotational angle.

    摘要翻译： 组件包括第一凸轮架和用于机动车辆的可调转向柱的固定装置的至少一个其它凸轮架。 每个凸轮支架具有至少一个凸轮，并且托架彼此相对地定位，使得它们可以围绕旋转轴线彼此相对旋转。 当第一凸轮架相对于另一个凸轮架旋转一个围绕旋转轴线的转角时，第一凸轮架的凸轮在接触路径上靠着另一个凸轮架的凸轮滑动并滑动。 接触路径在距离旋转轴线的径向距离处延伸，并且距离改变取决于旋转角度。

    JOINT ARRANGEMENT FOR A VEHICLE
    38.
    发明申请
    JOINT ARRANGEMENT FOR A VEHICLE 有权
    车辆联合安排

    公开(公告)号：US20100221061A1

    公开(公告)日：2010-09-02

    申请号：US12295327

    申请日：2007-05-08

    申请人： Michael Hahn ,  Thomas Herrmann

    发明人： Michael Hahn ,  Thomas Herrmann

    IPC分类号： F16J15/52

    CPC分类号： B62D3/12 ,  B62D7/163 ,  F16C11/0623 ,  F16C35/02 ,  F16C2326/24 ,  Y10T74/1967 ,  Y10T403/315 ,  Y10T403/32631 ,  Y10T403/32729

    摘要： A joint arrangement, for a vehicle, is provided with a joint (7), which has a joint housing (8) and a pivot pin (9) mounted movably in relation thereto. The arrangement also includes a rod (4), which has a cavity (6) and is connected to the joint (7); a sealing bellows (10), which defines an interior space (10) and in which the joint (7) is arranged at least partially; and a gas-permeable connection (13), which connects the cavity (6) of the rod (4) to the interior space (11) of the sealing bellows (10) and has at least one groove (15), which is formed in a front side (21) of the joint (7), which said front side faces the rod (4), opens into the interior space (11) and has a radially outer end (27). The groove (15) with its radially outer end ends at a spaced location from the outer circumferential contour of the front surface (21).

    摘要翻译： 一种用于车辆的联合装置设置有具有联接壳体（8）和可相对于其移动地安装的枢轴销（9）的接头（7）。 该装置还包括具有空腔（6）并连接到接头（7）的杆（4）; 密封波纹管（10），其限定内部空间（10），并且所述接头（7）至少部分地布置在所述密封波纹管中; 以及将所述杆（4）的空腔（6）连接到所述密封波纹管（10）的内部空间（11）并且具有至少一个凹槽（15）的透气连接件（13） 在所述前侧面向所述杆（4）的所述接头（7）的前侧（21）中，通向所述内部空间（11）并且具有径向外端（27）。 槽（15）的径向外端在与前表面（21）的外周轮廓相隔的位置处终止。