公开(公告)号：US09090344B2

公开(公告)日：2015-07-28

申请号：US13405649

申请日：2012-02-27

申请人： Martin Stucki

发明人： Martin Stucki

IPC分类号： B64C27/48 ,  B64C27/35

CPC分类号： B64C27/48 ,  B64C27/35 ,  B64C27/37

摘要： A rotor blade coupling device (9) comprising a torsionally rigid carrier (4) is disclosed, the carrier (4) being mounted in a manner which is free of centrifugal force between a thrust bearing (3) and a control bearing (5), resilient impact and pivoting movements of the rotor blade coupling device (9) being able to take place in a damped manner. The rotor blade coupling device (9) is clamped between a rotor head star (101) and a rotor head central piece (102) and held rotatably about the rotor axis A. The centrifugal forces which occur, are transmitted from a rotor blade holder (2) to the rotor head star (101) and thus kept away from the carrier (4).

摘要翻译： 公开了一种包括扭转刚性载体（4）的转子叶片联接装置（9），载体（4）以推力轴承（3）和控制轴承（5）之间没有离心力的方式安装， 能够以阻尼方式发生的转子叶片联接装置（9）的弹性冲击和枢转运动。 转子叶片联接装置（9）被夹紧在转子头部星形件（101）和转子头部中心件（102）之间并且围绕转子轴线A可旋转地保持。发生的离心力从转子叶片保持器 2）到转子头星（101），并因此远离载体（4）。

公开(公告)号：US20070151369A1

公开(公告)日：2007-07-05

申请号：US11634087

申请日：2006-12-06

申请人： Ennio Bitto ,  Gerhard Eckert ,  Sergej Lopatin ,  Christian Matt ,  Helmut Pfeiffer ,  Alfred Rieder ,  Martin Anklin-Imhof ,  Martin Stucki

发明人： Ennio Bitto ,  Gerhard Eckert ,  Sergej Lopatin ,  Christian Matt ,  Helmut Pfeiffer ,  Alfred Rieder ,  Martin Anklin-Imhof ,  Martin Stucki

IPC分类号： G01F1/84

CPC分类号： G01F1/8477 ,  G01F1/8409 ,  G01F1/8413 ,  G01F1/8422 ,  G01F1/8427

摘要： The measurement transducer includes at least two oscillatably held transducer tubes vibrating, at least at times, during operation, of which at least one transducer tube serving to convey at least a volume portion of a medium to be measured, communicates with a pipeline; as well as at least one transducer element for converting electrical energy into mechanical and/or vice versa. The two transducer tubes are mechanically coupled together by means of at least one, inlet-side, coupling element and by means of at least one, outlet-side, coupling element in such a manner that both the inlet-side coupling element, as well as also the outlet-side coupling element, are subjected during operation repeatedly to deformations which correspond to vibrations of at least one of the two transducer tubes for converting electrical energy into mechanical, oscillatory energy and/or vice versa. The transducer element, especially a transducer element formed by means of a piezoelectric, deformation body, and at least one of the coupling elements, are, at least mediately, mechanically coupled together in such a manner that the transducer element executes, at least in part, oscillatory movements, which correspond with the repeated deformations at least of this coupling element.

摘要翻译： 该测量传感器包括至少两个可振荡地保持的换能器管，至少在操作期间振动，其中至少一个用于输送要测量的介质的体积部分的换能器管与管道连通; 以及用于将电能转换成机械和/或反之亦然的至少一个换能器元件。 两个换能器管通过至少一个入口侧联接元件并且借助于至少一个出口侧联接元件以这样的方式机械耦合在一起，使得入口侧耦合元件以及 以及出口侧联接元件也在重复操作时经受对应于两个换能器管中的至少一个的振动的变形，用于将电能转换成机械振荡能量和/或反之亦然。 传感器元件，特别是通过压电变形体和至少一个耦合元件形成的换能器元件至少中介地以这样的方式机械耦合在一起，使得换能器元件至少部分地执行 ，振荡运动，其至少与该耦合元件的重复变形相对应。

公开(公告)号：US08783613B2

公开(公告)日：2014-07-22

申请号：US13405838

申请日：2012-02-27

申请人： Martin Stucki

发明人： Martin Stucki

IPC分类号： B64C1/14

CPC分类号： B64C1/1476 ,  B64C1/14 ,  B64C27/04 ,  B64D7/00

摘要： An observation port (4) in a primary structure (13) of a helicopter cabin (0) is disclosed, which is arranged between a pilot's seat (2) and a co-pilot's seat (3). The observation port (4) is delimited from the interior by an inner screen (15), and from the atmosphere by an outer screen (16), wherein the pilot can observe the space underneath the helicopter cabin (0) through the observation port (4). As a result of the configuration of the observation port (4) the pilot can assume an ergonomic and relaxed seating position at any time, even when he is executing flights with suspended loads. By means of the observation port (4) and the windows (15, 16), which extend laterally between the two pilots' seats (2, 3), a novel unrestricted vertical visual frame of reference onto the suspended load is achieved, wherein the length of the load cable has practically no influence.

摘要翻译： 公开了一种直升机舱（0）的主结构（13）中的观察端口（4），其布置在飞行员座椅（2）和副飞行员座椅（3）之间。 观察端口（4）由内部屏幕（15）从内部界定，并且通过外部屏幕（16）从大气层限定，其中飞行员可以通过观察端口（0）观察直升机机舱（0）下方的空间 4）。 作为观察端口（4）的配置的结果，即使当他执行悬挂载荷的飞行时，飞行员也可以随时承担人体工程学和放松的就座位置。 通过在两个飞行员座位（2,3）之间横向延伸的观察端口（4）和窗口（15,16），实现了悬挂载荷上的新颖的无限制垂直视觉参考系，其中， 负载电缆的长度几乎没有影响。

公开(公告)号：US20100018572A1

公开(公告)日：2010-01-28

申请号：US12308911

申请日：2007-06-19

申请人： Thomas Grimberg ,  Martin Stucki

发明人： Thomas Grimberg ,  Martin Stucki

IPC分类号： H01L31/00 ,  H02G3/08 ,  H05K5/00 ,  H05K7/20

CPC分类号： H02G3/086 ,  H02S40/34 ,  H02S40/345

摘要： A connection box (1) suited for wiring one or more solar cells (33) includes a housing base (2) and a housing top (3) that includes retaining means (21) for receiving a circuit board.

摘要翻译： 适于布线一个或多个太阳能电池（33）的连接盒（1）包括壳体基座（2）和壳体顶部（3），其包括用于接收电路板的保持装置（21）。

公开(公告)号：US20120217345A1

公开(公告)日：2012-08-30

申请号：US13405838

申请日：2012-02-27

申请人： Martin Stucki

发明人： Martin Stucki

IPC分类号： B64C1/14

CPC分类号： B64C1/1476 ,  B64C1/14 ,  B64C27/04 ,  B64D7/00

摘要： An observation port (4) in a primary structure (13) of a helicopter cabin (0) is disclosed, which is arranged between a pilot's seat (2) and a co-pilot's seat (3). The observation port (4) is delimited from the interior by an inner screen (15), and from the atmosphere by an outer screen (16), wherein the pilot can observe the space underneath the helicopter cabin (0) through the observation port (4). As a result of the configuration of the observation port (4) the pilot can assume an ergonomic and relaxed seating position at any time, even when he is executing flights with suspended loads. By means of the observation port (4) and the windows (15, 16), which extend laterally between the two pilots' seats (2, 3), a novel unrestricted vertical visual frame of reference onto the suspended load is achieved, wherein the length of the load cable has practically no influence.

摘要翻译： 公开了一种直升机舱（0）的主结构（13）中的观察端口（4），其布置在飞行员座椅（2）和副飞行员座椅（3）之间。 观察端口（4）由内部屏幕（15）从内部界定，并且通过外部屏幕（16）从大气层限定，其中飞行员可以通过观察端口（0）观察直升机机舱（0）下方的空间 4）。 作为观察端口（4）的配置的结果，即使当他执行悬挂载荷的飞行时，飞行员也可以随时承担人体工程学和放松的就座位置。 通过在两个飞行员座位（2,3）之间横向延伸的观察端口（4）和窗口（15,16），实现了悬挂载荷上的新颖的无限制垂直视觉参考系，其中， 负载电缆的长度几乎没有影响。

公开(公告)号：US07325461B2

公开(公告)日：2008-02-05

申请号：US11634087

申请日：2006-12-06

申请人： Ennio Bitto ,  Gerhard Eckert ,  Sergej Lopatin ,  Christian Matt ,  Helmut Pfeiffer ,  Alfred Rieder ,  Martin Anklin-Imhof ,  Martin Stucki

发明人： Ennio Bitto ,  Gerhard Eckert ,  Sergej Lopatin ,  Christian Matt ,  Helmut Pfeiffer ,  Alfred Rieder ,  Martin Anklin-Imhof ,  Martin Stucki

IPC分类号： G01F1/84

CPC分类号： G01F1/8477 ,  G01F1/8409 ,  G01F1/8413 ,  G01F1/8422 ,  G01F1/8427

摘要： The measurement transducer includes at least two oscillatably held transducer tubes vibrating, at least at times, during operation, of which at least one transducer tube serving to convey at least a volume portion of a medium to be measured, communicates with a pipeline; as well as at least one transducer element for converting electrical energy into mechanical and/or vice versa. The two transducer tubes are mechanically coupled together by means of at least one, inlet-side, coupling element and by means of at least one, outlet-side, coupling element in such a manner that both the inlet-side coupling element, as well as also the outlet-side coupling element, are subjected during operation repeatedly to deformations which correspond to vibrations of at least one of the two transducer tubes for converting electrical energy into mechanical, oscillatory energy and/or vice versa. The transducer element, especially a transducer element formed by means of a piezoelectric, deformation body, and at least one of the coupling elements, are, at least mediately, mechanically coupled together in such a manner that the transducer element executes, at least in part, oscillatory movements, which correspond with the repeated deformations at least of this coupling element.

摘要翻译： 该测量传感器包括至少两个可振荡地保持的换能器管，至少在操作期间振动，其中至少一个用于输送要测量的介质的体积部分的换能器管与管道连通; 以及用于将电能转换成机械和/或反之亦然的至少一个换能器元件。 两个换能器管通过至少一个入口侧联接元件并且借助于至少一个出口侧联接元件以这样的方式机械耦合在一起，使得入口侧耦合元件以及 以及出口侧联接元件也在重复操作时经受对应于两个换能器管中的至少一个的振动的变形，用于将电能转换成机械振荡能量和/或反之亦然。 传感器元件，特别是通过压电变形体和至少一个耦合元件形成的换能器元件至少中介地以这样的方式机械耦合在一起，使得换能器元件至少部分地执行 ，振荡运动，其至少与该耦合元件的重复变形相对应。

公开(公告)号：US5593675A

公开(公告)日：1997-01-14

申请号：US360334

申请日：1994-12-21

申请人： Gerhard Hodler ,  Peter Lerch ,  Martin Stucki

发明人： Gerhard Hodler ,  Peter Lerch ,  Martin Stucki

IPC分类号： A61K9/08 ,  A61K39/395 ,  A61K47/02 ,  A61K47/18 ,  A61K47/26 ,  C07K1/18 ,  C07K16/00 ,  C07K16/06 ,  C07K16/34 ,  C07K1/14 ,  C07K16/46

CPC分类号： C07K16/065 ,  C07K16/34

摘要： An anti-D immunoglobulin G-preparation is produced in high-yield from human plasma containing anti-D IgG, or a plasma fraction containing an anti-D IgG, in which (A) the plasma, or the plasma fraction, with a pH in the range of pH 3.5 to 6.5 and a conductivity value in the range of 2 to 4 mS/cm, is subjected to ion exchange chromatography with an adsorbent which has carboxymethyl groups as functional groups, the anti-D IgG being bound to the adsorbent, (B) the adsorbent with the bound anti-D IgG is first rinsed with a wash solution at a pH in the range of 5 to 8 and a conductivity value in the range of 2 to 4 mS/cm, and the anti-D IgG is subsequently eluted, and further (C) the eluted anti-D IgG at a pH in the range of 6 to 8 and a conductivity value in the range of 2 to 4 mS/cm is treated with an alkaline adsorbent with ion-exchange characteristics in order to bind undesired components, and finally, the anti-D IgG is concentrated. The non-infectious anti-D concentrate thus obtained possesses a high specific activity of more than 1% anti-D IgG per gram of total IgG.

摘要翻译： 抗-D免疫球蛋白G制剂以含有抗-D IgG的人血浆的高产率或含有抗-DIgG的血浆级分产生，其中（A）血浆或血浆级分具有pH 在pH 3.5〜6.5的范围内，电导率值在2〜4mS / cm的范围内，用具有羧甲基作为官能团的吸附剂进行离子交换层析，抗D IgG与吸附剂结合 ，（B）具有结合的抗-D IgG的吸附剂首先用pH为5〜8，电导率值为2〜4mS / cm的洗涤溶液冲洗，反-D 随后洗脱IgG，并且进一步（C）在6至8范围内的pH值和2至4mS / cm 2范围内的电导率值下洗脱的抗-D IgG用离子交换的碱性吸附剂处理 特性以便结合不合需要的组分，最后浓缩抗D IgG。 由此获得的非感染性抗-D浓缩物具有高于每克总IgG超过1％抗-D IgG的比活性。