公开(公告)号：US08523101B2

公开(公告)日：2013-09-03

申请号：US12178711

申请日：2008-07-24

申请人： Olivier Cazals ,  Alexander Koch

发明人： Olivier Cazals ,  Alexander Koch

IPC分类号： B64C15/00

CPC分类号： B64D27/20 ,  B64C5/12 ,  B64C15/02 ,  B64C39/12 ,  B64F5/40

摘要： An aircraft capable of making short takeoffs and landings includes essentially a fuselage, a wing secured to the fuselage, a front horizontal stabilizer secured to the fuselage on the front end of the fuselage and at least two jet engines for propulsion. According to the architecture proposed, the propulsion engines are arranged side by side above the fuselage in a rear part of the fuselage with a width at least equal to the width of the propulsion group, a fuselage flap device is arranged in the back of the fuselage so that the fuselage flaps adopt at least a position in which the flaps are considerably in a horizontal plane and take at least a high-lift position in which the flaps are turned downward in such a way that the blast created by the jet engines is channeled towards the top surface of the fuselage flaps to induce a blowing effect.

摘要翻译： 能够短时起飞和着陆的飞机基本上包括机身，固定在机身上的机翼，固定在机身前端的机身上的前水平稳定器和至少两个用于推进的喷气发动机。 根据所提出的结构，推进发动机在机身的后部并排布置在机身的后部，其宽度至少等于推进组的宽度，机身翼片装置布置在机身的后部 使得机身翼片至少采用襟翼相当于水平面的位置，并且至少采取高升力位置，在该位置襟翼向下转动，使得由喷气发动机产生的气流被引导 朝向机身襟翼的顶面，以引起吹风效果。

公开(公告)号：US08152095B2

公开(公告)日：2012-04-10

申请号：US12178704

申请日：2008-07-24

申请人： Olivier Cazals ,  Alexander Koch

发明人： Olivier Cazals ,  Alexander Koch

IPC分类号： B64D27/20

CPC分类号： B64C5/02 ,  B64C5/06 ,  B64D27/20 ,  B64D29/04 ,  B64D29/08 ,  B64D33/02 ,  B64D33/06 ,  B64D2033/0286 ,  Y02T50/44

摘要： An aircraft, the propulsive units of which include engines, and which is distinguished by reduced noise emissions, includes a wing structure fixed to an upper region of the fuselage, and a vertical tail system having at least two vertical stabilizers which are generally vertically fixed to the fuselage aftwardly of the wing structure. The engines are disposed side by side in a propulsive package disposed above the fuselage, which propulsive package includes the following: air inlet openings for the propulsive package, which openings are disposed above the fuselage between a point at the leading edge and a point at the trailing edge of an aerodynamic root chord of the wing structure; and exhaust nozzle conduit outlets associated with exhaust nozzle conduits, which outlets are formed by the structure (cowling structure) of the propulsive package, and are disposed above the fuselage forwardly of an aft terminus of the fuselage and between the vertical stabilizers.

摘要翻译： 飞机的推进单元包括发动机，其特征在于减少的噪声排放，包括固定到机身上部区域的机翼结构，以及具有至少两个垂直稳定器的垂直尾翼系统，该垂直尾翼系统通常垂直固定到 机身后部的机身结构。 发动机并排布置在设置在机身上方的推进式包装中，该推进式包装包括以下内容：用于推进包装的空气入口开口，该开口设置在机身的上方，位于前缘的一点和 机翼结构的气动根弦的后缘; 以及与排气喷嘴管道相关联的排气喷嘴导管出口，这些出口由推进式包装的结构（整流罩结构）形成，并且设置在机身的后端的机身前方和垂直稳定器之间。

公开(公告)号：US20090084889A1

公开(公告)日：2009-04-02

申请号：US12178704

申请日：2008-07-24

申请人： Olivier Cazals ,  Alexander Koch

发明人： Olivier Cazals ,  Alexander Koch

IPC分类号： B64C11/00 ,  B64D27/00 ,  B64D33/02 ,  B64D29/00

CPC分类号： B64C5/02 ,  B64C5/06 ,  B64D27/20 ,  B64D29/04 ,  B64D29/08 ,  B64D33/02 ,  B64D33/06 ,  B64D2033/0286 ,  Y02T50/44

摘要： An aircraft the propulsive units of which include engines, and which is distinguished by reduced noise emissions, includes a wing structure fixed to an upper region of the fuselage, and a vertical tail system having at least two vertical stabilizers which are generally vertically fixed to the fuselage aftwardly of the wing structure. The engines are disposed side by side in a propulsive package disposed above the fuselage, which propulsive package includes the following, air inlet openings for the propulsive package, which openings are disposed above the fuselage between a point at the leading edge and a point at the trailing edge of an aerodynamic root chord of the wing structure; and exhaust nozzle conduit outlets associated with exhaust nozzle conduits, which outlets are formed by the structure (cowling structure) of the propulsive package, and are disposed above the fuselage forwardly of an aft terminus of the fuselage and between the vertical stabilizers.

摘要翻译： 包括引擎在内的推进单元的飞机包括固定在机身上部区域的机翼结构以及具有至少两个垂直稳定器的垂直尾翼系统，该垂直尾翼系统通常垂直地固定在机身上 机身后部的机身结构。 发动机并排布置在设置在机身上方的推进式包装中，该推进包装包括用于推进包装的以下空气入口，这些开口设置在机身的上方，位于前缘的一点和 机翼结构的气动根弦的后缘; 以及与排气喷嘴管道相关联的排气喷嘴导管出口，这些出口由推进式包装的结构（整流罩结构）形成，并且设置在机身的后端的机身前方和垂直稳定器之间。

公开(公告)号：US20100272384A1

公开(公告)日：2010-10-28

申请号：US12774383

申请日：2010-05-05

申请人： Mathias MUELLER ,  Lars Hoffmann ,  Tobias Lautenschlager ,  Alexander Koch

发明人： Mathias MUELLER ,  Lars Hoffmann ,  Tobias Lautenschlager ,  Alexander Koch

IPC分类号： G02B6/00

CPC分类号： G01L1/243 ,  G01L1/246 ,  G01L5/166

摘要： A force-moment sensor is provided for measuring at least one force and/or moment, which comprises a first part, a second part and an optical fibre arranged therebetween, said optical fibre comprising in at least one section a component for detecting deformations and/or stresses of the fibre transversely to its longitudinal axis. The present invention further relates to a method for measuring forces and/or moments. Thus, a fibre is provided which comprises at least one component for detecting deformations and/or stresses of the fibre transversely to a longitudinal axis of the fibre and into which light is introduced. According to this method, a force and/or moment acts on the fibre, wherein at least one component of the force and/or moment acts perpendicularly to the longitudinal axis of the fibre. The light reflected in the fibre is then detected and the detected spectrum analysed.

摘要翻译： 提供力矩传感器用于测量至少一个力和/或力矩，其包括第一部分，第二部分和布置在其间的光纤，所述光纤在至少一个部分中包括用于检测变形和/ 或纤维横向于其纵向轴线的应力。 本发明还涉及一种用于测量力和/或力矩的方法。 因此，提供了一种纤维，其包括至少一个用于检测纤维的变形和/或应力横向于纤维的纵向轴线并且被引入光的部件。 根据该方法，力和/或力矩作用在纤维上，其中力和/或力矩的至少一个分量垂直于纤维的纵向轴线作用。 然后检测在光纤中反射的光并分析检测到的光谱。

公开(公告)号：US07675304B2

公开(公告)日：2010-03-09

申请号：US12360323

申请日：2009-01-27

申请人： Alexander Koch ,  Arkady Ivannikov ,  Ted Toth

发明人： Alexander Koch ,  Arkady Ivannikov ,  Ted Toth

IPC分类号： G01R31/02

CPC分类号： G01R1/06705

摘要： An improved test probe assembly has an improved mounting assembly which provides the test probe multi-directional freedom of movement with respect to a base in order to resist damage frequently caused to the test probe. The improved mounting assembly may, for example, include at least a first resilient mount disposed on the base and having at least a first support and at least a first resilient element. The at least a first resilient element, which may, for example, be at least a first spring, is deflectable when the test probe engages a structure, such as a device under testing (DUT). Accordingly, the improved test probe assembly of the invention can be deflected an infinite number of positions, in order to resist damage caused, for example, by misalignment between the probe and the DUT.

摘要翻译： 改进的测试探针组件具有改进的安装组件，其提供测试探针相对于基座的多方向运动自由度，以便抵抗经常对测试探针造成的损坏。 改进的安装组件可以例如包括设置在基座上的至少第一弹性支架，并且具有至少第一支撑件和至少第一弹性元件。 当测试探针接合诸如被测设备（DUT）的结构时，至少第一弹性元件（例如可以是至少第一弹簧）是可偏转的。 因此，本发明的改进的测试探针组件可以偏转无限数量的位置，以便抵抗例如由探针和被测物之间的对准引起的损伤。

公开(公告)号：US07268567B2

公开(公告)日：2007-09-11

申请号：US11051012

申请日：2005-02-04

申请人： Alexander Koch ,  Arkady Ivannikov ,  Ted Toth

发明人： Alexander Koch ,  Arkady Ivannikov ,  Ted Toth

IPC分类号： G01R31/02

CPC分类号： G01R1/06705

摘要： An improved test probe assembly has an improved mounting assembly which provides the test probe multi-directional freedom of movement with respect to a base in order to resist damage frequently caused to the test probe. The improved mounting assembly may, for example, include at least a first resilient mount disposed on the base and having at least a first support and at least a first resilient element. The at least a first resilient element, which may, for example, be at least a first spring, is deflectable when the test probe engages a structure, such as a device under testing (DUT). Accordingly, the improved test probe assembly of the invention can be deflected an infinite number of positions, in order to resist damage caused, for example, by misalignment between the probe and the DUT.

摘要翻译： 改进的测试探针组件具有改进的安装组件，其提供测试探针相对于基座的多方向运动自由度，以便抵抗经常对测试探针造成的损坏。 改进的安装组件可以例如包括设置在基座上的至少第一弹性支架，并且具有至少第一支撑件和至少第一弹性元件。 当测试探针接合诸如被测设备（DUT）的结构时，至少第一弹性元件（例如可以是至少第一弹簧）是可偏转的。 因此，本发明的改进的测试探针组件可以偏转无限数量的位置，以便抵抗例如由探针和被测物之间的对准引起的损伤。

公开(公告)号：US20060289190A1

公开(公告)日：2006-12-28

申请号：US11249409

申请日：2005-10-14

申请人： Winston Mok ,  Alexander Koch ,  Arkady Ivannikov

发明人： Winston Mok ,  Alexander Koch ,  Arkady Ivannikov

IPC分类号： H02G3/08 ,  H05K9/00

CPC分类号： G01R29/0821 ,  H05K9/0007

摘要： An RF isolation container that includes a counterweight system to assist an operator with opening and closing operations, an electromagnet locking mechanism for easier and consistent locking of the RF isolation container and a motion damping mechanism to relieve fatigue on operating components and on human operators.

摘要翻译： 一种RF隔离容器，其包括用于辅助操作者打开和关闭操作的配重系统，用于更容易且一致地锁定RF隔离容器的电磁体锁定机构和用于减轻操作部件和人类操作者的疲劳的运动阻尼机构。

公开(公告)号：US07807933B2

公开(公告)日：2010-10-05

申请号：US12117186

申请日：2008-05-08

申请人： Winston Mok ,  Alexander Koch ,  Arkady Ivannikov

发明人： Winston Mok ,  Alexander Koch ,  Arkady Ivannikov

IPC分类号： H05K9/00 ,  G01R31/02

CPC分类号： G01R29/0821 ,  H05K9/0007

摘要： An RF isolation container that includes a counterweight system to assist an operator with opening and closing operations, an electromagnet locking mechanism for easier and consistent locking of the RF isolation container and a motion damping mechanism to relieve fatigue on operating components and on human operators.

摘要翻译： 一种RF隔离容器，其包括用于辅助操作者打开和关闭操作的配重系统，用于更容易且一致地锁定RF隔离容器的电磁体锁定机构和用于减轻操作部件和人类操作者的疲劳的运动阻尼机构。

公开(公告)号：US20080012590A1

公开(公告)日：2008-01-17

申请号：US11780913

申请日：2007-07-20

申请人： Alexander Koch ,  Arkady Ivannikov ,  Ted Toth

发明人： Alexander Koch ,  Arkady Ivannikov ,  Ted Toth

IPC分类号： G01R1/067

CPC分类号： G01R1/06705

摘要： An improved test probe assembly has an improved mounting assembly which provides the test probe multi-directional freedom of movement with respect to a base in order to resist damage frequently caused to the test probe. The improved mounting assembly may, for example, include at least a first resilient mount disposed on the base and having at least a first support and at least a first resilient element. The at least a first resilient element, which may, for example, be at least a first spring, is deflectable when the test probe engages a structure, such as a device under testing (DUT). Accordingly, the improved test probe assembly of the invention can be deflected an infinite number of positions, in order to resist damage caused, for example, by misalignment between the probe and the DUT.

摘要翻译： 改进的测试探针组件具有改进的安装组件，其提供测试探针相对于基座的多方向运动自由度，以便抵抗经常对测试探针造成的损坏。 改进的安装组件可以例如包括设置在基座上的至少第一弹性支架，并且具有至少第一支撑件和至少第一弹性元件。 当测试探针接合诸如被测设备（DUT）的结构时，至少第一弹性元件（例如可以是至少第一弹簧）是可偏转的。 因此，本发明的改进的测试探针组件可以偏转无限数量的位置，以便抵抗例如由探针和被测物之间的对准引起的损伤。

公开(公告)号：US20090134899A1

公开(公告)日：2009-05-28

申请号：US12360323

申请日：2009-01-27

申请人： Alexander Koch ,  Arkady Ivannikov ,  Ted Toth

发明人： Alexander Koch ,  Arkady Ivannikov ,  Ted Toth

IPC分类号： G01R31/02

CPC分类号： G01R1/06705

摘要： An improved test probe assembly has an improved mounting assembly which provides the test probe multi-directional freedom of movement with respect to a base in order to resist damage frequently caused to the test probe. The improved mounting assembly may, for example, include at least a first resilient mount disposed on the base and having at least a first support and at least a first resilient element. The at least a first resilient element, which may, for example, be at least a first spring, is deflectable when the test probe engages a structure, such as a device under testing (DUT). Accordingly, the improved test probe assembly of the invention can be deflected an infinite number of positions, in order to resist damage caused, for example, by misalignment between the probe and the DUT.

摘要翻译： 改进的测试探针组件具有改进的安装组件，其提供测试探针相对于基座的多方向运动自由度，以便抵抗经常对测试探针造成的损坏。 改进的安装组件可以例如包括设置在基座上的至少第一弹性支架，并且具有至少第一支撑件和至少第一弹性元件。 当测试探针接合诸如被测设备（DUT）的结构时，至少第一弹性元件（例如可以是至少第一弹簧）是可偏转的。 因此，本发明的改进的测试探针组件可以偏转无限数量的位置，以便抵抗例如由探针和被测物之间的对准引起的损伤。