公开(公告)号：US5407099A

公开(公告)日：1995-04-18

申请号：US961684

申请日：1994-03-09

Applicant: Karl-Heinrich Heuke ,  Guenter Schmitz

Inventor： Karl-Heinrich Heuke ,  Guenter Schmitz

IPC: B65D75/58 ,  B67B7/24

CPC classification number: B65D75/5877 ,  B67B7/26

Abstract: A sealing member inside the bag and a withdrawing member outside the bag can be interplugged and cooperate by complimentary conical sealing surfaces to dispense flowable material from the bag. A retaining member is attached to the outer side of the bag wall and clamps a portion of the bag wall between the retaining member and the sealing member to allow a plastic deformation of that portion by the withdrawing member until it ruptures.

Abstract translation: PCT No.PCT / US91 / 03911 Sec。 371日期1994年3月9日 102（e）1994年3月9日PCT PCT 1991年6月3日PCT公布。 第WO92 / 00895号公报 日期：1992年1月23日。袋内的密封构件和袋外的取出构件可以通过互补的锥形密封表面被插入并配合，以从袋中分配可流动的材料。 保持构件附接到袋壁的外侧，并且夹持在保持构件和密封构件之间的袋壁的一部分，以允许该部分由抽出构件塑性变形直到破裂。

公开(公告)号：US20120022820A1

公开(公告)日：2012-01-26

申请号：US12934721

申请日：2009-04-17

Applicant: Guenter Schmitz ,  Tim Schmitz

Inventor： Guenter Schmitz ,  Tim Schmitz

IPC: G06F15/00

CPC classification number: G01C21/165

Abstract: The invention relates to a method for underwater navigation, particularly for scuba divers, and for autonomous, manned, or remote-controlled underwater vessels, wherein the signals of at least one sensor, comprising at least one acceleration sensor for determining the actual position, are integratively analyzed, accuracy is improved by means of the use of reference measurements, and a correction is carried out by way of a correction vector obtained from the transformation of the vector of the accelerations measured by the acceleration sensor in the diving computer coordinate system into the global coordinate system, the comparison to at least one of the reference measurement values, the determination of the deviation and the reverse transformation of the deviation to the diving computer coordinate system.

Abstract translation: 本发明涉及一种用于水下航行的方法，特别是用于水肺潜水员和用于自主的，载人的或远程控制的水下血管的方法，其中包括至少一个用于确定实际位置的加速度传感器的至少一个传感器的信号是 综合分析，通过使用参考测量来提高精度，并且通过从由潜水计算机坐标系中的加速度传感器测量的加速度向量的变换获得的校正矢量进行校正，进入 全局坐标系，与至少一个参考测量值的比较，偏差的确定和与潜水计算机坐标系的偏差的反向变换。

公开(公告)号：US20110033690A1

公开(公告)日：2011-02-10

申请号：US12936057

申请日：2009-02-17

Applicant: Guenter Schmitz

Inventor： Guenter Schmitz

IPC: C09K11/02 ,  B32B27/38 ,  B05D3/10 ,  B32B27/08 ,  B32B15/092 ,  B32B17/10 ,  B32B18/00 ,  B32B21/08

CPC classification number: C09D7/1216 ,  C04B35/44 ,  C04B2235/3206 ,  C04B2235/3208 ,  C04B2235/3213 ,  C04B2235/3215 ,  C04B2235/3224 ,  C04B2235/76 ,  C08K3/10 ,  C09D5/22 ,  C09D7/61 ,  C09D7/69 ,  C09K11/02 ,  C09K11/7706 ,  C09K11/7734 ,  C09K11/7792 ,  Y10T428/31511 ,  Y10T428/31525 ,  Y10T428/31529

Abstract: The present invention relates to an afterglow coating comprising a clear varnish and a photoluminescent pigment, wherein the pigment comprises a white luminous colour in which the clear varnish is distributed. The present invention furthermore relates to methods for producing these coatings and to their use for coating surfaces in the cabin of aircraft.

Abstract translation: 本发明涉及一种包含透明清漆和光致发光颜料的余辉涂层，其中颜料包括其中分布透明清漆的白色发光颜色。 本发明还涉及制造这些涂层的方法及其用于在飞机机舱中涂覆表面的用途。

公开(公告)号：US20080029667A1

公开(公告)日：2008-02-07

申请号：US11832882

申请日：2007-08-02

Applicant: Guenter Schmitz

Inventor： Guenter Schmitz

IPC: F16B21/02

CPC classification number: F16B2/185 ,  Y10T24/44026 ,  Y10T403/591 ,  Y10T403/75

Abstract: A plug and a method for fixing at least two devices, includes a tension element, a pin, a lever element and a compression element. In one example, the tension element includes a tension stamp on a first end and a coupling member on a second end and a lever element includes a first sliding and a coupling element, with the pin coupling the lever element with the tension element. A compression element having an area-shaped contact that is capable of sliding onto the tension element until the area-shaped contact contacts the tension stamp. When the lever element is coupled to the tension element by a pin and is engaged by using a lever movement, a compression element is compressed by shortening a distance between the tension stamp and the lever element.

Abstract translation: 用于固定至少两个装置的插头和方法包括张紧元件，销，杠杆元件和压缩元件。 在一个示例中，张紧元件包括在第一端上的张紧印模和在第二端上的联接构件，并且杠杆元件包括第一滑动件和联接元件，销钉将杠杆元件与张力元件连接。 具有能够滑动到张力元件上的区域形状的接触件的压缩元件，直到该区域形状的接触件接触张紧印模。 当杠杆元件通过销联接到张紧元件并且通过使用杠杆运动而接合时，压缩元件通过缩短张紧印模和杠杆元件之间的距离而被压缩。

公开(公告)号：US09243151B2

公开(公告)日：2016-01-26

申请号：US12936057

申请日：2009-02-17

Applicant: Guenter Schmitz

Inventor： Guenter Schmitz

IPC: C09K11/02 ,  B32B27/38 ,  B05D3/10 ,  B32B27/08 ,  B32B15/092 ,  B32B17/10 ,  B32B18/00 ,  B32B21/08 ,  C09D7/12 ,  C09D5/22 ,  C09K11/77 ,  C04B35/44 ,  C08K3/00

CPC classification number: C09D7/1216 ,  C04B35/44 ,  C04B2235/3206 ,  C04B2235/3208 ,  C04B2235/3213 ,  C04B2235/3215 ,  C04B2235/3224 ,  C04B2235/76 ,  C08K3/10 ,  C09D5/22 ,  C09D7/61 ,  C09D7/69 ,  C09K11/02 ,  C09K11/7706 ,  C09K11/7734 ,  C09K11/7792 ,  Y10T428/31511 ,  Y10T428/31525 ,  Y10T428/31529

Abstract: The present invention relates to an afterglow coating comprising a clear varnish and a photoluminescent pigment, wherein the pigment comprises a white luminous color in which the clear varnish is distributed. The present invention furthermore relates to methods for producing these coatings and to their use for coating surfaces in the cabin of aircraft.

Abstract translation: 本发明涉及一种包含透明清漆和光致发光颜料的余辉涂层，其中颜料包括其中分布透明清漆的白色发光颜色。 本发明还涉及制造这些涂层的方法及其用于在飞机机舱中涂覆表面的用途。

公开(公告)号：US08690453B2

公开(公告)日：2014-04-08

申请号：US13008585

申请日：2011-01-18

Applicant: Guenter Schmitz

Inventor： Guenter Schmitz

IPC: G02B6/36

CPC classification number: H01R43/26 ,  G02B6/3817 ,  G02B6/389 ,  G02B6/3897 ,  H01R13/6273 ,  H01R2201/26

Abstract: The present invention relates to a plug/socket arrangement, in particular an electrical and/or optical plug/socket arrangement of an aircraft or spacecraft, which comprises a housing and at least one insert which can be received in the housing. It further comprises a releasable connection means which is adjustable between a locked position, in which the insert and the housing are locked to one another, and an unlocked position, in which the insert and the housing are not locked to one another; and an adjustment member which is adjustable between an inoperative position, in which the adjustment member is not operatively connected to the connection means, and a release position, in which the adjustment member is operatively connected to the connection means for releasing the locked position into the unlocked position of the connection means.

Abstract translation: 本发明涉及一种插头/插座装置，特别是飞行器或航天器的电气和/或光学插头/插座装置，其包括壳体和可容纳在壳体中的至少一个插入件。 它还包括一个可释放的连接装置，该连接装置可以在插入件和壳体彼此锁定的锁定位置和锁定位置之间调节，在该位置，插入件和壳体彼此不锁定; 以及调节构件，其可在调节构件不可操作地连接到连接装置的非工作位置和释放位置之间可调节，在该位置中，调节构件可操作地连接到连接装置，以将锁定位置释放到 连接装置的解锁位置。

公开(公告)号：US06404209B1

公开(公告)日：2002-06-11

申请号：US09597068

申请日：2000-06-20

Applicant: Juergen Klattenhoff ,  Guenter Schmitz ,  Holger Schroeter

Inventor： Juergen Klattenhoff ,  Guenter Schmitz ,  Holger Schroeter

IPC: G01R2700

CPC classification number: G01F23/243 ,  G01R17/02

Abstract: A measuring instrument (11) for fill level sensors (4) having a measuring electrode (6) and a compensating electrode (9). The measuring instrument (11) has a bridge circuit whose one bridge branch (21) is formed by two series-connected test resistors (23, 24). The other bridge branch (22) is formed by the measuring resistor (17) on the measuring electrode (6) and the compensating resistor (18) on the compensating electrode (9). Between the two bridge branches (21, 22) a diagonal line (26) with a test switch (27) is provided. The measuring instrument (11) is controlled by the control circuit (13) so that the diagonal line (26) is closed outside of preset test time periods, and interrupted at preset test time periods. The end of the diagonal line (26) located between the two test resistors (23, 24) is connected to the base potential (25) of the measuring circuit (12). The resistors (17, 18, 23, 24) are designed so that when the test switch (27) is closed, the imbalance of the bridge is determined by the second bridge branch (22), whereas when the test switch (27) is open, the imbalance of the bridge is determined by the first bridge branch (21), simulating in this way a situation in which the fill level has dropped below the limit value. The control circuit (13) provides an error signal if the signal of measuring circuit (12) is not corresponding. In this way, the measuring instrument (11) automatically tests its functionality.

Abstract translation: 一种用于具有测量电极（6）和补偿电极（9）的填充液位传感器（4）的测量仪器（11）。 测量仪器（11）具有桥式电路，其桥式分支（21）由两个串联连接的测试电阻（23,24）形成。 另一桥分支（22）由测量电极（6）上的测量电阻（17）和补偿电极（9）上的补偿电阻（18）形成。 在两个桥接支路（21,22）之间，提供了带有测试开关（27）的对角线（26）。 测量仪器（11）由控制电路（13）控制，使得对角线（26）在预设测试时间段之外关闭，并在预设的测试时间段中断。 位于两个测试电阻器（23,24）之间的对角线（26）的端部连接到测量电路（12）的基极（25）。 电阻器（17,18,23,24）被设计成使得当测试开关（27）闭合时，桥接器的不平衡由第二桥接支路（22）确定，而当测试开关（27）为 开放，桥梁的不平衡由第一桥梁分支（21）确定，模拟这种填充水平已经降到极限值以下的情况。 如果测量电路（12）的信号不对应，则控制电路（13）提供误差信号。 以这种方式，测量仪器（11）自动测试其功能。

公开(公告)号：US6003481A

公开(公告)日：1999-12-21

申请号：US68083

申请日：1998-08-04

Applicant: Franz Pischinger ,  Martin Pischinger ,  Thomas Esch ,  Guenter Schmitz

Inventor： Franz Pischinger ,  Martin Pischinger ,  Thomas Esch ,  Guenter Schmitz

IPC: F01L9/04

CPC classification number: F01L9/04

Abstract: An electromagnetic actuator for actuating a gas-exchange valve in a reciprocating internal combustion engine, the electromagnetic actuator comprising: an armature which is operatively connected to the gas-exchange valve; two electromagnets, each having a pole face; two oppositely oriented restoring springs; wherein the armature is guided in a reciprocating manner counter to the force of the two oppositely oriented restoring springs between the pole faces of the two electromagnets whose current supply can be controlled by a control device, the two electromagnets being disposed in mutual spacing and acting as opening and closing devices; and at least one additional mass which is associated with the gas-exchange valve and can be guided so that it is movable relative thereto and in the same direction of the gas-exchange valve, the at least one additional mass entering into operative connection with the gas-exchange valve, in the final phase of the armature's motion in the direction of a respective one of the two electromagnets, via a coupler.

Abstract translation: PCT No.PCT / EP97 / 04565 Sec。 371日期：1998年8月4日 102（e）日期1998年8月4日PCT 1997年8月22日PCT公布。 WO98 / 10175 PCT出版物 日期1998年3月12日，一种用于致动往复式内燃机中的气体交换阀的电磁致动器，该电磁致动器包括：可操作地连接到气体交换阀的电枢; 两个电磁铁，各有一个极面; 两个相对定向的复原弹簧; 其中电枢以往复方式被引导，与两个电磁体的极面之间的两个相对定向的复位弹簧的力相反，电磁铁的电流可由控制装置控制，两个电磁铁相互间隔设置， 开闭装置; 以及与气体交换阀相关联的至少一个附加质量块，并且可以被引导以使得其相对于其移动并沿气体交换阀的相同方向移动，所述至少一个附加质量体与 在两个电磁体中的相应一个方向上的电枢运动的最后阶段中，通过耦合器。

公开(公告)号：US09046118B2

公开(公告)日：2015-06-02

申请号：US13148440

申请日：2010-02-10

Applicant: Guenter Schmitz

Inventor： Guenter Schmitz

IPC: F16D1/00 ,  F16B2/18 ,  F16B21/09

CPC classification number: F16B2/185 ,  F16B21/09 ,  Y10T403/55

Abstract: A fastening device for attaching a module element to a support structure in an aircraft includes a stud having a first end defining a broadened head configured to engage the support structure, a section which adjoins the head and defines a first lateral dimension and a second lateral dimension that is larger than, and is disposed at least substantially perpendicularly to, the first lateral dimension, and a second opposite end connected to a lever which is movable between open and closed positions relative to the stud. A bushing, which may be electrically conductive, is provided on and longitudinally movable along the stud, which is configured to contact the support structure and to support an outer wall of the module element. An eccentric may be actuated by the lever and is responsive to movement of the lever into the closed position to move the bushing along the stud towards the head.

Abstract translation: 用于将模块元件附接到飞行器中的支撑结构的紧固装置包括：螺柱，其具有限定扩展头部的第一端部，该头部构造成接合支撑结构;邻接头部并且限定第一横向尺寸和第二横向尺寸 其大于并且至少基本上垂直于第一横向尺寸设置，以及连接到杆的第二相对端，其可相对于螺栓在打开位置和关闭位置之间移动。 可以是导电的衬套沿着螺柱设置并且可沿纵向移动，所述螺柱被构造成接触支撑结构并支撑模块元件的外壁。 偏心轮可以由杠杆致动并且响应于杠杆进入关闭位置的运动，以使衬套沿螺柱朝向头部移动。

公开(公告)号：US08485486B2

公开(公告)日：2013-07-16

申请号：US12959923

申请日：2010-12-03

Applicant: Christian Riedel ,  Guenter Schmitz

Inventor： Christian Riedel ,  Guenter Schmitz

IPC: F16M11/10

CPC classification number: B60R11/0235 ,  B60R2011/0028 ,  B60R2011/0082 ,  B60R2011/0092 ,  B64D11/0015

Abstract: A display mount is provided for a vehicle, such an aircraft. The display mount includes, but is not limited to a support frame and a display accommodation device. The support frame is designed for incorporation in a supply channel, and the display accommodation device is designed to receive a display. The display accommodation device is connected to the support frame such that the display accommodation device is movable with a combined rotational movement and translational movement relative to the support frame between a first operating position and a second operating position.

Abstract translation: 为这种飞行器的车辆提供显示器支架。 显示器支架包括但不限于支撑框架和显示器容纳装置。 支撑框架设计用于结合在供应通道中，并且显示器容纳装置被设计成接收显示器。 显示器容纳装置连接到支撑框架，使得显示容纳装置可以在第一操作位置和第二操作位置之间相对于支撑框架的组合的旋转运动和平移运动而移动。