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1. 发明授权

US06951320B2 Lock mechanism for securing a door kinematics system and process of operating same 失效
标题翻译：用于固定门运动系统的锁定机构及其操作过程
公开(公告)号：US06951320B2
公开(公告)日：2005-10-04
申请号：US10446134
申请日：2003-05-28
申请人： Wolfgang Buchs , Thangaraju Nithyanandam , Holger Schreitmueller
发明人： Wolfgang Buchs , Thangaraju Nithyanandam , Holger Schreitmueller
IPC分类号： B64C1/14 , E05B47/00 , E05B47/06
CPC分类号： E05B47/0657 , E05B47/0012 , E05B2047/0022
摘要： A device for locking a door kinematics system of the door of an airplane includes a control unit, an actuator for actuating a locking system and an automatic reset device. The control unit actuates the actuator as a function of the existence of a predetermined signal so that the actuator brings the locking system in a locking position. The reset device, if required, brings the locking system autonomously into a release position.
摘要翻译：用于锁定飞机门的门运动系统的装置包括控制单元，用于致动锁定系统的致动器和自动复位装置。控制单元根据预定信号的存在来致动致动器，使得致动器将锁定系统带入锁定位置。如果需要，复位装置使锁定系统自动进入释放位置。

2. 发明授权

US5667169A Door system, particularly for a passenger plane 失效
标题翻译：门系统，特别是客机
公开(公告)号：US5667169A
公开(公告)日：1997-09-16
申请号：US423508
申请日：1995-04-17
申请人： Hannes Erben , Wolfgang Buchs
发明人： Hannes Erben , Wolfgang Buchs
IPC分类号： B64C1/14 , E05C21/02
CPC分类号： B64C1/143 , B64C1/1407
摘要： A door system, particularly for a passenger plane, includes bearing and guiding device which operates between the door leaf and the door frame, as well as a lifting device which is arranged between the bearing and guiding device and the door leaf. The lifting device moves the door leaf at the end of the closing movement transversely to the moving path (B) of the guiding device with a form-locking engagement with door-frame-fixed receiving elements into the completely closed position and, at the start of the opening operation, in the opposite lifting direction (A) out of the form-locking engagement. The lifting device contains lifting kinematics for the control of the door blade lifting movement and an assigned lifting drive. In order to ensure a high safety standard and, at the same time, a simple weight-saving construction, the door leaf is provided with an electric drive unit for the lifting drive and a mechanically actuated lift securing device which can be cleared in parallel to the electric control of the lifting drive by a door opening command and locks the lifting device in the completely closed position automatically in a door-leaf-fixed manner.
摘要翻译：门系统，特别是用于客机的门系统包括在门扇和门框之间操作的轴承和引导装置，以及布置在轴承和引导装置与门扇之间的提升装置。提升装置在关闭运动结束时使门扇横向于导向装置的移动路径（B）移动，并与门框固定的接收元件形成锁定接合到完全关闭位置，并且在开始时的打开操作，在相反的提升方向（A）上脱离成形锁定接合。提升装置包含用于控制门扇提升运动的提升运动学和分配的起重驱动装置。为了确保高安全标准，同时，简单的节省重量的结构，门扇设有用于提升驱动的电动驱动单元和机械驱动的提升固定装置，可以平行清除通过门打开指令对提升驱动进行电控制，并以门扇固定的方式自动地将提升装置锁定在完全关闭位置。

3. 发明授权

US4334825A Elastomeric damping device especially for the neck of helicopter wing blades 失效
标题翻译：弹性阻尼装置，特别适用于直升机翼片的颈部
公开(公告)号：US4334825A
公开(公告)日：1982-06-15
申请号：US229538
申请日：1981-01-29
申请人： Dieter Braun , Wolfgang Buchs , Andreas Kirchner
发明人： Dieter Braun , Wolfgang Buchs , Andreas Kirchner
IPC分类号： F16F15/12 , B64C27/00 , B64C27/46 , B64C27/51 , F16F9/30 , F16F15/14 , B64C27/38
CPC分类号： F16F9/306 , B64C27/001 , B64C27/46 , B64C27/51
摘要： The neck of a hingeless helicopter rotor wing blade is provided with a damping device effective to dampen lead-lag movements of the rotor wing blade. For this purpose the damping device comprises at least two stiff plates secured to opposite sides of the blade neck by a plurality of elastomeric members glued or bonded to the respective stiff plate and to the blade neck at spaced intervals. The difference of deformation between the stiff plates and the blade neck causes a deformation of the individual members in directions substantially across the longitudinal blade direction (in lead-lag plane). The spacings between adjacent members are located where the damping action is inherently low.
摘要翻译：无铰链直升机转子翼片的颈部设置有有效地抑制转子翼片的超前滞后运动的阻尼装置。为此目的，阻尼装置包括至少两个刚性板，其通过多个弹性体构件固定到叶片颈部的相对侧，所述多个弹性构件以间隔的间隔胶合或粘合到相应的刚性板和叶片颈部。刚性板和叶片颈部之间的变形差异导致各个构件在基本上跨纵向叶片方向（在超前滞后平面中）的方向上的变形。相邻构件之间的间距位于阻尼作用固有地低的位置。

4. 发明授权

US4273818A Force infeed element for laminar panel assembly 失效
标题翻译：用于层板组装的强制进给元件
公开(公告)号：US4273818A
公开(公告)日：1981-06-16
申请号：US75993
申请日：1979-09-17
申请人： Wolfgang Buchs
发明人： Wolfgang Buchs
IPC分类号： B29D24/00 , B32B3/12 , B64C1/00 , H01L31/042
CPC分类号： B29D24/005 , B32B3/12 , Y10S136/292 , Y10T428/24149
摘要： A laminar panel assembly which is particularly useful in space vehicles for contact with solar cells includes a first and a second cover layer, a supporting core structure interposed between the cover layers and at least one force infeed element disposed within the core structure between the cover layers. The force infeed element includes at least one solid central piece for punctiform load infeed, and shear webs extending from the central piece radially outwardly in a branched formation such that the number of shear webs increases with increasing radial distance from the central piece.
摘要翻译：特别适用于与太阳能电池接触的太空车辆的层板组件包括第一和第二覆盖层，插入在所述覆盖层之间的支撑芯结构和设置在所述芯结构内的所述覆盖层之间的至少一个力进给元件。力进给元件包括用于点状加载进给的至少一个实心中心件，以及从中心件以分支形式径向向外延伸的剪力网，使得随着距离中心件的径向距离的增加，抗剪腹板的数量增加。

5. 发明授权

US08881524B2 Device for opening a passenger door in case of emergency 有权
标题翻译：紧急情况下打开乘客门的装置
公开(公告)号：US08881524B2
公开(公告)日：2014-11-11
申请号：US12921520
申请日：2009-03-02
申请人： Stefan Andres , Hans Bartosch , Wolfgang Buchs , Manfred Held , Rainer Hertle
发明人： Stefan Andres , Hans Bartosch , Wolfgang Buchs , Manfred Held , Rainer Hertle
IPC分类号： F01B29/08 , F02N13/00 , B64C1/14 , F42B3/04 , F42B3/00 , E05F15/12 , E05F15/04
CPC分类号： B64C1/1407 , E05F15/53 , E05F15/54 , E05F15/63 , E05F15/72 , E05Y2201/422 , E05Y2201/434 , E05Y2201/72 , E05Y2800/252 , E05Y2800/67 , E05Y2900/502 , E05Y2900/531 , F42B3/006 , F42B3/04
摘要： The invention relates to a device for opening a passenger door (1) of an aircraft in case of emergency, which is fastened so it is manually pivotable on the fuselage (3) of the aircraft via a hinge and/or support arm configuration (2), an auxiliary-energy-operated emergency opening drive (4) being provided between the fuselage (3) and the passenger door (1), which automatically opens the passenger door (1) in accordance with an emergency control unit (5), the auxiliary energy for the emergency opening drive (4) being pyrotechnic energy, whose gas expanding inside an expansion chamber (6) after triggering by the emergency control unit (5) impinges the emergency opening drive (4) with pressure medium to open the passenger door (1), wherein said emergency opening drive (4) generates a rotational movement.
摘要翻译：本发明涉及一种用于在紧急情况下打开飞机的乘客门（1）的装置，其被紧固以便可以通过铰链和/或支撑臂构造（2）手动地枢转在飞行器的机身（3）上），在机身（3）和乘客门（1）之间设置有辅助能量操作的应急开启驱动器（4），根据应急控制单元（5）自动打开乘客门（1）用于紧急打开驱动器（4）的辅助能量是烟火能量，其在由应急控制单元（5）触发之后在膨胀室（6）内扩张的气体用压力介质撞击紧急打开驱动器（4）以打开乘客门（1），其中所述紧急打开驱动器（4）产生旋转运动。

6. 发明申请

US20120025022A1 FUSELAGE STRUCTURE MADE OF COMPOSITE MATERIAL 有权
标题翻译：复合材料的熔敷结构
公开(公告)号：US20120025022A1
公开(公告)日：2012-02-02
申请号：US13191734
申请日：2011-07-27
申请人： Wolfgang Buchs , Gabriele Dreher , Umberto Girard , Steffen Kunze , Thomas Thiess
发明人： Wolfgang Buchs , Gabriele Dreher , Umberto Girard , Steffen Kunze , Thomas Thiess
IPC分类号： B64C1/14
CPC分类号： B64C1/1461 , B29C35/02 , B29C65/4835 , B29C65/5014 , B29C65/5021 , B29C65/5042 , B29C65/505 , B29C66/112 , B29C66/131 , B29C66/1312 , B29C66/43441 , B29C66/721 , B29C70/76 , B29D99/001 , B29L2031/3082 , B64C1/12 , B64C2001/0072 , Y02T50/43
摘要： A fuselage structure, particularly an aircraft door (1) of composite material comprising at least one panel (2) and at least one beam (3) mounted to each other and the panel (2) with the panel (2) being formed of at least one group of composite layers (5, 6, 20). The at least one beam (3) is provided at least at one of its respective ends (10, 11) with a flange (13) suitable for adhesive engagement with the at least one panel (2). The at least one group of composite layers (5, 6, 20) of the panel (2) is in form locking engagement with this flange (13) of the beam (3).
摘要翻译：一种机身结构，特别是复合材料的飞机门（1），其包括至少一个面板（2）和至少一个彼此安装的梁（3）和具有面板（2）的面板（2），所述面板（2）由至少一组复合层（5,6,20）。至少一个梁（3）至少在其相应的端部（10,11）中的一个上具有适于与所述至少一个面板（2）粘合接合的凸缘（13）。面板（2）的至少一组复合层（5,6,20）与梁（3）的该凸缘（13）形成锁定接合。

7. 发明授权

US4300354A Suspension system for a low temperature tank 失效
标题翻译：低温罐的悬挂系统
公开(公告)号：US4300354A
公开(公告)日：1981-11-17
申请号：US116888
申请日：1980-01-30
申请人： Wolfgang Buchs , Martin Mueller , Werner Malburg , Albert Seidel
发明人： Wolfgang Buchs , Martin Mueller , Werner Malburg , Albert Seidel
IPC分类号： F17C13/08 , F17C7/02
CPC分类号： F17C13/086 , F17C2201/0104 , F17C2203/01 , F17C2203/016 , F17C2203/0316 , F17C2203/0391 , F17C2203/0629 , F17C2205/0196 , F17C2209/228 , F17C2221/017 , F17C2223/0161 , F17C2223/033
摘要： A low temperature tank is suspended in an outer shell or container by a pality of straps of fiber compound materials. Each strap comprises a plurality of individual strap elements arranged in series. The strap elements are made of different fibers whereby the strap element closest to the tank is made of a fiber material having the lowest heat expansion coefficient as compared to the heat expansion coefficient of the other elements of a strap further away from the tank. Preferably the strap elements are thermally insulated from each other. In that case the strap elements need not necessarily be made of fiber materials having different heat expansion coefficients.
摘要翻译：低温罐通过多个纤维复合材料带悬挂在外壳或容器中。每个带包括串联布置的多个单独的带元件。带元件由不同的纤维制成，由此最靠近罐的带元件由与更远离罐的带的其它元件的热膨胀系数相比具有最低热膨胀系数的纤维材料制成。优选地，带元件彼此热绝缘。在这种情况下，带元件不一定由具有不同热膨胀系数的纤维材料制成。

8. 发明授权

US08622346B2 Fuselage structure made of composite material 有权
标题翻译：机身结构由复合材料制成
公开(公告)号：US08622346B2
公开(公告)日：2014-01-07
申请号：US13191734
申请日：2011-07-27
申请人： Wolfgang Buchs , Gabriele Dreher , Umberto Girard , Steffen Kunze , Thomas Thiess
发明人： Wolfgang Buchs , Gabriele Dreher , Umberto Girard , Steffen Kunze , Thomas Thiess
IPC分类号： B64C1/14
CPC分类号： B64C1/1461 , B29C35/02 , B29C65/4835 , B29C65/5014 , B29C65/5021 , B29C65/5042 , B29C65/505 , B29C66/112 , B29C66/131 , B29C66/1312 , B29C66/43441 , B29C66/721 , B29C70/76 , B29D99/001 , B29L2031/3082 , B64C1/12 , B64C2001/0072 , Y02T50/43
摘要： A fuselage structure, particularly an aircraft door (1) of composite material comprising at least one panel (2) and at least one beam (3) mounted to each other and the panel (2) with the panel (2) being formed of at least one group of composite layers (5, 6, 20). The at least one beam (3) is provided at least at one of its respective ends (10, 11) with a flange (13) suitable for adhesive engagement with the at least one panel (2). The at least one group of composite layers (5, 6, 20) of the panel (2) is in form locking engagement with this flange (13) of the beam (3).
摘要翻译：一种机身结构，特别是复合材料的飞机门（1），其包括至少一个面板（2）和至少一个彼此安装的梁（3）和具有面板（2）的面板（2），所述面板（2）由至少一组复合层（5,6,20）。至少一个梁（3）至少在其相应的端部（10,11）中的一个上具有适于与所述至少一个面板（2）粘合接合的凸缘（13）。面板（2）的至少一组复合层（5,6,20）与梁（3）的该凸缘（13）形成锁定接合。

9. 发明申请

US20110131986A1 DEVICE FOR OPENING A PASSENGER DOOR IN CASE OF EMERGENCY 有权
标题翻译：在紧急情况下打开乘客门的装置
公开(公告)号：US20110131986A1
公开(公告)日：2011-06-09
申请号：US12921520
申请日：2009-03-02
申请人： Stefan Andres , Hans Bartosch , Wolfgang Buchs , Manfred Held , Rainer Hertle
发明人： Stefan Andres , Hans Bartosch , Wolfgang Buchs , Manfred Held , Rainer Hertle
IPC分类号： B64C1/32 , F01B29/08 , E05F15/04 , B64C1/14 , B64D25/00
CPC分类号： B64C1/1407 , E05F15/53 , E05F15/54 , E05F15/63 , E05F15/72 , E05Y2201/422 , E05Y2201/434 , E05Y2201/72 , E05Y2800/252 , E05Y2800/67 , E05Y2900/502 , E05Y2900/531 , F42B3/006 , F42B3/04
摘要： The invention relates to a device for opening a passenger door (1) of an aircraft in case of emergency, which is fastened so it is manually pivotable on the fuselage (3) of the aircraft via a hinge and/or support arm configuration (2), an auxiliary-energy-operated emergency opening drive (4) being provided between the fuselage (3) and the passenger door (1), which automatically opens the passenger door (1) in accordance with an emergency control unit (5), the auxiliary energy for the emergency opening drive (4) being pyrotechnic energy, whose gas expanding inside an expansion chamber (6) after triggering by the emergency control unit (5) impinges the emergency opening drive (4) with pressure medium to open the passenger door (1), wherein said emergency opening drive (4) generates a rotational movement.
摘要翻译：本发明涉及一种用于在紧急情况下打开飞机的乘客门（1）的装置，其被紧固以便可以通过铰链和/或支撑臂构造（2）手动地枢转在飞行器的机身（3）上），在机身（3）和乘客门（1）之间设置有辅助能量操作的应急开启驱动器（4），根据应急控制单元（5）自动打开乘客门（1）用于紧急打开驱动器（4）的辅助能量是烟火能量，其在由应急控制单元（5）触发之后在膨胀室（6）内扩张的气体用压力介质撞击紧急打开驱动器（4）以打开乘客门（1），其中所述紧急打开驱动器（4）产生旋转运动。

10. 发明授权

US06729581B2 Supporting arm of a passenger door of an aircraft 有权
标题翻译：飞机乘客门的支撑臂
公开(公告)号：US06729581B2
公开(公告)日：2004-05-04
申请号：US10227540
申请日：2002-08-26
申请人： Wolfgang Buchs , Ralf Schmidt , Herbert Schramm , Bernd Wuest
发明人： Wolfgang Buchs , Ralf Schmidt , Herbert Schramm , Bernd Wuest
IPC分类号： B64C114
CPC分类号： B64C1/1407 , E05D3/12 , E05D9/00 , E05Y2900/502 , Y02T50/43
摘要： A supporting arm of a passenger door of an aircraft, has a curved structure which forms hollow chambers and movably connects the passenger door to a frame on the fuselage. Receiving means one for the supporting arm for receiving connecting means which enable a movable connection on the one hand to the passenger door and a pivoting drive and on the other hand to the frame on the fuselage, so that the door is movable by means of the supporting arm on a linear-displacement path and a pivoting path. The structure of the supporting arm is formed from fiber composite, the structure-forming fiber composite being formed from individual structural elements. This fiber composite structure further improves the thermal insulation of the supporting arm and nevertheless achieves a further weight reduction of the supporting arm, while maintaining exacting structural safety requirements for the latter.
摘要翻译：飞机乘客门的支撑臂具有弯曲的结构，其形成中空室并将乘客门可移动地连接到机身上的框架。接收装置是用于支撑臂的接收装置，用于接收连接装置，所述连接装置一方面可移动连接到乘客门，并且枢转驱动，另一方面可移动到机身上的框架，使得门可通过支撑臂在线性位移路径和枢转路径上。支撑臂的结构由纤维复合材料形成，结构形成纤维复合材料由单独的结构元件形成。这种纤维复合结构进一步提高了支撑臂的隔热性，并且还能够进一步减轻支撑臂的重量，同时保持后者的严格的结构安全性要求。

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