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    • 1. 发明授权
    • Closed loop control system for controlling an air discharge out of an
aircraft body
    • 用于控制从飞行器机体排出空气的闭环控制系统
    • US5934614A
    • 1999-08-10
    • US891519
    • 1997-07-11
    • Wolfgang MuellerBernd Klein
    • Wolfgang MuellerBernd Klein
    • B64D13/04
    • B64D13/04Y02T50/44
    • The flow volume of used air to be discharged from an aircraft cabin is controlled in a valve control system in which each outflow valve has at least two slave controllers responsive to any one of at least two master controllers in a closed loop control system. For this purpose the slave controllers and the master controllers are interconnected by an intermeshed conductor network including a plurality of conductor sections interconnected by electrical conductor junctions or optical conductor couplers forming interfaces between the conductor sections to provide a redundant number of communication paths to keep the system operable even if failures or faults occur.
    • 要从飞机机舱排出的用过的空气的流量在阀控制系统中被控制,其中每个流出阀具有响应于闭环控制系统中的至少两个主控制器中的任何一个的至少两个从属控制器。 为此,从控制器和主控制器通过相互啮合的导体网络相互连接,该网络包括通过电导体接头互连的多个导体部分或形成导体部分之间的接口的光导体耦合器,以提供冗余数量的通信路径以保持系统 即使发生故障或故障也可以操作。
    • 2. 发明授权
    • System for preventing the automatic opening of an improperly closed and
locked aircraft door
    • 防止自动打开不正确关闭和锁定的飞机门的系统
    • US5480109A
    • 1996-01-02
    • US210629
    • 1994-03-18
    • Bernd KleinWolfgang Mueller
    • Bernd KleinWolfgang Mueller
    • B64C1/14E05B45/06
    • B64C1/1407Y10S292/65
    • A system for preventing the automatic or inadvertent opening of an aircraft door or access hatch that has not been closed and locked properly provides an increase in the overall flight safety of aircraft. The system includes a door monitoring system (1), which is connected to at least one of a cabin pressure control arrangement (4), a cabin temperature control arrangement (5), and an air tap system control arrangement (36). The door monitoring system (1) provides a signal indicating if at least one door or access hatch is not properly closed and locked. The controllers (4, 5, 36) receive the door monitor signal at respective inputs and also receive information necessary for determining the current flight configuration of the aircraft from various other aircraft systems, such as a landing gear control arrangement or an engine monitor arrangement. The controllers (4, 5, 36) evaluate the several input signals and provide output signals for controlling at least one of a cabin air venting valve, a cabin air flow control valve, and a tap air shut-off valve.
    • 一种用于防止未正确关闭和锁定的飞机门或进入舱的自动或无意打开的系统提供了飞机的整体飞行安全性的增加。 该系统包括门监视系统(1),该系统连接至机舱压力控制装置(4),机舱温度控制装置(5)和空气抽头系统控制装置(36)中的至少一个。 门监控系统(1)提供一个信号,指示至少一个门或接入舱是否没有被正确关闭和锁定。 控制器(4,5,6)在相应的输入处接收门监控信号,并且还接收从各种其他飞行器系统(诸如起落架控制装置或发动机监视装置)确定飞机当前飞行配置所需的信息。 控制器(4,5,6)评估多个输入信号并提供用于控制机舱通气阀,客舱空气流量控制阀和抽气断气阀中的至少一个的输出信号。
    • 8. 发明授权
    • Test carrier for analysis of fluids
    • 测试载体用于分析流体
    • US5258163A
    • 1993-11-02
    • US960222
    • 1992-10-13
    • Manfred KrauseBernd KleinGerhard SchindlerPeter SchaferSiegfried Notzel
    • Manfred KrauseBernd KleinGerhard SchindlerPeter SchaferSiegfried Notzel
    • G01N33/52G01N33/543
    • G01N33/54386G01N33/525G01N33/528Y10S435/805Y10S435/97
    • Test carrier for the analysis of fluids with a frame (2) consisting of at least two parts surrounding a test field opening (6) and with a test field disposed in the test field opening (6). In order to provide such a test carrier with frame with which it is possible to assemble the test field out of several test layers manufactured separately from one another, it is proposed that the test field be designed as a test layer package (7) with test layers (10, 11, 12) resting loosely on one another, the frame (2) comprise two shaped pieces of plastics material, one of which serves as base part (4) and comprises a seat (16) for accommodating the test layers (10, 11, 12), while the other serves as lid part (3) and comprises a bearing surface (17) resting on the topmost layer (10) of the test layer package (7). The lid part (3) and the base part (4) are in addition designed with elastic properties so that the pressure with which the bearing surface (17) presses onto the test layer package (7) is substantially constant in the tolerance range of the thickness of the test field package (7).
    • 用于分析流体的测试载体,框架(2)由围绕测试场开口(6)的至少两个部分组成,并且具有设置在测试场开口(6)中的测试场。 为了提供这种具有框架的测试载体,可以通过框架来组装彼此分开制造的几个测试层的测试场,建议将测试场设计为具有测试的测试层封装(7) 所述框架(2)包括两个成形的塑料件,其中一个塑料件用作基座部分(4),并且包括用于容纳测试层的座(16) 10,11,12),而另一个用作盖部分(3),并且包括搁置在测试层封装(7)的最上层(10)上的支承表面(17)。 盖部分(3)和基部部分(4)另外设计有弹性特性,使得支承表面(17)压在测试层包装(7)上的压力在 测试场包装的厚度(7)。