THERMAL HEATING DEVICE USING LIGHT FOR BINDER ACTIVATION AND ITS INTEGRATION IN PREFORMING DEVICE
    3.
    发明申请
    THERMAL HEATING DEVICE USING LIGHT FOR BINDER ACTIVATION AND ITS INTEGRATION IN PREFORMING DEVICE 审中-公开
    使用光束进行绑定激活的热加热装置及其在预装置中的集成

    公开(公告)号:WO2015185203A3

    公开(公告)日:2016-04-14

    申请号:PCT/EP2015001108

    申请日:2015-06-01

    Abstract: The invention relates to a binder material activating device (10) to activate a binder material (18) on a fibrous substrate (14), the binder material activating device (10) comprising a heat exposing device (20) to expose the fibrous substrate (14) with the binder material (18) to heat. The heat exposing device (20) comprises a non- focused light source (22) to provide a non-focused light beam (12) and an optics device (28) to be arranged in between the fibrous substrate (14) to be exposed to heat and the light source (22) to focus the non-focused light beam (12) onto the fibrous substrate (14). Further, the invention relates to a preforming device (40) comprising the binder material activating device (10).

    Abstract translation: 本发明涉及一种活化粘合剂材料(18)的粘合剂材料活化装置(10),该粘合剂材料活化装置(10)包括一个热曝光装置(20),用于暴露纤维基质( 14)与粘合剂材料(18)加热。 热曝光装置(20)包括非聚焦光源(22),以提供非聚焦光束(12)和光学装置(28),以布置在待暴露于 热和光源(22)将非聚焦光束(12)聚焦到纤维基底(14)上。 此外,本发明涉及包括粘合剂材料活化装置(10)的预成型装置(40)。

    DIRECT CURRENT SWITCHING DEVICE AND CONTROL METHOD
    4.
    发明申请
    DIRECT CURRENT SWITCHING DEVICE AND CONTROL METHOD 审中-公开
    DC控制器及其控制方法

    公开(公告)号:WO2016096101A2

    公开(公告)日:2016-06-23

    申请号:PCT/EP2015002450

    申请日:2015-12-04

    Abstract: The present invention relates particularly to a direct current switching device comprising at least one switching unit which can be mounted between two terminals. The device can further comprise at least one control unit for controlling the switching unit. The switching unit can comprise at least a first and a second semiconductor switching element, which can be mounted in parallel to each other, and the first switching element can be a high-voltage switching element and the second switching element can be a switching element with little power loss. The switching unit can be controlled by the control unit such that when the switching unit is switched off, first the second switching element can be switched to nonconductive and then the first switching element can be switched to nonconductive, and when the switching unit is switched on, first the first switching element can be switched to conductive and then the second switching element can be switched to conductive.

    Abstract translation: 本申请尤其涉及具有至少一个开关单元,其可以被布置在两个端子之间的直流开关装置。 此外,所述装置可以包括至少一个控制单元,用于控制切换单元。 开关单元可包括至少包括第一和第二半导体开关元件,其可以平行地布置成彼此,其特征在于,所述第一开关元件可以是高电压开关元件和第二开关元件可以是功率损耗,差开关元件。 开关单元可以是由,当开关单元断开第二开关元件不能在第一被打开,然后第一开关元件不能被导通,并且接通开关单元上的控制单元控制,所述第一开关元件可以被接通第一 和第二开关元件后可以打开。

    CHANGEABLE WING PROFILE
    5.
    发明申请
    CHANGEABLE WING PROFILE 审中-公开
    CHANGEABLE翼型

    公开(公告)号:WO2015007259A3

    公开(公告)日:2015-03-19

    申请号:PCT/DE2014000348

    申请日:2014-07-10

    Inventor: HASLACH HORST

    CPC classification number: B64C3/48 B64C9/00 B64C13/24 Y02T50/145

    Abstract: The invention relates to changes to wing profiles. In order to provide an aerodynamic structure that can be adapted and changed in many ways in terms of the wing profile, an aerodynamic structure (10) for a wing device or control surface device of an aircraft according to the invention has a supporting structure (12) and an outer skin (14). The supporting structure has a stationary spar (16) in the longitudinal direction, which spar extends from a root region to an outer end region. The supporting structure also has a plurality of adaptive framework segments (18) in the transverse direction, which each consist of a plurality of triangular compartments (20), which are arranged next to each other and are formed by control elements (22) of stationary length and control elements (24) of adjustable length. The framework segments are connected to the stationary spar. At least some of the triangular compartments have one of the adjustable control elements, at least on one side, such that the framework segments are adjustable in shape. The outer skin is fastened to the framework segments. An outer contour (26) of the aerodynamic structure can be changed at least in the transverse direction by adjusting the shape of the frameworks.

    Abstract translation: 本发明涉及的翼型变化。 为了提供可用的空气动力学结构,其能够在翼型和变化的角度来适应不同的,它提供了一个空气动力学结构(10),用于具有支撑结构(12)和外蒙皮(14)的飞行器的机翼或舵装置。 所述支撑结构包括在上从根部部分延伸到外端区域的固定梁(16)的纵向方向。 该支撑结构还具有在横向方向上的多个自适应桁架分段(18),各由多个固定在转向部件(22)的长度和在长度的转向元件(24)可调节形成的并置三角形隔间(20)的组成。 桁架段连接到所述固定轨道。 至少三角形隔室的一部分具有至少在所述可调节的导向元件的一侧上,以使桁架区段在它们的形状可调节的。 外皮被固定保持在桁架段。 通过调整桁架的形式的至少所述空气动力学结构的外轮廓(26)在横向方向上是可变的。

    TENT
    6.
    发明申请
    TENT 审中-公开
    帐篷

    公开(公告)号:WO2014154190A3

    公开(公告)日:2015-01-29

    申请号:PCT/DE2014000072

    申请日:2014-02-20

    CPC classification number: E04H15/02 A62B31/00 E04H2015/201

    Abstract: The invention relates to a tent (ZT), which comprises an outer covering (AH) and an air-tight inner covering (IH), having the following features: a connection module (AM) is integrated in an air-tight manner in the inner covering (IH), wherein said connection module (AM) has connection devices (A) for cables and/or hoses to supply appliances inside the tent, the outer covering (AH) has an opening such that the connection module (AM) is accessible from the outside.

    Abstract translation: 本发明涉及一个帐篷(ZT),其包括外护套(AH)和气密内部包装(1H),具有以下特点: - 在所述内壳(IH)是一个终端模块(AM)气密地结合,所述 连接模块(AM),用于电缆和/或软管连接装置的(a)具有对存在于帐篷内部供给器具, - 外部护套(AH)具有这样的开口,该终端模块(AM)是从外部接触。

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