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    Cylinder head gasket for internal combustion engines
    3.
    发明授权
    Cylinder head gasket for internal combustion engines 失效
    内燃机气缸盖垫片

    公开(公告)号：US4312512A

    公开(公告)日：1982-01-26

    申请号：US113322

    申请日：1980-01-18

    Applicant: Jean-Francois Conte ,  Henri Carles

    Inventor： Jean-Francois Conte ,  Henri Carles

    IPC: F16J15/08 ,  F16J15/12

    CPC classification number: F16J15/123 ,  F16J15/0825 ,  F16J15/12 ,  F05C2225/02 ,  F16J2015/0856

    Abstract: A cylinder gasket having three flat metal foils connected together. The fluid passages between the cylinder head and engine block are sealed by forming a centrally located first aperture in the two external flat metal foils. A smaller second aperture, centrally located to the first aperture, is formed in the central flat metal foil so as to form first and second flat zones. In the preferred embodiment, an elastomer band is attached to the central flat metal foil around the periphery of the second aperture and the first and second flat zones to seal the fluid passages. The cylinder lining is sealed by a second ring member with an external round lip. The second ring member is mounted in a third aperture in the two external flat metal foils centrally located with the cylinder lining. The external round lip is sandwiched between the two external flat metal foils and a fourth aperture in the central flat metal foil which is centrally located with the third aperture. An escape channel is provided to vent gases to the exterior of the engine. In an alternate embodiment, a C shaped circular member is attached to the central flat metal foil around the periphery of the second aperture. A metal ring is interposed the C shaped circular member and first ring member.

    Abstract translation: 具有连接在一起的三个扁平金属箔的气缸垫圈​​。 气缸盖和发动机缸体之间的流体通道在两个外部扁平金属箔中形成位于中心的第一孔密封。 在中心平坦的金属箔中形成有较小的第二孔，位于第一孔的中央，以便形成第一和第二平坦区。 在优选实施例中，弹性体带围绕第二孔和第一和第二平坦区的周边连接到中央扁平金属箔上以密封流体通道。 气缸衬套由具有外圆唇的第二环构件密封。 第二环构件安装在位于圆筒衬里中心的两个外部平面金属箔的第三孔中。 外部圆形唇缘夹在两个外部扁平金属箔之间，中心平坦金属箔中的第四个孔位于第三个孔的中心位置。 提供排气通道以将气体排放到发动机的外部。 在替代实施例中，C形圆形构件围绕第二孔的周边连接到中央扁平金属箔。 金属环插入C形圆形构件和第一环构件。

    ATTACHMENT STRUCTURE FOR A TURBOJET ENGINE
    5.
    发明申请
    ATTACHMENT STRUCTURE FOR A TURBOJET ENGINE 审中-公开
    涡轮发动机的附件结构

    公开(公告)号：US20110308257A1

    公开(公告)日：2011-12-22

    申请号：US12921239

    申请日：2009-01-09

    Applicant: Guy Bernard Vauchel ,  Andre Baillard ,  Francois Conte

    Inventor： Guy Bernard Vauchel ,  Andre Baillard ,  Francois Conte

    IPC: F02C7/20

    CPC classification number: B64D27/26 ,  B64D2027/264

    Abstract: The present invention relates to an attachment structure (1) for attaching a turbojet engine (2) to a fixed structure of an airplane via an attachment pylon, characterized in that it comprises a one-piece box section intended to extend at least partially on each side of a fan casing (3) of the turbojet engine about a substantially longitudinal axis thereof and comprising, on the one hand, means of attachment to the pylon and, on the other hand, means of attachment of the engine (4) which are positioned on the box section on each side of a substantially longitudinal axis of the turbojet engine and are intended to be connected to part of the turbojet engine in such a way as to react the forces applied thereto.

    Abstract translation: 本发明涉及一种用于通过附接塔将涡轮喷气发动机（2）附接到飞机的固定结构的附接结构（1），其特征在于，其包括一个整体的箱部分，其旨在至少部分地延伸到每个 涡轮喷气发动机的风扇壳体（3）的大致纵向轴线的侧面，一方面包括附接到塔架的装置，另一方面，包括附接发动机（4）的装置 定位在涡轮喷气发动机的基本上纵向轴线的每一侧上的箱部分上，并且旨在以与施加到其上的力反应的方式连接到涡轮喷气发动机的一部分。

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