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    APPAREIL DE SURVEILLANCE D’UN VOLET D’AERONEF ET APPLICATION D’UNE BROCHE DYNAMOMETRIQUE
    1.
    发明申请
    APPAREIL DE SURVEILLANCE D’UN VOLET D’AERONEF ET APPLICATION D’UNE BROCHE DYNAMOMETRIQUE 审中-公开
    用于监视飞机皮瓣的装置和动力学主轴的应用

    公开(公告)号：WO2004008097A2

    公开(公告)日：2004-01-22

    申请号：PCT/FR2003/002231

    申请日：2003-07-15

    Applicant: FGP INSTRUMENTATION ,  GIBERT, Francis

    Inventor： GIBERT, Francis

    IPC: G01L5/22

    CPC classification number: C04B38/103 ,  B64C9/02 ,  B64D45/0005 ,  B64D2045/001 ,  C04B2103/0028 ,  C09K8/473 ,  G01L1/2225 ,  G01L5/22 ,  C04B24/16 ,  C04B24/32 ,  C04B28/02 ,  C04B2103/40 ,  C04B2103/48

    Abstract: L'invention concerne la surveillance des volets. Elle se rapporte à une broche dynamométrique destinée à former un pivot de fixation d'un volet hypersustentateur, et qui possède un corps cylindrique (10) ayant une tête hexagonale (12) et un embout fileté (14). Les dimensions et autres caractéristiques du corps (10), de la tête (12) et de 1'embout (14) correspondent à celles des pivots normalement utilises pour la fixation de ces volets hypersustentateurs. Le corps (10) possède une gorge (16) qui peut avoir une faible profondeur, de quelques dixièmes de millimètre, et forme un simple dégagement qui empêche le contact entre une branche d'étrier ou un bras de volet et la broche au niveau de la gorge (16). Un élément sensible (18) est place au niveau de la gorge et est enfermé de manière très étanche. Application aux volets des aéronefs.

    Abstract translation: 本发明涉及快门监视。 它涉及到agrave; 一个准备使用的测力主轴 形成用于附接高升力襟翼的枢轴，并且具有圆柱形本体（10），该圆柱形本体（10）具有六边形头部（12）和螺纹端部件; （14）。 主体（10），头部（12）和端部（14）的尺寸和其他特征相互对应。 那些通常用于固定这些高升力襟翼的枢轴。 本体（10）具有凹槽（16），其可以具有几毫米的浅深度，并形成防止身体分支之间接触的简单间隙。 分类或者将百叶窗臂和主轴置于凹槽（16）处。 一个敏感的（18）被放置在咽喉的水平并被封闭。 以非常紧张的方式。 应用于飞机的百叶窗。

    APPARATUS FOR MONITORING AN AIRCRAFT FLAP AND APPLICATION OF A DYNAMOMETRIC ROD
    2.
    发明申请
    APPARATUS FOR MONITORING AN AIRCRAFT FLAP AND APPLICATION OF A DYNAMOMETRIC ROD 审中-公开
    用于监测飞机平面图和应用动态范围的装置

    公开(公告)号：WO2004008097A3

    公开(公告)日：2004-04-08

    申请号：PCT/FR0302231

    申请日：2003-07-15

    Applicant: FGP INSTRUMENTATION ,  GIBERT FRANCIS

    Inventor： GIBERT FRANCIS

    IPC: B64C9/02 ,  B64D45/00 ,  G01L1/22 ,  G01L5/22 ,  B64C13/00

    CPC classification number: C04B38/103 ,  B64C9/02 ,  B64D45/0005 ,  B64D2045/001 ,  C04B2103/0028 ,  C09K8/473 ,  G01L1/2225 ,  G01L5/22 ,  C04B24/16 ,  C04B24/32 ,  C04B28/02 ,  C04B2103/40 ,  C04B2103/48

    Abstract: The invention relates to aircraft flap monitoring. More specifically, the invention relates to a dynamometric rod which is intended to form a pivot for fixing a wing flap, said dynamometric rod comprising a cylindrical body (10) with a hexagonal head (12) and a threaded end-piece (14). The dimensions and other characteristics of the body (10), head (12) and end-piece (14) correspond to those of pivots normally used for fixing said wing flaps. The aforementioned body (10) is provided with a groove (16) which can be provided with a small depth of several tenths of a millimetre and which forms a simple gap which prevents contact between a branch of a clamp or an arm of the flap and the rod at the groove (16). In addition, a sensitive element (18) is positioned at the groove and is very tightly sealed closed. The invention is suitable for aircraft flaps.

    Abstract translation: 本发明涉及飞机翼片监测。 更具体地，本发明涉及一种旨在形成用于固定翼片的枢轴的测力杆，所述测力杆包括具有六角头（12）和螺纹端件（14）的圆柱体（10）。 主体（10），头部（12）和端部件（14）的尺寸和其他特征对应于通常用于固定翼片的枢轴的尺寸和其他特性。 上述主体（10）设置有可以设置有十分之几毫米的小深度的凹槽（16），并且形成一个简单的间隙，该间隙防止了夹子的一个分支或瓣片的一个臂的接触， 所述杆在所述凹槽（16）处。 此外，敏感元件（18）定位在凹槽处并且被非常紧密地密封封闭。 本发明适用于飞机襟翼。

    4.
    发明专利
    未知

    公开(公告)号：DE60317202T2

    公开(公告)日：2008-08-07

    申请号：DE60317202

    申请日：2003-07-15

    Applicant: FGP INSTRUMENTATION

    Inventor： GIBERT FRANCIS

    IPC: G01L5/22 ,  B64C9/02 ,  B64C13/00 ,  B64D45/00 ,  G01L1/22

    Abstract: A dynamometric rod intended to form a pivot for fixing an aircraft wing flap, includes a cylindrical body ( 10 ) with a hexagonal head ( 12 ) and a threaded end-piece ( 14 ). The dimensions and other characteristics of the body ( 10 ), head ( 12 ) and end-piece ( 14 ) correspond to those of pivots normally used for fixing wing flaps. The aforementioned body ( 10 ) is provided with a groove ( 16 ) which can be provided with a small depth of several tenths of a millimetre and which forms a simple gap which prevents contact between a branch of a clamp or an arm of the flap and the rod at the groove ( 16 ). In addition, a sensitive element ( 18 ) is positioned at the groove and is very tightly sealed closed. The invention is suitable for aircraft flaps.

    5.
    发明专利
    未知

    公开(公告)号：FR2842598A1

    公开(公告)日：2004-01-23

    申请号：FR0209006

    申请日：2002-07-16

    Applicant: FGP INSTRUMENTATION

    Inventor： GIBERT FRANCIS JEAN PAUL

    IPC: B64C9/02 ,  B64D45/00 ,  G01L1/22 ,  G01L5/22

    Abstract: A dynamometric rod intended to form a pivot for fixing an aircraft wing flap, includes a cylindrical body ( 10 ) with a hexagonal head ( 12 ) and a threaded end-piece ( 14 ). The dimensions and other characteristics of the body ( 10 ), head ( 12 ) and end-piece ( 14 ) correspond to those of pivots normally used for fixing wing flaps. The aforementioned body ( 10 ) is provided with a groove ( 16 ) which can be provided with a small depth of several tenths of a millimetre and which forms a simple gap which prevents contact between a branch of a clamp or an arm of the flap and the rod at the groove ( 16 ). In addition, a sensitive element ( 18 ) is positioned at the groove and is very tightly sealed closed. The invention is suitable for aircraft flaps.

    10.
    发明专利
    未知

    公开(公告)号：DE60317202D1

    公开(公告)日：2007-12-13

    申请号：DE60317202

    申请日：2003-07-15

    Applicant: FGP INSTRUMENTATION

    Inventor： GIBERT FRANCIS

    IPC: G01L5/22 ,  B64C9/02 ,  B64C13/00 ,  B64D45/00 ,  G01L1/22

    Abstract: A dynamometric rod intended to form a pivot for fixing an aircraft wing flap, includes a cylindrical body ( 10 ) with a hexagonal head ( 12 ) and a threaded end-piece ( 14 ). The dimensions and other characteristics of the body ( 10 ), head ( 12 ) and end-piece ( 14 ) correspond to those of pivots normally used for fixing wing flaps. The aforementioned body ( 10 ) is provided with a groove ( 16 ) which can be provided with a small depth of several tenths of a millimetre and which forms a simple gap which prevents contact between a branch of a clamp or an arm of the flap and the rod at the groove ( 16 ). In addition, a sensitive element ( 18 ) is positioned at the groove and is very tightly sealed closed. The invention is suitable for aircraft flaps.

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