Reduction of parachute sail surface

    公开(公告)号:FR2731202A1

    公开(公告)日:1996-09-06

    申请号:FR9502671

    申请日:1995-03-02

    Applicant: PASCAL GERARD

    Abstract: The parachute sail double surface wing span is reduced by folding, in flight, one or more cavities onto themselves by a system of halyards (1) and internal pulleys (2). The halyards and pulleys are fastened on the inter-cavity partitions (3) to form a reduction zone and bring closer together these partitions when the halyards are pulled. The halyards are joined in a single cavity partition (4) in order to allow simultaneous pulling and locking by the parachutist. The anchoring point of one partition has an eyelet for fixing the halyard ends which then pass through holes in reduction zone partitions to join on to the pulleys

    Vehicle power unit mounting
    8.
    发明专利

    公开(公告)号:FR2776244A1

    公开(公告)日:1999-09-24

    申请号:FR9803710

    申请日:1998-03-20

    Abstract: Mounting has rigid struts (14,20,26,30) extending longitudinally from an attachment zone with one point attached to chassis and a spaced longitudinal point attached to the engine, which is lower than the first attachment zone.- DETAILED DESCRIPTION - In event of a front impact, the strut pivots at attachment zones about axis extending transversely from the vehicle where impact is transmitted along strut to guide the engine rearwards and down. One strut attachment zone is non-pivotal prior to the impact and the other has a vibration damper

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