首页> 外国专利> FLEXIBLE WING FOR A PARACHUTE OR AN APPARATUS FOR SLOPE FLIGHT, ASCENT FLIGHT OR MOTORIZED FLIGHT

FLEXIBLE WING FOR A PARACHUTE OR AN APPARATUS FOR SLOPE FLIGHT, ASCENT FLIGHT OR MOTORIZED FLIGHT

机译:用于降落伞,上升飞行或机动飞行的降落伞或装置的柔性翼

摘要

Parachute wing with a particularly performing aerodynamic configuration and capable of keeping such configuration when the flight conditions are disturbed. The wing (1) comprises open cells (6) which are open at the leading edge and closed at the trailing edge (2), and closed cells (13) which are swollen from the open cells. The ribs (16) separating these two types of cells have air inlet orifices (17) which are provided with anti-return valves. Thus, the closed cells (13) remain swollen and keep their configuration if the pressure drops in the front openings (14) of the open cells. Furthermore, their leading edge (15) may have an appropriate shape and their profile may be thinner than that of the open cells. The invention is applicable to parachutes or crafts for hill flight, climbing flight or even motor flight.
机译:降落伞机翼具有特别出色的空气动力学构造,并且在飞行条件受到干扰时能够保持这种构造。机翼(1)包括在前缘处敞开而在后缘(2)处封闭的开孔(6),以及从开孔膨胀的闭孔(13)。分隔这两种类型的电池的肋(16)具有进气孔(17),该进气孔设有止回阀。因此,如果压力在开孔的前开口(14)中下降,则闭孔(13)保持膨胀并保持其构造。此外,它们的前边缘(15)可以具有适当的形状,并且它们的轮廓可以比敞开的单元的轮廓薄。本发明适用于用于降落飞行,爬升飞行甚至机动飞行的降落伞或飞行器。

著录项

  • 公开/公告号FR2610288A1

    专利类型

  • 公开/公告日1988-08-05

    原文格式PDF

  • 申请/专利权人 KALBERMATTEN LAURENT DE;

    申请/专利号FR19870001388

  • 发明设计人

    申请日1987-02-03

  • 分类号B64D17/02;B64C31/02;

  • 国家 FR

  • 入库时间 2022-08-22 06:51:00

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