THRUST REVERSER CASCADE FOR AN AIRCRAFT NACELLE

    公开(公告)号:US20200291893A1

    公开(公告)日:2020-09-17

    申请号:US16785117

    申请日:2020-02-07

    Abstract: A thrust reverser cascade for an aircraft nacelle includes a plurality of blades having a first and a second surface, the blades being connected to members connected to attachment flanges for attaching the thrust reverser cascade to the nacelle. At least one of the surfaces of the blades is covered with at least one layer of fibers, each layer including a plurality of fiber pieces which are pre-impregnated with resin. The fiber pieces are superimposed on one another, positioned parallel to the aerodynamic surface of the blade and oriented in different directions.

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