| 摘要 |
The invention relates to guiding carriers (6, 7) for the lining (1) of jet engines for aeroplanes, comprising a base body (8, 9) formed by a hollow profiled element (14, 15) with an essentially closed cross-section, said base body comprising at least one sliding device (10, 11) for the mobile mounting of a thrust reverser (2), a connection for an inner lining (5) of the jet engine, and fittings (12, 13) for detachable and pivotable fixing to a carrier structure for connection to another guiding carrier (7). In order to create such a guiding carrier (6, 7) which is especially light and therefore sufficiently rigid, the hollow profiled element (14, 15) is produced from a carbon fibre reinforced plastic material according to the resin infusion method. The connection to the inner lining (5) of the jet engine is ensured by two flanges (18, 19) arranged on the hollow profiled element (14, 15) of the base body (8, 9) of the guiding carrier (6, 7). |
