TRAILING EDGE FOR A COMPOSITE MULTISPAR INTEGRATED LIFTING SURFACE AND METHOD FOR MANUFACTURING SAID TRAILING EDGE

The invention provides a trailing edge (2) for a composite multispar integrated lifting surface (1) comprising: a first C-shape composite form (10) that comprises a web (11) and two flanges (12). The web (11) forming a portion of the rear spar (20) of a torsion box (3). The two flanges (12) extendin...

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Bibliographische Detailangaben
Hauptverfasser:	BALSA-GONZALEZ ALBERTO, LOZANO GARCIA JOSE LUIS, KOBIERECKI ROBERT
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULARARTICLES PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Beschreibung
Zusammenfassung:	The invention provides a trailing edge (2) for a composite multispar integrated lifting surface (1) comprising: a first C-shape composite form (10) that comprises a web (11) and two flanges (12). The web (11) forming a portion of the rear spar (20) of a torsion box (3). The two flanges (12) extending along the skin (21) chordwise direction.- A second C-shape composite form (15) comprising a web (16) and two flanges (17). The web (16) forming an auxiliary spar (22). The flanges (17) extending along the skin (21) chordwise direction.The first C-shape composite form (10) and the second C-shape composite form (15) forming a first auxiliary cell (30) and a second cell (31). The first auxiliary cell (30) being delimited by the first C-shape composite form (10) and the second C-shape composite form (15). The second cell (31) being an open cell delimited by the second C-shape composite form (15). 本发明提供一种用于复合多梁集成升力面(1)的后缘(2)，包括:第一C形复合形状(10)，其包括腹板(11)和两个凸缘(12)。腹板(11)形成扭力盒(3)的后梁(20)的一部分。两个凸缘(12)沿蒙皮(21)翼弦方向延伸。第二C形复合形状(15