发明名称 Aerodynamic surface with leak baffle for wing of aircraft has square-cut trailing edge with small split flap on underside with concealed hinge
摘要 The wing (1) is of a typical aerodynamic section, with a narrow square-cut trailing edge (5) at 90 degrees to the chord of the wing. The bottom surface of the trailing edge hinges down to form a split flap whose chord is only a few hundredths of the total chord (C) of the wing. The hinge (9) of the flap is concealed in a recess in the underside (3) of the wing. The top surface (2) of the wing is devoid of hinges.
申请公布号 FR2792285(A1) 申请公布日期 2000.10.20
申请号 FR19990004777 申请日期 1999.04.16
申请人 ONERA (OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES) 发明人 CORREGE MICHEL;MIGNOSI ANDRE;CARUANA DANIEL;GOBERT JEAN LOUIS
分类号 B64C3/14;B64C3/58;(IPC1-7):B64C3/28;B64C21/00 主分类号 B64C3/14
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