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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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