首页> 外国专利> Aircraft with twin rudders on wings with trailing-edge flaps - has ventilating flaps forward of others in wing section inboard of rudders

Aircraft with twin rudders on wings with trailing-edge flaps - has ventilating flaps forward of others in wing section inboard of rudders

机译:带尾缘襟翼的机翼上装有双舵的飞机-在舵翼内侧的机翼部分具有通风襟翼

摘要

The aircraft of canard configuration with twin rudders has these on either side of the fuselage, mounted on the wings which also have trailing-edge flaps. In the wing (6) portions between the fuselage (3) and rudder fins (1,2) there are ventilating flaps (11,12) immediately forward of the trailing-edge flaps (13,14), hinged along their forward edge. When raised, each flap opens a duct through the wing discharging ahead of the rudder hinge-line. Both sets of flaps extend full-width between the fuselage and rudder fin, remaining in contact with the fuselage at all angles. This portion of trailing-edge flap operates also as a trimming flap.
机译:带有双舵的鸭式配置飞机在机身的两侧都安装了这些,安装在机翼上,机翼也有后缘襟翼。在机身(3)和舵鳍(1,2)之间的机翼(6)部分中,紧接在后缘襟翼(13,14)前方的通风襟翼(11,12)沿其前缘铰接。升起时,每个襟翼打开一条通过机翼的导管,并在舵铰链线之前排放。两组襟翼均在机身和舵鳍之间延伸全宽,并保持与机身的所有角度接触。后缘襟翼的这一部分也用作修剪襟翼。

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