【中文】本实用新型涉及一种基于高压捕获翼外形的高速飞行器，包括机体，机体的下方设有下翼面，机体的上方设置有高压捕获翼，且下翼面的下方设置有吸气式发动机；水平投影上具有对称轴线，在对称轴线上，将高压捕获翼的最前端定义为A点，从A点开始沿着光滑曲线向两侧后掠，到达侧面的最远点B点，A点和B点之间的连线与水平线的夹角为α，30°<α<50°，高压捕获翼侧部从最远点B点沿着直线往后延伸至C点，对称轴线上的最末端点定义为D点，C点和D点之间的连线与对称轴线的夹角为β，45°<β<90°；本实用新型后掠程度相对于传统的超高声速飞行器的高压捕获翼较小，尾部燕尾形设计，尽可能多的利用高压区；将吸气式发动机结合到飞行器中，提升航速。 【EN】The utility model relates to a high-speed aircraft based on high pressure catches wing appearance, which comprises a bod, the below of organism is equipped with down the airfoil, the top of organism is provided with the high pressure and catches the wing, and the below of lower airfoil is provided with the air-breathing engine, the last axis of symmetry that has of horizontal projection, on the axis of symmetry, the foremost end that catches the wing with the high pressure is defined as A point, sweep backward to both sides along smooth curve from A point, the most distal point B point of side is reachd, the line between A point and the B point is α with the contained angle of horizontal line, 30 ° < α <50 °, high pressure catches the wing lateral part and extends backward to C point along the straight line from most distal point B point, the most distal point on the axis of symmetry is defined as D point, the line between C point and D point is β with the contained angle of axis, 45 ° < β <90 °, the utility model discloses the sweepback degree is less than traditional high pressure of super high-speed aircraft, tail swallow tail shape design, as far as possible utilization high pressure area is combined to the aircraft, promote the speed in the air.
; 李广利
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