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SUPERSONIC AIRPLANE AND METHOD FOR REDUCING SONIC BOOMS

机译:超音速飞机及其减震方法

摘要

[Problem] To provide a supersonic airplane and a method for reducing sonic booms, by which sonic booms due to engine exhaust can be reduced. [Solution] This supersonic airplane has: a pair of engine nacelles 12R, 12L installed in a fuselage 11 of a plane body 10; a pair of fins 13R, 13L serving as blocking plates that prevent engine exhaust 15 discharged from jet engines (not illustrated) accommodated in the engine nacelles 12R, 12L from being suctioned into a lower portion of the plane body 10; and a pair of horizontal stabilizers 14R, 14L disposed behind the engine nacelles 12R, 12L. The fins 13R, 13L are disposed in the horizontal stabilizers 14R, 14L, respectively, with the engine exhaust 15 therebetween.
机译:[问题]提供一种超音速飞机和减少声波臂的方法,通过该方法可以减少由于发动机排气引起的声波臂。 [解决方案]该超音速飞机具有:一对安装在飞机主体10的机身11中的发动机机舱12R,12L;以及一对发动机舱12R,12L。一对翅片13R,13L用作阻挡板,以防止从容纳在发动机机舱12R,12L中的喷气发动机(未示出)排出的发动机排气15被吸入飞机主体10的下部;一对水平稳定器14R,14L设置在发动机机舱12R,12L的后面。散热片13R,13L分别布置在水平稳定器14R,14L中,并且发动机排气口15位于其间。

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