首页> 外国专利> Rather than having the wing next to the missiles in the same direction as the direction of travel, the missile is mounted slightly inclined to the resistance of the air by the law of reaction.

Rather than having the wing next to the missiles in the same direction as the direction of travel, the missile is mounted slightly inclined to the resistance of the air by the law of reaction.

机译:导弹的机翼不是按照与行进方向相同的方向放在导弹旁边,而是根据反作用定律安装成略微倾斜于空气阻力。

摘要

The present invention relates to a method for reducing air resistance in flying objects such as a missile. According to the present invention, a wing of a missile is installed and mounted with a slight inclination to allow the missile to be advanced by a force received while the missile is flying. Accordingly, when the missile is advanced, the wing reduces air resistance.
机译:本发明涉及一种减小飞行物体如导弹中的空气阻力的方法。根据本发明,导弹的机翼以稍微倾斜的方式安装和安装,以允许导弹在导弹飞行时受到的力使导弹前进。因此,当导弹前进时,机翼减小了空气阻力。

著录项

  • 公开/公告号KR20190101317A

    专利类型

  • 公开/公告日2019-08-30

    原文格式PDF

  • 申请/专利权人 KIM GOUNG JOON;

    申请/专利号KR20190087169

  • 发明设计人 KIM GOUNG JOON;

    申请日2019-07-15

  • 分类号F42B10/64;B64C1/26;F42B10/14;F42B10/26;

  • 国家 KR

  • 入库时间 2022-08-21 11:49:55

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