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1. 发明授权

US08525089B2 Wing device and flight vehicle having the same 有权
标题翻译：翼装置和飞行器具有相同的
公开(公告)号：US08525089B2
公开(公告)日：2013-09-03
申请号：US13084434
申请日：2011-04-11
申请人： Sang-Hun Shin , Hae-Yong Jeong
发明人： Sang-Hun Shin , Hae-Yong Jeong
IPC分类号： F42B15/01 , B64C3/56
CPC分类号： F42B10/16
摘要： Disclosed are a wing device for a flight vehicle and a flight vehicle having the same, the wing device including a fixing shaft disposed in a lengthwise direction of a main body of the flight vehicle, a wing rotatably mounted to the fixing shaft so as to be deployed from a state of being laid on an outer circumferential surface of the main body to an erected state, and slidable along the fixing shaft, a fixing groove formed to face the wing in a sliding direction of the wing, and a spring unit configured to apply a first elastic force in an outer circumferential direction of the main body for deployment of the wing, and apply a second elastic force in a lengthwise direction of the main body for inserting the wing into the fixing groove, whereby the wing can be fixed after deployment so as to enhance stability of the flight vehicle.
摘要翻译：公开了一种用于飞行器车辆的翼装置和具有该翼装置的飞行器，所述翼装置包括沿着飞行车辆的主体的长度方向设置的固定轴，可旋转地安装到固定轴的翼，从主体的外周面放置到竖立状态的状态，沿着固定轴滑动，形成为沿机翼的滑动方向与机翼相对的固定槽，弹簧单元构成为在主体的外周方向上施加第一弹性力以展开机翼，并且在主体的长度方向上施加第二弹性力，以将翼插入固定槽中，由此翼可以固定在固定槽之后部署，以提高飞行器的稳定性。

2. 发明申请

US20110315812A1 WING DEVICE AND FLIGHT VEHICLE HAVING THE SAME 有权
标题翻译：具有相同功能的装置和飞行器
公开(公告)号：US20110315812A1
公开(公告)日：2011-12-29
申请号：US13084434
申请日：2011-04-11
申请人： Sang-Hun Shin , Hae-Yong Jeong
发明人： Sang-Hun Shin , Hae-Yong Jeong
IPC分类号： B64C3/56
CPC分类号： F42B10/16
摘要： Disclosed are a wing device for a flight vehicle and a flight vehicle having the same, the wing device including a fixing shaft disposed in a lengthwise direction of a main body of the flight vehicle, a wing rotatably mounted to the fixing shaft so as to be deployed from a state of being laid on an outer circumferential surface of the main body to an erected state, and slidable along the fixing shaft, a fixing groove formed to face the wing in a sliding direction of the wing, and a spring unit configured to apply a first elastic force in an outer circumferential direction of the main body for deployment of the wing, and apply a second elastic force in a lengthwise direction of the main body for inserting the wing into the fixing groove, whereby the wing can be fixed after deployment so as to enhance stability of the flight vehicle.
摘要翻译：公开了一种用于飞行器车辆的翼装置和具有该翼装置的飞行器，所述翼装置包括沿着飞行车辆的主体的长度方向设置的固定轴，可旋转地安装到固定轴的翼，从主体的外周面向竖立状态放置的状态，沿着固定轴可滑动地形成为沿机翼的滑动方向与机翼相对的固定槽，弹簧单元构成为在主体的外周方向上施加第一弹性力以展开机翼，并且在主体的长度方向上施加第二弹性力，以将翼插入固定槽中，由此翼可以固定在固定槽之后部署，以提高飞行器的稳定性。

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