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1. 发明授权

US06978967B1 Space saving fin deployment system for munitions and missiles 失效
标题翻译：用于弹药和导弹的节省空间的部署系统
公开(公告)号：US06978967B1
公开(公告)日：2005-12-27
申请号：US10709180
申请日：2004-04-20
申请人： Eric Scheper , Anthony Vella , Dave Maurizi , Andrew Molina
发明人： Eric Scheper , Anthony Vella , Dave Maurizi , Andrew Molina
IPC分类号： F42B10/00 , F42B10/16
CPC分类号： F42B10/16
摘要： A fin deployment system for missiles and munitions that deploys and activates straight flat fins for roll control authority. The fin deployment system employs numerous design features, among which are the following: A wrap-around fin concept generates space-savings within a projectile body whereby the fins are arranged in a wrapped configuration around a boomtail structure. The fins may be constructed of a super-elastic material; the system eliminates mechanical means of deploying the wrapped fins, eliminating the need for springs to deploy the fins. The fin deployment achieves substantial space savings for increasing the onboard towing capacity of electronic packaging or lethality in the missiles and munitions systems, while at the same time providing a good roll control authority during flight by enabling a straight fin deployment resulting from the use of super-elastic materials.
摘要翻译：用于导弹和弹药的翅片部署系统，用于部署并激活用于滚转控制权限的直扁平翅片。散热器部署系统采用众多的设计特征，其中包括以下内容：绕线散热器概念在射弹体内产生节省空间，由此散热片以围绕吊杆结构的缠绕结构布置。翅片可以由超弹性材料构成; 该系统消除了部署包裹翅片的机械手段，消除了弹簧部署翅片的需要。翅片部署实现了大量的空间节省，以增加导弹和弹药系统中电子包装或杀伤力的板载牵引能力，同时在飞行过程中提供良好的滚转控制权限，通过使用超级弹性材料。

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