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1. 发明申请

WO2008118159A2 SPIN STABILIZER PROJECTILE TRAJECTORY CONTROL 审中-公开
标题翻译：旋转稳定器项目轨迹控制（SPIN STABILIZER PROJECTILE TRAJECTORY CONTROL）
公开(公告)号：WO2008118159A2
公开(公告)日：2008-10-02
申请号：PCT/US2007/025111
申请日：2007-12-07
申请人： SIMMONDS PRECISION PRODUCTS, INC. , JENKINS, Dennis Hyatt , BYRNE, Jim , CHRISTIANA, John , FRANZ, Paul , KELLY, Tom
发明人： JENKINS, Dennis Hyatt , BYRNE, Jim , CHRISTIANA, John , FRANZ, Paul , KELLY, Tom
IPC分类号： F42B10/62 , F42B10/26
CPC分类号： F42B10/62 , F41G7/346 , F41G7/36 , F42B15/01
摘要： A Reconfigurable Nose Control System (RNCS) is designed to adjust the flight path of spin-stabilized artillery projectiles. The RNCS uses the surface of a projectile nose cone as a trim tab. The nose cone may be despun by the action of aerodynamic surfaces, to zero spin relative to earth fixed coordinates using local air flow, and deflected by a simple rotary motion of a Divert Motor about the longitudinal axis of the projectile. A forward section of the nose cone having an ogive is mounted at an angle to the longitudinal axis of the projectile, forming an axial offset of an axis of the forward section with respect to the longitudinal axis of the projectile. Another section of the nose cone includes another motor, the Roll Generator Motor, that is rotationally decoupled from the forward section and rotates the deflected forward section so that its axis may be pointed in any direction within its range of motion. Accordingly, deflection and direction of the forward section may be modulated by combined action of the motors during flight of the projectile.
摘要翻译：可重构鼻子控制系统（RNCS）旨在调整旋转稳定炮弹的飞行路径。 RNCS使用弹丸鼻锥的表面作为装饰片。鼻锥可以通过空气动力学表面的作用去除，使用局部气流相对于地球固定坐标进行零旋转，并且通过转向马达围绕射弹纵轴的简单旋转运动而偏转。具有ogive的鼻锥体的前部部分以与射弹的纵向轴线成一定角度安装，形成相对于射弹的纵向轴线的前部分的轴线的轴向偏移。鼻锥的另一部分包括另一个电动机，即辊发生器电动机，其与前部旋转地解耦并使偏转的前部旋转，使得其轴线可以在其运动范围内的任何方向上指向。因此，前向部分的偏转和方向可以通过在抛射体飞行期间电机的组合作用来调节。

2. 发明公开

EP2100090A2 SPIN STABILIZER PROJECTILE TRAJECTORY CONTROL 有权
标题翻译：飞行方向控制旋转稳压FLOOR
公开(公告)号：EP2100090A2
公开(公告)日：2009-09-16
申请号：EP07873489.4
申请日：2007-12-07
申请人： Simmonds Precision Products, Inc.
发明人： JENKINS, Dennis Hyatt , BYRNE, Jim , CHRISTIANA, John , FRANZ, Paul , KELLY, Tom
IPC分类号： F42B10/62 , F42B15/01 , F41G7/34
CPC分类号： F42B10/62 , F41G7/346 , F41G7/36 , F42B15/01
摘要： A Reconfigurable Nose Control System (RNCS) (100) is designed to adjust the flight path of spin-stabilized artillery projectiles. The RNCS (IOO) uses the surface of a projectile nose cone as a trim tab. The nose cone may be despun by the action of aerodynamic surfaces, to zero spin relative to earth fixed coordinates using local air flow, and deflected by a simple rotary motion of a Divert Motor (132) about the longitudinal axis of the projectile. A forward section (130) of the nose cone having an ogive is mounted at an angle to the longitudinal axis of the projectile, forming an axial offset of an axis of the, forward section (130) with respect to the longitudinal axis of the projectile. Another section of the nose cone includes another motor, the Roll Generator Motor(122), that is rotationally decoupled from the forward section(130) and rotates the deflected forward section (130) so that its axis may be pointed in any direction within its range of motion. Accordingly, deflection and direction of the forward section (130) may be modulated by combined action of the motors during flight of the projectile.

3. 发明授权

EP2100090B1 SPIN STABILIZER PROJECTILE TRAJECTORY CONTROL 有权
标题翻译：飞行方向控制旋转稳压FLOOR
公开(公告)号：EP2100090B1
公开(公告)日：2014-01-22
申请号：EP07873489.4
申请日：2007-12-07
申请人： Simmonds Precision Products, Inc.
发明人： JENKINS, Dennis Hyatt , BYRNE, Jim , CHRISTIANA, John , FRANZ, Paul , KELLY, Tom
IPC分类号： F42B10/62 , F42B15/01 , F41G7/34
CPC分类号： F42B10/62 , F41G7/346 , F41G7/36 , F42B15/01

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