公开(公告)号：US20110114783A1

公开(公告)日：2011-05-19

申请号：US12943472

申请日：2010-11-10

Applicant: Richard ROY ,  Simon HUGUENIN

Inventor： Richard ROY ,  Simon HUGUENIN

IPC: F42B10/64

CPC classification number: F42B10/14 ,  F42B10/50

Abstract: A projectile body intended to evolve in a fluid, such body equipped with at least two radially deployable control surfaces, such control surfaces being accommodated prior to their deployment in housings made in the body, body in which the housings communicate at their intersection point, each housing being blocked by sealing means preventing any fluid from the exterior of the projectile body from passing through the housings when the control surfaces are deployed.

Abstract translation: 一种用于在液体中演化的射弹体，这种主体装备有至少两个可径向展开的控制表面，这些控制表面在它们展开在壳体内制成的壳体中被容纳，壳体在壳体中在其交点处通信， 壳体被密封装置阻挡，当控制表面展开时防止来自射弹体外部的任何流体通过壳体。

公开(公告)号：US07923671B1

公开(公告)日：2011-04-12

申请号：US11528377

申请日：2006-09-28

Applicant: Simon Huguenin ,  Richard Roy

Inventor： Simon Huguenin ,  Richard Roy

IPC: F42B10/64 ,  F42B10/14

CPC classification number: F42B10/64

Abstract: A device for driving in rotation fins of a projectile, the fins being of the deployable type integral with fin heads which are able to be oriented along an axis of spin (X, Y) substantially orthogonal to a projectile's longitudinal axis (Z), wherein the fin heads are driven in rotation by motors and substantially ring sector-shaped sliders which slide in a circular groove.

Abstract translation: 一种用于在射弹的旋转翅片中驱动的装置，所述翅片是能够沿着与射弹的纵向轴线（Z）基本正交的旋转轴线（X，Y）定向的翅片头的展开型，其中 翅片头由马达驱动旋转，并且基本上环形的扇形滑块以圆形凹槽滑动。

公开(公告)号：US20110073705A1

公开(公告)日：2011-03-31

申请号：US11528377

申请日：2006-09-28

Applicant: Simon Huguenin ,  Richard Roy

Inventor： Simon Huguenin ,  Richard Roy

IPC: F42B10/64 ,  F42B15/01

CPC classification number: F42B10/64

Abstract: A device for driving in rotation fins of a projectile, the fins being of the deployable type integral with fin heads which are able to be oriented along an axis of spin (X, Y) substantially orthogonal to a projectile's longitudinal axis (Z), wherein the fin heads are driven in rotation by motors and substantially ring sector-shaped sliders which slide in a circular groove.

Abstract translation: 一种用于在射弹的旋转翅片中驱动的装置，所述翅片是能够沿着与射弹的纵向轴线（Z）基本正交的旋转轴线（X，Y）定向的翅片头的展开型，其中 翅片头由马达驱动旋转，并且基本上环形的扇形滑块以圆形凹槽滑动。

公开(公告)号：US06477958B1

公开(公告)日：2002-11-12

申请号：US09721654

申请日：2000-11-27

Applicant: Jo{overscore (e)}l Leblond ,  Simon Huguenin ,  Nicolas Eches ,  Richard Roy

Inventor： Jo{overscore (e)}l Leblond ,  Simon Huguenin ,  Nicolas Eches ,  Richard Roy

IPC: F42B1200

CPC classification number: F42B5/073

Abstract: A device including a ring for linking a case and a projectile carrying a sealing band having a rear skirt providing low pressure sealing and a front rib lodged in a first groove in the projectile. The ring has a flared rear part connected with the case and a front part connected with the projectile by attachment means. The front part of the ring is lodged between the rear skirt of the band and the projectile and has a lip co-operating with the first groove or with a second groove in the projectile. A process for mounting the sealing band and ring to link the case and projectile includes sliding the sealing band and ring along the projectile in a single operation.

Abstract translation: 一种装置，包括用于连接壳体的环和携带具有提供低压密封的后裙部的密封带的弹丸和放置在射弹中的第一凹槽中的前肋。 环具有与壳体连接的扩口后部，并且通过附接装置与突出部连接的前部。 环的前部被放置在带的后裙部和抛射体之间，并且具有与第一凹槽配合的唇缘或与抛射体中的第二凹槽配合。 用于安装密封带和环以连接壳体和抛射体的过程包括在单个操作中沿着射弹滑动密封带和环。

公开(公告)号：US08450669B2

公开(公告)日：2013-05-28

申请号：US12943472

申请日：2010-11-10

Applicant: Richard Roy ,  Simon Huguenin

Inventor： Richard Roy ,  Simon Huguenin

IPC: F42B15/01 ,  B64C1/24 ,  B64C9/34

CPC classification number: F42B10/14 ,  F42B10/50

Abstract: A projectile body intended to evolve in a fluid, such body equipped with at least two radially deployable control surfaces, such control surfaces being accommodated prior to their deployment in housings made in the body, such that the housings communicate at their intersection point, each housing being blocked by sealing device preventing any fluid from the exterior of the projectile body from passing through the housings when the control surfaces are deployed.

Abstract translation: 一种用于在流体中演化的射弹体，这种主体装备有至少两个可径向展开的控制表面，这些控制表面在它们展开在壳体内部的壳体中之前被容纳，使得壳体在它们的交点处通信，每个壳体 被密封装置阻挡，当控制表面展开时防止来自射弹体外部的任何流体通过壳体。