公开(公告)号：US3756539A

公开(公告)日：1973-09-04

申请号：US3756539D

申请日：1971-06-28

Applicant: TAMPELLA OY AB

Inventor： DONNER F ,  KRONHOLM T

IPC: F42B10/06 ,  F42B15/16 ,  B64C5/06

CPC classification number: F42B10/06

Abstract: A stabilization fin for use with projectiles which demonstrates improved aerodynamic stability as a result of unique crosssection and profile. The fin assembly is defined by multiple fins extending radially from a carrier tube. Each fin has a precisely tapered outer profile while the sides incorporate longitudinal depressions. A series of these depressions extend radially along the side of each fin and each depression originates at a point to the rear of the leading edge of the fin profile and terminates at a point ahead of the trailing edge.

Abstract translation: 与抛射体一起使用的稳定翅片，由于具有独特的横截面和轮廓，表现出改善的空气动力学稳定性。 翅片组件由从载体管径向延伸的多个翅片限定。 每个翅片具有精确的锥形外轮廓，而侧面包括纵向凹陷。 一系列这些凹陷沿着每个翅片的侧面径向延伸，并且每个凹陷起始于鳍片轮廓的前缘的后部，并且终止于后缘前方的一点。

公开(公告)号：US3765620A

公开(公告)日：1973-10-16

申请号：US3765620D

申请日：1971-07-09

Applicant: TAMPELLA OY AB

Inventor： DONNER F ,  ASIKAINEN N

IPC: F42B10/06 ,  F42B13/22

CPC classification number: F42B10/06

Abstract: A fin assembly for use with fin-stabilized projectiles such as grenades and mortars includes a tail carrier tube with a plurality of longitudinally extending fins projecting radially from the tube, the base or foot portion of each fin being pressfitted into the material of the tail carrier tube. The fins are composed of a material having substantially greater strength than the material of the tail carrier tube, and the foot portion of each fin preferably has an undulated configuration with respect to the longidutinal axis of the fin.

Abstract translation: 用于与翅片稳定的射弹（例如手榴弹和迫击炮）一起使用的翅片组件包括尾管，其具有从管径向突出的多个纵向延伸翅片，每个翼片的基部或脚部被压配合到尾架的材料中 管。 翅片由具有比尾部载体管的材料强大的强度的材料构成，并且每个翅片的脚部优选地相对于翅片的中心轴具有波浪形结构。