
基本信息:
- 专利标题: Spin or Aerodynamically Stabilized Ammunition
- 专利标题(中):旋转或空气动力学稳定弹药
- 申请号:US13560770 申请日:2012-07-27
- 公开(公告)号:US20140077024A1 公开(公告)日:2014-03-20
- 发明人: Lubomir Mihaylov TOMOV
- 申请人: Lubomir Mihaylov TOMOV
- 优先权: BGPCT/BG2010/000017 20101012
- 主分类号: F42B10/30
- IPC分类号: F42B10/30 ; F42B33/00 ; F42B10/26
摘要:
The disclosure relates to spin-stabilized ammunition for use in grooved or smooth bore handheld firearms with calibers up to 60 mm. The projectile of the ammunition features: a body in the shape of a truncated cone at the top of a cylinder with proportions of the cone length to the cylinder length varying between from one-to-six to one-to-three depending on the expected initial speed of the projectile after the ammunition has been discharged; a central longitudinal barrel through the projectile with a proportion of the entrance diameter and exit diameter of 1.38-to-one for expected discharge speeds near sound velocity or of 1.22-to-one for expected discharge of hypersonic velocities; nozzles for the creation of a spinning motion of the ammunition around the projectile's axis, the nozzle being located between cavities for propellant charges.
摘要(中):
本公开涉及用于具有高达60mm的口径的带槽或平滑孔手持式火器的旋转稳定弹药。 弹药的弹丸特征是:圆柱体顶端的截头圆锥体的形状,锥体长度与气缸长度的比例在一到六到一到三之间变化,这取决于预期的 弹药发射后的弹丸初速度; 通过射弹的中心纵向筒体,入口直径和出口直径的比例为1.38对,用于预期排放速度接近声速或1.22对1以预期排放超音速; 喷嘴用于在弹丸的轴线周围产生弹药的旋转运动,喷嘴位于用于推进剂装料的腔之间。
公开/授权文献:
- US08844443B2 Spin or aerodynamically stabilized ammunition 公开/授权日:2014-09-30
IPC结构图谱:
F | 机械工程;照明;加热;武器;爆破 |
--F42 | 弹药;爆破 |
----F42B | 爆炸装药,例如用于爆破;烟火;弹药 |
------F42B10/00 | 效应装置,例如改进弹丸或发射物的空气动力学性质;弹丸或发射物的稳定、控制、降低射程、增加射程或减速降落用的装置 |
--------F42B10/02 | .稳定装置 |
----------F42B10/14 | ..使用发射后,例如离开身管后,伸开或展开的翼 |
------------F42B10/28 | ...由气体的作用引起的 |
--------------F42B10/30 | ....使用火箭发动机喷嘴 |