发明名称 Subsonic Bullet
摘要 A bullet whose aerodynamics is suitable for stable subsonic flight, including a parabolic or hemispherical nose section, cylindrical midsection, and a parabolic into conical tail section. It is constructed of a copper shell filled, in the tail, with a material having a density less than or equal to 3.0 g/cm3, and in the nose with a material having a density greater than or equal to 11 g/cm3. The bullet further includes a length sufficient to fill an appropriate standard casing combined with the proper amount of smokeless powder for subsonic flight. These characteristics allow for the bullet's stable and accurate flight at speeds below 343.2 m/s.
申请公布号 US2017003107(A1) 申请公布日期 2017.01.05
申请号 US201615167251 申请日期 2016.05.27
申请人 McWilliam, SR. Charles Edmond;McWilliam Jamie George 发明人 McWilliam, SR. Charles Edmond;McWilliam Jamie George
分类号 F42B10/02;F42B12/74;F42B5/16;F42B12/78 主分类号 F42B10/02
代理机构 代理人
主权项 1. A bullet for subsonic applications, aerodynamically comprising: a parabolic or hemispherical nose section, a cylindrical midsection of diameter such that the bullet fits snugly into a casing of appropriate caliber, and a parabolic into conical tail section.
地址 Boulder City NV US