Claims
- 1. A weapon apparatus comprising:
- a barrel having rifling and a muzzle chamber in the inside thereof, said barrel being monolithic and having a completely closed circumferential surface exterior to said chamber;
- an operating assembly means for operating said weapon; and
- a muzzle cap in the muzzle end of said chamber, said muzzle cap having a completely closed annular front surface, a center ring, a plurality of internal vanes extending between said circumferential surface and said center ring, said ring having an opening therein for the passage of the bullet, all of said vanes being angled opposite from the rifling in said barrel, and said chamber and vanes being in direct flow contact whereby the gases filling said chamber impinge directly against said plurality of vanes.
- 2. A weapon apparatus in accordance with claim 1 in which said ring has a predetermined inner diameter for the passage of the bullet from said barrel.
Parent Case Info
This is a continuation of a divisional application Ser. No 07/000,683 filed on Jan. 5, 1987, now abandoned, of parent application Ser. No. 702,635 filed on Feb. 4, 1985 from which has been issued as U.S. Pat. No. 4,703,826, dated Nov. 3, 1987.
US Referenced Citations (8)
Non-Patent Literature Citations (1)
Entry |
Gaynor, Frank, AEROSPACE DICTIONARY, 1960, "Turbine", p. 244. |
Divisions (1)
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Number |
Date |
Country |
Parent |
702635 |
Feb 1985 |
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Continuations (1)
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Number |
Date |
Country |
Parent |
683 |
Jan 1987 |
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