Method of making a projectile by metal injection molding
The present invention provides a method of making a metal ammunition projectile by metal injection molding comprising the steps of: providing a projectile mold to form a nose extending essentially symmetrically to a shoulder; and an essentially cylindrical bearing surface extending from the shoulder to a base; providing a metal injection molding feedstock comprising a powdered metal and a first binding agent and a second binding agent; injection molding the metal injection molding feedstock into the projectile mold to form a first projectile having a first size; debinding the first projectile to remove the first binding agent; and sintering the first projectile to remove the second binding agent and form a projectile having a second size.
1. A method of making a metal ammunition projectile by metal injection molding comprising the steps of:
providing a projectile mold to form a nose extending symmetrically to a shoulder; and an essentially cylindrical bearing surface extending from the shoulder to a base;
providing a metal injection molding feedstock comprising a powdered metal and at least a first binding agent and a second binding agent;
injection molding the metal injection molding feedstock into the projectile mold to form a first projectile having a first size;
debinding the first projectile to remove the first binding agent; and
sintering the first projectile to remove the second binding agent and form a projectile having a second size.
2. The method of claim 1 , wherein the powdered metal comprises stainless steel, brass, ceramic alloys, tungsten, tungsten carbide, carballoy, ferro-tungsten, titanium, copper, cobalt, nickel, uranium, depleted uranium, alumina oxide, zirconia and aluminum.
3. The method of claim 1 , wherein the powdered metal comprises stainless steel, brass, or ceramic alloys.
4. The method of claim 1 , wherein the powdered metal comprises 102, 174, 201, 202, 300, 302, 303, 304, 308, 309, 316, 316L, 316Ti, 321, 405, 408, 409, 410, 415, 416, 416R, 420, 430, 439, 440, 446 or 601-665 grade stainless steel.
5. The method of claim 1 , wherein the second size is 5 percent to 30 percent smaller than the first size.
6. The method of claim 1 , wherein the second size is 10 percent to 20 percent smaller than the first size.
7. The method of claim 1 , wherein the second size is 0.5, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, or 30 percent smaller than the first size.
8. The method of claim 1 , wherein the projectile comprises a cannelure formed on an outer circumferential surface of the cylindrical bearing surface intermediate the shoulder and the base.
9. The method of claim 1 , wherein the projectile comprises more than 1 cannelure formed on an outer circumferential surface of the cylindrical bearing surface intermediate the shoulder and the base.
10. The method of claim 1 , wherein more than 1 cannelure comprises 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, or 15 cannelures formed on an outer circumferential surface of the cylindrical bearing surface intermediate the shoulder and the base.
11. The method of claim 1 , wherein the metal ammunition projectile comprises stainless steel, brass, ceramic alloys, tungsten, tungsten carbide, carballoy, ferro-tungsten, titanium, copper, uranium, depleted uranium, and alumina.
12. The method of claim 1 , wherein the powdered metal comprises:
a) 2-16% Ni; 10-20% Cr; 0-5% Mo; 0-0.6% C; 0-6.0% Cu; 0-0.5% Nb+Ta; 0-4.0% Mn; 0-2.0% Si and the balance Fe;
b) 2-6% Ni; 13.5-19.5% Cr; 0-0.10% C; 1-7.0% Cu; 0.05-0.65% Nb+Ta; 0-3.0% Mn; 0-3.0% Si and the balance Fe;
c) 3-5% Ni; 15.5-17.5% Cr; 0-0.07% C; 3-5.0% Cu; 0.15-0.45% Nb+Ta; 0-1.0% Mn; 0-1.0% Si and the balance Fe;
d) 10-14% Ni; 16-18% Cr; 2-3% Mo; 0-0.03% C; 0-2% Mn; 0-1% Si and the balance Fe;
e) 12-14% Cr; 0.15-0.4% C; 0-1% Mn; 0-1% Si and the balance Fe;
f) 16-18% Cr; 0-0.05% C; 0-1% Mn; 0-1% Si and the balance Fe;
g) 3-12% aluminum, 2-8% vanadium, 0.1-0.75% iron, 0.1-0.5% oxygen, and the remainder titanium; or
h) 6% aluminum, 4% vanadium, 0.25% iron, 0.2% oxygen, and the remainder titanium.
13. The method of claim 1 , further comprising the step of applying a metal coating over the projectile.
14. The method of claim 1 , wherein the projectile is 5.56 mm, 7.62 mm, 308, 338, 3030, 3006, 50 caliber, 45 caliber, 380 caliber, 38 caliber, 9 mm, 10 mm, 12.7 mm, 14.5 mm, 14.7 mm, 20 mm, 25 mm, 30 mm, 40 mm, 57 mm, 60 mm, 75 mm, 76 mm, 81 mm, 90 mm, 100 mm, 105 mm, 106 mm, 115 mm, 120 mm, 122 mm, 125 mm, 130 mm, 152 mm, 155 mm, 165 mm, 175 mm, 203 mm, 460 mm, 8 inch, or 4.2 inch.
15. The method of claim 1 , wherein the at least a first binding agent comprises 2, 3, 4, 5, 6 or more binders.
16. The method of claim 1 , wherein the second binding agent comprises 2, 3, 4, 5, 6 or more binders.
17. The method of claim 1 , wherein the powdered metal comprises an alloy comprising copper, cobalt, and nickel.