Method for Thermal Processing Bullets

Abstract

A method for thermal processing bullets to reduce adhesive stress, the method includes obtaining one or more bullets configured to be propelled down a gun barrel, disposing the one or more bullets within a chamber having a temperature gradient between ambient temperature and cryogenic temperature, the chamber having a plurality of temperature zones, moving the one or more bullets between the plurality of temperature zones of the chamber, and returning the one or more bullets to the ambient temperature to reduce adhesive stress between the bullets and the gun barrel.

Claims

1. A method for thermal processing bullets to reduce adhesive stress, the method comprising: obtaining one or more bullets configured to be propelled down a gun barrel; disposing the one or more bullets within a chamber having a temperature gradient between ambient temperature and cryogenic temperature, the chamber having a plurality of temperature zones; moving the one or more bullets between the plurality of temperature zones of the chamber; and returning the one or more bullets to the ambient temperature to reduce adhesive stress between the bullets and the gun barrel.

2. The method of claim 1, wherein the plurality of temperature zones includes a first temperature zone ranging from about 60 F. to about 80 F., a second temperature zone ranging from about 0 F., and a third temperature zone ranging from about 200 F. to about 500 F.

3. The method of claim 1, wherein the chamber includes a temperature reducing agent.

4. The method of claim 1, wherein the temperature reducing agent group including liquid nitrogen, gaseous nitrogen, dry ice.

5. The method of claim 1, wherein the one or more bullets are moved between the plurality of temperature zones of the chamber using a mechanical means including a ball screw mechanism, a pulley mechanism, and a conveyor mechanism.

6. The method of claim 5, wherein the one or more bullets are moved at a predetermined rate of less than 5 degrees per minute.

7. The method of claim 6, wherein internal structures of the one or more bullets are stress relieved after being moved between the plurality of temperature zones and then back to the ambient temperature.

8. The method of claim 1, wherein an adhesive stress between the bullets and the gun barrel is reduced causing an increase in sealing capacities between the bullets and the gun barrel.

9. The method of claim 8, wherein the increase in sealing capacities between the bullets and the gun barrel results in higher travel velocity, axial symmetry and concentricity of the bullet in flight.

10. The method of claim 9, wherein an external perimeter of the one or more bullets has a uniform compressive stress after being moved between the plurality of temperature zones and then back to the ambient temperature.

11. A system for thermal processing bullets to yield a refined grain structure, the system comprising: a chamber containing a plurality of cooling agents to form a plurality of temperature zones, with temperatures getting progressively cooler at each deeper temperature zone; a bullet carrier configured to hold one or more bullets to be moved through the plurality of temperature zones, each bullet comprising a bullet cartridge case detachably affixed to a bullet lead core jacketed with a gilding metal such that, upon firing the bullet, the bullet lead core with gilding metal jacket is propelled down a bore of a gun barrel; and a mechanical mechanism configured to first lower the bullet carrier holding the one or more bullets through the plurality of temperature zones and then raise the carrier holding the one or more bullets back up through the plurality of temperature zones, wherein the bullet carrier and the one or more bullets held in the bullet carrier are moved through the plurality of temperature zones at a predetermined rate and wherein at least one of the plurality of temperature zones is predetermined to cause a grain size of the bullet lead core with gilding metal jacket of the one or more bullets to become less than 50 microns.

12. The system of claim 11, wherein the plurality of temperature zones includes a first temperature zone ranging from 60 F. to 80 F., a second temperature zone intermediate of 60 F. and 200 F. and a third temperature zone ranging from 200 F. to 459.67 F.

13. The system of claim l1, wherein the chamber includes a temperature reducing agent.

14. The system of claim 13, wherein the temperature reducing agent comprises at least one of liquid nitrogen, gaseous nitrogen, and dry ice.

15. The system of claim 11, wherein the mechanical mechanism configured to lower and raise the bullet carrier holding the one or more bullets through the plurality of temperature zones comprises at least one of a ball screw mechanism, a pulley mechanism, and a conveyor mechanism.

16. The system of claim 11, wherein the predetermined rate is less than 5 F. per minute.

17. The system of claim 16, wherein internal structures of the one or more bullets are stress relieved after being moved between the plurality of temperature zones and then back to an ambient temperature.

19. The system of claim 17, wherein an external perimeter of the one or more bullets has a uniform compressive stress after being moved between the plurality of temperature zones and then back to the ambient temperature.

20. A system for thermal processing bullets to yield a refined grain structure, each bullet comprising a bullet cartridge case detachably affixed to a bullet lead core jacketed with a gilding metal such that, upon firing the bullet, the bullet lead core with gilding metal jacket is propelled down a bore of a gun barrel; the system comprising: a chamber configured to have a first temperature zone and a different second temperature zone, wherein the second temperature zone is predetermined to cause a grain size of the bullet lead core with gilding metal jacket of each of the one or more bullets to be less than 50 microns; and a bullet carrier configured to hold one or more bullets to be moved through the first and second temperature zones, wherein the bullet carrier and the one or more bullets held in the bullet carrier are moved through the first and temperature zones at a predetermined rate and wherein the second temperature zone is predetermined to cause a grain size of the bullet lead core with gilding metal jacket of the one or more bullets to become less than 50 microns.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0016] These and/or other aspects of the present general inventive concept will become apparent and more readily appreciated from the following description of the embodiments, taken in conjunction with the accompanying drawings of which:

[0017] FIG. 1 illustrates a diagrammatic view of a bullet entering a temperature gradient.

[0018] FIG. 2 illustrates a diagrammatic view of a bullet moving into a temperature gradient.

[0019] FIG. 3 illustrates a diagrammatic view of a bullet moving into and then out of a temperature gradient.

[0020] FIG. 4 illustrates a flow chart of an exemplary method of processing a bullet using a thermal processing system according to present general inventive concept.

[0021] FIG. 5 is a schematic diagram illustrating a bullet within a conventional firearm.

[0022] FIG. 6A is an enlarged detail view of item A within FIG. 5;

[0023] FIG. 6B is an enlarged detail view of item B within FIG. 5;

[0024] FIG. 7A is an enlarged detail view of item B within FIG. 5 with a conventional bullet disposed therein; and

[0025] FIG. 7B is an enlarged detail view of item B within FIG. 5 with a conventional bullet processed according to the method illustrated in FIG. 4.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0026] The present inventive concept will now be described more fully with reference to the accompanying drawings, in which exemplary embodiments of the present general inventive concept are illustrated. The inventive concept may, however, be embodied in many different forms and should not be construed as being limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the concept of the invention to those skilled in the art. Like reference numerals refer to like elements throughout.

[0027] The present general inventive concept includes methods and systems for thermally processing bullets that allows for the continuous cooling of the bullet from an ambient temperature down to, but not limited to about 300 F. and then back to ambient temperature, without stopping.

[0028] The present general inventive concept provides a method for thermal processing bullets to yield a refined grain structure, the method includes obtaining one or more bullet, disposing the one or more bullets within a chamber having a temperature gradient between ambient temperature and cryogenic temperature, the chamber having a plurality of temperature zones, moving the one or more bullets between the plurality of temperature zones of the chamber at a predetermined rate, and returning the one or more bullets to the ambient temperature.

[0029] FIG. 1 illustrates a diagrammatic view of bullet 10 entering a temperature gradient. In certain embodiments, said bullet 10 being comprised of, but not limited to cartridge case and bullet and the like made of a plurality of metal types such as but not limited to brass, cupronickel, copper alloys, and steel etc. A plurality of temperature gradients 22 being established by means of, but not limited to a chamber 20 containing cooling agents 24 such as, but not limited to liquid nitrogen, gaseous nitrogen and dry ice etc. therein. The figure showing bullet 10 entering temperature gradient T1. Said temperature gradient T1 including a first temperature zone ranging from about 60 F. to about 80 F.

[0030] FIG. 2 illustrates a diagrammatic view of a bullet 10 moving into a temperature gradient TI, passing through temperature gradient T2 and arriving at temperature T3. Other embodiments may include either more or less gradients depending on desired outcomes. Said temperature gradient T2 being comprised of a cooling agent 24 at a temperature of, but not limited to from about 100 F. to about 250 F. Temperature gradient T3 being comprised of a cooling agent 24 at a temperature of, but not limited to from about 200 F. to about 500 F. Said bullets 10 can be transported into temperature gradients individually or as multiple groups of bullets 10.

[0031] FIG. 3 illustrates a diagrammatic view of an bullet 10 moving into temperature gradients T1, T2, and T3 and then moving out said temperature gradients T1, T2, and T3. In other embodiments, bullets 10 may remain stationary and said cooling agents may be changed inside chamber 20. For example, in such an embodiment, temperature gradients first being established by introducing nitrogen gas to achieve temperature gradient T1 over a predetermined time and then introducing proportions of liquid nitrogen to achieve temperature gradient T2 over a predetermined time and then completely filling chamber 20 with liquid nitrogen to achieve temperature gradient T3 over a predetermined time. Other embodiments may incorporate other combinations of cooling agents, chambers and ammunition movements to obtain the desired aforementioned temperature gradient regimens. In embodiments wherein said bullets 10 being moved through temperature gradients inside a chamber or structure, the means of travel being performed by, but not limited to apparatuses such as ball screw mechanisms, pulley mechanisms, and conveyor mechanisms and the like. In addition, bullet 10 dwell times at the various temperature gradients T1, T2 and T3 may vary and a multitude of cooling cycles within the various said temperature gradients may also performed depending on the desired outcomes.

[0032] FIG. 4 illustrates a flow chart of an exemplary method 200 of thermal processing ammunition using a thermal processing system 100 according to present general inventive concept.

[0033] In the present embodiment, the method 200 for thermal processing bullets to yield a refined grain structure begins at step 202 by obtaining one or more bullets.

[0034] At step 204, the one or more bullets are then disposed within a chamber having a temperature gradient between ambient temperature and cryogenic temperature, wherein the chamber has a plurality of temperature zones.

[0035] At step 206, the one or more bullets are moved between the plurality of temperature zones of the chamber at a predetermined rate. In the present exemplary embodiment, the predetermined rate is negative 2 degrees per minute. However, the present general inventive concept is not limited thereto.

[0036] At step 208, the one or more bullets are then returned to the ambient temperature.

[0037] In alternative embodiments, the chamber used within the method 200 includes a plurality of temperature zones includes a first temperature zone ranging from about 60 F. to about 80 F., a second temperature zone ranging from about 0 F., and a third temperature zone ranging from about 200 F. to about 500 F. In an alternative embodiment, the third temperature zone ranges from about 100 F. and below, however, the present general inventive concept is not limited thereto.

[0038] In exemplary embodiments, the chamber may include a temperature reducing agent such as liquid nitrogen, gaseous nitrogen, dry ice. However, the present general inventive concept is not limited thereto. The one or more bullets are moved between the plurality of temperature zones of the chamber using a mechanical means including a ball screw mechanism, a pulley mechanism, and a conveyor mechanism.

[0039] In exemplary embodiments, internal structures of the one or more bullets are stress relieved after being moved between the plurality of temperature zones and then back to the ambient temperature.

[0040] In exemplary embodiments, an external perimeter of the one or more bullets has a uniform compressive stress after being moved between the plurality of temperature zones and then back to the ambient temperature.

[0041] In exemplary embodiments, a grain size of the one or more bullets is less than 50 microns. However, the present general inventive concept is not limited thereto. That is, in alternative embodiments, the grain size of the one or more bullets is less than 10 microns.

[0042] FIG. 5 is a schematic diagram illustrating a bullet 10 within a conventional firearm 20. FIG. 6A is an enlarged detail view of item A within FIG. 5 and FIG. 6B is an enlarged detail view of item B within FIG. 5. FIG. 7A is an enlarged detail view of item B within FIG. 5 with a conventional bullet disposed therein and FIG. 7B is an enlarged detail view of item B within FIG. 5 with a conventional bullet 10 processed according to the method illustrated in FIG. 4.

[0043] As illustrated in FIG. 7A, under magnification, the bullet 10 has a coarser grain structure as compared to the bullet 10 treated using the method according to the present invention. As a result, the bullet 10, shown in FIG. 7B, creates a tighter seal with an inner surface of the barrel, thereby resulting in significant increases in sealing capacities between said bullets 10 and gun barrels, ultimately resulting in higher travel velocity, axial symmetry and concentricity of the bullet in flight.

[0044] The present general inventive concept provides a system for thermal processing bullets to yield a refined grain structure, the system includes obtaining one or more bullet in a chamber, disposing the one or more bullets within the chamber having a temperature gradient between ambient temperature and cryogenic temperature, the chamber having a plurality of temperature zones, moving the one or more bullets between the plurality of temperature zones of the chamber at a predetermined rate, and returning the one or more bullets to the ambient temperature.

[0045] While the present general inventive concept has been illustrated by description of several example embodiments, and while the illustrative embodiments have been described in detail, it is not the intention of the applicant to restrict or in any way limit the scope of the general inventive concept to such descriptions and illustrations. Instead, the descriptions, drawings, and claims herein are to be regarded as illustrative in nature, and not as restrictive, and additional embodiments will readily appear to those skilled in the art upon reading the above description and drawings. Additional modifications will readily appear to those skilled in the art. Accordingly, departures may be made from such details without departing from the spirit or scope of applicant's general inventive concept.