Laser machining of explosives

• US 6,150,630 A
• Filed: 04/17/1998
• Issued: 11/21/2000
• Est. Priority Date: 01/11/1996
• Status: Expired due to Term

• Current Assignee: Lawrence Livermore National Security LLC (Government of the United States of America)
• Original Assignee: Regents of the University of California (University of California)
• Inventors: Sefcik, Joseph A., Perry, Michael D., Banks, Paul S., Stuart, Brent C., Myers, Booth R.
• Primary Examiner(s): Ryan, Patrick
• Assistant Examiner(s): ELVE, MARIA ALEXANDRA
• Application Number:
  US09/062,078
• Time in Patent Office: 949 Days
• Field of Search: 219/121.68, 219/121.69, 219/121.6, 219/121.61, 219/121.67, 219/121.78, 219/121.79
• US Class Current: 219/121.68
• CPC Class Codes: B23K 2103/05 Stainless steel
• CPC Class Codes: B23K 2103/50 Inorganic material, e.g. metals, not provided for in B23K2103/02 – B23K2103/26
• CPC Class Codes: B23K 26/0624 using ultrashort pulses, i.e. pulses of 1ns or less
• CPC Class Codes: B23K 26/12 in a special atmosphere, e.g. in an enclosure
• CPC Class Codes: B23K 26/127 in an enclosure
• CPC Class Codes: B23K 26/18 using absorbing layers on the workpiece, e.g. for marking or protecting purposes
• CPC Class Codes: B23K 26/382 by boring
• CPC Class Codes: C06B 21/0033 Shaping the mixture
• CPC Class Codes: F42B 33/008 Cutting explosive or propulsive charges
• CPC Class Codes: G02F 1/392 Parametric amplification
• CPC Class Codes: H01S 3/0057 Temporal shaping, e.g. pulse compression, frequency chirping soliton generation and propagation G02F1/3513, H01S3/063 and H01S3/108

Abstract

The invention consists of a method for machining (cutting, drilling, sculpting) of explosives (e.g., TNT, TATB, PETN, RDX, etc.). By using pulses of a duration in the range of 5 femtoseconds to 50 picoseconds, extremely precise and rapid machining can be achieved with essentially no heat or shock affected zone. In this method, material is removed by a nonthermal mechanism. A combination of multiphoton and collisional ionization creates a critical density plasma in a time scale much shorter than electron kinetic energy is transferred to the lattice. The resulting plasma is far from thermal equilibrium. The material is in essence converted from its initial solid-state directly into a fully ionized plasma on a time scale too short for thermal equilibrium to be established with the lattice. As a result, there is negligible heat conduction beyond the region removed resulting in negligible thermal stress or shock to the material beyond a few microns from the laser machined surface. Hydrodynamic expansion of the plasma eliminates the need for any ancillary techniques to remove material and produces extremely high quality machined surfaces. There is no detonation or deflagration of the explosive in the process and the material which is removed is rendered inert.

Claims

1. A method for machining explosive materials, comprising:

producing a pulsed laser output beam comprising a plurality of laser pulses wherein each pulse of said plurality of laser pulses has a pulse repetition rate greater than 1 Hz, wherein each said pulse has a pulse duration of 50 picosecond or less; and

directing said pulsed laser output beam onto a workpiece comprising explosive material, wherein each said pulse converts approximately 0.01 to 1 micron of said explosive material of said workpiece from the solid state to the plasma state with substantially no transfer of thermal or mechanical energy into the remaining material and substantially no collateral damage thereto, wherein said explosive material is removed from said workpiece by hydrodynamic expansion of said plasma, wherein said plasma consists of inert gases and no toxic vapor, wherein said method does not induce detonation or deflagration of said explosive material.

2. A method for machining explosive material, comprising:

directing a laser beam onto a workpiece comprising explosive material, wherein said laser beam comprises a plurality of laser pulses, wherein each pulse of said plurality of laser pulses has a pulse repetition rate greater than 1 Hz, wherein each said pulse has a pulse duration within the range of 5 femtoseconds to 100 picoseconds and a focused irradiance of greater than 10¹² W/cm², wherein each pulse of said plurality of laser pulses converts approximately 0.01 to 1 micron of said explosive material of said workpiece from the solid state to the plasma state with substantially no transfer of thermal or mechanical energy into the remaining material and substantially no collateral damage thereto, wherein said material is removed from said workpiece by hydrodynamic expansion of said plasma, wherein said plasma consists of inert gases and no toxic vapor, wherein said laser beam produces no detonation or deflagration of said explosive material.

3. The method of claim 2, wherein said plurality of laser pulses removes said explosive material from said workpiece with no modification of or damage to the structure of remaining explosive material of said workpiece beyond approximately 1 micron from the kerf.

4. The method of claim 2, wherein said plurality of laser pulses removes said explosive material with no modification of or damage to the structure of remaining explosive material of said workpiece beyond a depth within a range of approximately 0.1-1 micron (depending upon the particular material).

5. The method of claim 2, wherein said pulse duration is adjusted such that the thermal penetration depth L_th during the pulse (which is equal to 2√

α

τ

(α

=k/ρ

c_p is the thermal diffusivity, k is the thermal conductivity, ρ

is the density, c_p is the heat capacity and τ

is the duration of the laser pulse)) is less than one micron.

6. The method of claim 2, wherein the electric field of each said pulse penetrates more deeply into said explosive material than the thermal wave produced in said explosive material during each said pulse.

7. The method of claim 2, wherein said plurality of laser pulses removes said explosive material from said workpiece with no modification of or damage to the structure of remaining explosive material of said workpiece beyond approximately 1 micron from the kerf, wherein external cooling of said workpiece is unnecessary.

8. The method of claim 2, wherein even though only a very small depth of material is removed per pulse, the high repetition rate enables extremely high cut rates (beyond 1 mm depth per second).

9. The method of claim 5, wherein each said pulse converts said explosive material from the solid-state to the plasma state so quickly that there is insufficient time for significant heat transfer beyond the depth removed from said workpiece, wherein as each said pulse encounters the solid surface of said explosive material for the duration of said pulse, energy is deposited into said explosive material to raise a depth thereof to a temperature far beyond its boiling point (typically to temperatures above the ionization point), wherein after said pulse is over, said depth leaves the surface of said workpiece with an expansion velocity determined by the initial temperature.