Method and apparatus for ballistic tailoring of propellant structures and operation thereof for downhole stimulation

Patent metadata

Field	Value
Publication number	US-9447672-B2
Application number	US-201313781217-A
Country	US
Kind code	B2
Filing date	Feb 28, 2013
Priority date	Feb 28, 2013
Publication date	Sep 20, 2016
Grant date	Sep 20, 2016

Abstract

Propellant structures and stimulation tools incorporating propellant structures may comprise composite propellant structures including two or more regions of propellant having different compositions, different grain structures, or both. An axially extending initiation bore containing an initiation element may extend through a center of the propellant structure, or may be laterally offset from the center. An offset initiation bore may be employed with a composite grain structure. Methods of tailoring ballistic characteristics of propellant burn to result in desired operational pressure pulse characteristics are also disclosed.

First claim

What is claimed is:

1. A downhole stimulation tool, comprising:
a housing; and
a propellant structure within the housing and comprising:
at least one propellant grain of a formulation;
a single longitudinal bore extending through the at least one propellant grain;
at least another propellant grain of a formulation different from the formulation of the at least one propellant grain adjacent the at least one propellant grain; and
at least one initiation element for initiating the at least one propellant grain, the at least one initiation element disposed in the single longitudinal bore.

2. The downhole stimulation tool of claim 1 , wherein the at least another propellant grain comprises a sleeve surrounding the at least one propellant grain.

3. The downhole stimulation tool of claim 2 , wherein the at least another propellant grain comprises at least two other propellant grains, at least one of the at least two other propellant grains of a formulation different from the formulation of at least one of the at least one propellant grain and at least another of the at least two other propellant grains, each of the at least two other propellant grains comprising a tubular sleeve.

4. The downhole stimulation tool of claim 2 , wherein the at least one propellant grain is of one of substantially cylindrical transverse cross-section and polygonal transverse cross-section.

5. The downhole stimulation tool of claim 1 , wherein the at least one initiation element extends substantially through the longitudinal bore.

6. The downhole stimulation tool of claim 5 , wherein the single longitudinal bore is laterally offset from a center of the at least one propellant grain.

7. The downhole stimulation tool of claim 5 , wherein the single longitudinal bore comprises one of a circular transverse cross-section and a non-circular transverse cross-section.

8. The downhole stimulation tool of claim 5 , wherein the single longitudinal bore comprises a polygonal transverse cross-section.

9. The downhole stimulation tool of claim 1 , wherein the at least one initiation element comprises initiation elements proximate opposing ends of the single longitudinal bore.

10. The downhole stimulation tool of claim 9 , further comprising at least one other initiation element disposed within the single longitudinal bore.

11. The downhole stimulation tool of claim 10 , wherein the at least one other initiation element extends substantially through the single longitudinal bore.

12. The downhole stimulation tool of claim 1 , each of the at least one propellant grain and the at least another propellant grain comprising:
a polymer selected from the group consisting of polyvinyl chloride, glycidyl nitrate (GLYN), nitratomethylmethyloxetane (NMMO), glycidyl azide (GAP), diethyleneglycol triethyleneglycol nitraminodiacetic acid terpolymer (9DT-NIDA), bis(azidomethyl)-oxetane (BAMO), azidomethylmethyl-oxetane (AMMO), nitraminomethyl methyloxetane (NAMMO), bis(difluoroaminomethyl)oxetane (BFMO), difluoroaminomethylmethyloxetane (DFMO), copolymers thereof, cellulose acetate, cellulose acetate butyrate (CAB), nitrocellulose, polyamide (nylon), polyester, polyethylene, polypropylene, polystyrene, polycarbonate, a polyacrylate, a wax, a hydroxyl-terminated polybutadiene (HTPB), a hydroxyl-terminated poly-ether (HTPE), carboxyl-terminated polybutadiene (CTPB) and carboxyl-terminated polyether (CTPE), diaminoazoxy furazan (DAAF), 2,6-bis(picrylamino)-3,5-dinitropyridine (PYX), a polybutadiene acrylonitrile/acrylic acid copolymer binder (PBAN), polyvinyl chloride (PVC), ethylmethacrylate, acrylonitrile-butadiene-styrene (ABS), a fluoropolymer, polyvinyl alcohol (PVA), or combinations thereof;
a fuel selected from the group consisting of aluminum, nickel, magnesium, silicon, boron, beryllium, zirconium, hafnium, zinc, tungsten, molybdenum, copper, or titanium, or alloys mixtures or compounds thereof, such as aluminum hydride (AlH 3 ), magnesium hydride (MgH 2 ), or borane compounds (BH 3 ); and
an oxidizer selected from the group consisting of ammonium perchlorate, potassium perchlorate, ammonium nitrate, potassium nitrate, hydroxylammonium nitrate (HAN), ammonium dinitramide (ADN), hydrazinium nitroformate, cyclotetramethylene tetranitramine (HMX), cyclotrimethylene trinitramine (RDX), 2,4,6,8,10,12-hexanitro-2,4,6,8,10,12-hexaazaisowurtzitane (CL-20 or HNIW), and 4,10-dinitro-2,6,8,12-tetraoxa -4,10-diazatetracyclo-[5.5.0.0 5,9 .0 3,11 ]-dodecane (TEX).

13. A downhole stimulation tool, comprising:
a housing; and
a propellant structure within the housing and comprising:
at least one propellant grain of one of substantially cylindrical transverse cross-section and polygonal transverse cross-section having a single longitudinal bore extending therethrough laterally offset from a center of the at least one propellant grain; and
one or more additional propellant grains, each additional propellant grain configured as a sleeve and surrounding another propellant grain, at least one of the additional propellant grains of a formulation different from a formulation of the at least one substantially cylindrical propellant grain; and

at least one initiation element for initiating the at least one propellant grain within the longitudinal bore.

14. The downhole stimulation tool of claim 13 , wherein the at least one initiation element extends substantially through the longitudinal bore.

15. The downhole stimulation tool of claim 13 , wherein the longitudinal bore comprises one of a circular transverse cross-section and a non-circular transverse cross-section.

16. The downhole stimulation tool of claim 13 , wherein the longitudinal bore comprises a polygonal transverse cross-section.

17. The downhole stimulation tool of claim 13 , wherein the at least one initiation element further comprises initiation elements proximate opposing ends of the single longitudinal bore.

18. A method of operating a downhole stimulation tool, the method comprising:
initiating a substantially cylindrical propellant grain of a formulation from a single longitudinally extending location within the propellant grain to burn the propellant grain in a radially extending direction; and
initiating another propellant grain of a different formulation comprising a tubular, substantially cylindrical sleeve surrounding a substantially cylindrical exterior surface of the propellant grain along at least a portion of a boundary between the propellant grain and the another propellant grain.

19. The method of claim 18 , wherein initiating the substantially cylindrical propellant grain from a single longitudinally extending location within the propellant grain comprises initiating the substantially cylindrical propellant grain from a single longitudinally extending location offset from a center of the substantially cylindrical propellant grain.

20. The method of claim 18 , further comprising initiating the substantially cylindrical propellant grain from a bore thereof of circular transverse cross-section.

21. The method of claim 18 , further comprising initiating the substantially cylindrical propellant grain from a bore thereof of non-circular transverse cross-section.

22. The method of claim 21 , further comprising initiating the substantially cylindrical propellant grain from a bore thereof of polygonal cross-section.

23. A method of operating a downhole stimulation tool, the method comprising initiating a substantially cylindrical propellant structure fro

Assignees

• Orbital Atk Inc

Inventors

• Arrell Jr John A
• Moore Steven E

Classifications

• F42B1/00

  Explosive charges characterised by form or shape but not dependent on shape of container · CPC title

• E21B43/263 Primary

  using explosives · CPC title

• C06B45/10

  the organic component containing a resin · CPC title

• C06B33/00

  Compositions containing particulate metal, alloy, boron, silicon, selenium or tellurium with at least one oxygen supplying material which is either a metal oxide or a salt, organic or inorganic, capable of yielding a metal oxide · CPC title

• C06B45/00 Primary

  Compositions or products which are defined by structure or arrangement of component of product (explosive charges of particular form or shape F42B1/00, F42B3/00) · CPC title