Downhole tool with a propellant charge
A method of removing material from a target is described. The method comprises the steps of providing a tool, the tool having at least one propellant source; pressurising the tool to a pressure higher than the environmental pressure; igniting at least one of the propellant source(s) to form a combustion zone; and directing combustion products generated at the combustion zone along at least one tool flow path. The tool flow path(s) is selectively openable or closable, such that upon exiting the tool flow path(s) the combustion products interact with a target, the interaction causing material to be removed from the target.
1. A method of removing material from a target, the method comprising the steps of:
providing a tool, the tool having at least one propellant source;
wherein the propellant is an explosive material having a low rate of combustion that once ignited burns or otherwise decomposes to produce propellant gas and other combustion products as a stream of combustion products at high pressure;
igniting propellant of at least one of the propellant source(s) to form a combustion zone producing a stream of combustion products;
pressurising the tool with the stream of combustion products to a pressure higher than an environmental pressure, and directing at least one jet of combustion products generated at the combustion zone along at least one tool flow path;
wherein the tool flow path(s) is (are) closed by a seal until selectively opened by a threshold pressure of the stream of combustion products, that breaks the seal;
whereupon the at least one jet of combustion products exiting the tool flow path(s) interacts with a target, the interaction causing material to be removed from the target.
2. The method of claim 1 , wherein material is removed from the target by ablation, erosion, impacting, cleaning and/or transmitting heat to the target.
3. The method of claim 2 , wherein ablation, erosion, impacting and/or cleaning the target and/or transmitting heat to the target removes material from the target by severing, crushing, vibrating, skimming, applying a pressure to, hitting the target, propelling or moving and/or melting the target.
4. The method of claim 1 , wherein the at least one jet of combustion products create creates a chemical reaction in the target.
5. The method of claim 1 , wherein the step of directing at least one jet of combustion products generated at the combustion zone along at least one tool flow path, is at least partially continuous.
6. The method of claim 1 , wherein the flow path defines a flow path profile, the flow path profile being configured to create a change in a combustion product parameter.
7. The method of claim 6 , wherein the flow path is configured to change the pressure, temperature and/or speed of the at least one jet of combustion products.
8. The method of claim 1 , wherein there are multiple flow paths.
9. The method of claim 8 , wherein, where there are multiple flow paths, at least some of the flow paths converge into a single flow path.
10. The method of claim 1 , wherein, where there is a single flow path, the single flow path diverges into multiple flow paths.
11. The method of claim 1 , wherein the flow path(s) has a variable cross-section.
12. The method of claim 1 , wherein the flow path(s) includes one or more restrictions.
13. The method of claim 12 , wherein the restriction(s) are movable with respect to the flow path(s) to create pulses in the at least one jet of combustion products.
14. The method of claim 12 , wherein the restriction(s) define a reduced flow path(s) cross section.
15. The method of claim 12 , wherein the restriction(s) define a varying flow path cross section.
16. The method of claim 1 , wherein the method further comprises the step of providing at least one additive.
17. The method of claim 16 , wherein the additive(s) is a heat transfer material.
18. The method of claim 16 , wherein the method comprises the step of introducing the additive(s) to the generated at least one jet of combustion products.
19. The method of claim 18 , wherein the additive(s) are introduced to the at least one jet of combustion products through a feed.
20. The method of claim 1 , wherein the propellant source generates the at least one jet of combustion products at high temperature.
21. The method of claim 1 , wherein the generated at least one jet of combustion products exits the flow path in a preferred direction.
22. The method of claim 1 , wherein the method further comprises the step of moving the tool with respect to the target.
23. The method of claim 1 , wherein the method comprises the step of varying the direction of the at least one jet of combustion products exiting the flow path with respect to the tool.
24. The method of claim 23 , wherein the angle and/or direction of the at least one jet of combustion products exiting the flow path is controlled by computer numerical control methods.
25. The method of claim 1 , wherein the method comprises the step of directing the at least one jet of combustion products generated at the combustion zone in a radially outwards direction.
26. The method of claim 1 , wherein the method comprises the step of deflecting the at least one jet of combustion products prior to exiting the flow path.
27. The method of claim 26 , wherein the at least one jet of combustion products is deflected by a deflector.
28. The method of claim 27 , wherein the deflector is sacrificial.
29. The method of claim 28 , wherein the deflector comprises an additive.
30. The method of claim 1 , wherein the method comprises forming a plurality of jets of combustion products.
31. The method of claim 1 , wherein the method comprises merging one or more jets of combustion products to form a single jet of combustion products.
32. The method of claim 1 , wherein the method comprises creating pulses in the generated at least one jet of combustion products.
33. The method of claim 1 , wherein the method comprises creating a sequence of jets of combustion products.
34. The method of claim 33 , wherein the sequence of jets of combustion products are pulses.
35. The method of claim 1 , wherein the method comprises the step of cooling the target.
36. The method of claim 1 , wherein the method comprises subjecting the target to thermal stress and/or thermal shock imparted partially with the generated at least one jet of combustion products.
37. The method of claim 1 , further comprising a step of monitoring the removal of material from the target.
38. The method of claim 37 , wherein the step of monitoring the removal of material from the target is performed by a camera.
39. The method of claim 1 , wherein the at least one jet of combustion products interacts directly with the target.
40. The method of claim 1 , wherein the at least one jet of combustion products interacts indirectly with the target.
41. The method of claim 1 , wherein the at least one jet of combustion products is adapted to propel an object or material into, adjacent to or through the target.
42. The method of claim 1 wherein the tool flow path(s) are selectively closeable.
43. A tool for removing material from a target, the tool comprising:
at least one propellant source;
at least one mechanism for igniting propellant of the propellant source(s),
wherein the propellant is an explosive material having a low rate of combustion that once ignited burns or otherwise decomposes to produce propellant gas and other combustion products as a stream of combustion products at high pressure;
wherein, upon ignition, propellant of at least one of the propellant source(s) combusts to form a combustion zone producing the stream of combustion products; and the tool further comprises;
at least one tool flow path, the tool flow path(s) being closed by a seal and selectively openable by a threshold pressure of the stream of combustion products, that breaks the seal;
wherein the stream of combustion products pressurises the tool to a pressure higher than the environmental pressure, opens the tool flow path(s) and directs at least one jet of combustion products, in use, to flow out of the tool along the tool flow path(s) towards a target from which material is to be removed.
44. The tool of claim 43 wherein the tool flow path(s) are selectively closeable.
45. A method of initiating a change in a target, the method comprising the steps of:
providing at least one propellant source;
igniting propellant of at least one of the propellant source(s) to form a combustion zone;
wherein the propellant is an explosive material having a low rate of combustion that once ignited burns or otherwise decomposes to produce propellant gas and other combustion products as a stream of combustion products at high pressure; and
directing at least one jet of combustion products generated at the combustion zone along at least one flow path, such that upon exiting the flow path(s) the at least one jet of combustion products interacts with a target, the interaction causing a change in the target.
46. The method of claim 45 , wherein the change in the target is a change in temperature, structure, position, composition, phase, physical properties and/or condition of the target or any other characteristic of the target.
47. The method of claim 45 , wherein the change in the target is to at least one of ablate, erode, impact, clean and transmit heat to the target.
48. The tool of claim 45 wherein the tool flow path(s) are selectively closeable.