IP Library Granted Patent US 10,041,321
Granted Patent B2
US 10,041,321 · App. 15/527,970 · Granted Aug 7, 2018

Downhole tool with a propellant charge

Inventors: Jamie Oag (Aberdeenshire, GB); Rae Younger (Aberdeenshire, GB); Sidney Dantuma Johnston (Aberdeenshire, GB)
Assignee: SPEX CORPORATE HOLDINGS LIMITED
E21B29/02B23K7/006E21B33/12E21B33/134E21B43/116E21B33/13
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Quick Facts
Patent No.
US 10,041,321
App. No.
15/527,970
Granted
Aug 7, 2018
Kind
B2
Abstract

A tool for manipulating a tubular, such as casing or production tubing, in a downhole environment, is described. The tool comprises a housing defining a chamber, the chamber having at least one outlet, a propellant source located within the chamber and an ignition mechanism for igniting the propellant source. Upon ignition of the propellant source, the propellant deflagrates, creating at least one stream of combustion products, the chamber directing the stream of combustion products through the/each outlet, towards the tubular to be manipulated, the/each stream of combustion products combining with at least one modifying agent to manipulate the tubular.

Claims (24)

1. A tool for manipulating a tubular in a downhole environment, the tool comprising:

a housing defining a chamber, the chamber having at least one outlet;

a propellant source located within the chamber;

an ignition mechanism for igniting the propellant source; and

at least one modifying agent provided in or adjacent the tool or generated by the tool;

wherein upon ignition of the propellant source, the propellant source is adapted to deflagrate, creating at least one stream of combustion products, the chamber directing the stream of combustion products through the/each outlet, towards the tubular to be manipulated, the/each stream of combustion products combining with at least one modifying agent to manipulate the tubular.

2. The tool of claim 1 , wherein in use, the at least one modifying agent cracks, displaces, erodes, ablates, abrades or removes at least a portion of the tubular to be manipulated.

3. The tool of claim 1 , wherein the propellant source comprises a plurality of propellants.

4. The tool of claim 1 , wherein the propellant source is formed of the combination of two or more materials within the tool.

5. The tool of claim 1 , wherein the propellant source is arranged to create an intermittent stream of combustion products.

6. The tool of claim 1 , wherein at least one of the at least one modifying agent is formed by the combustion of the propellant source.

7. The tool of claim 1 , wherein at least one of the at least one modifying agent is formed separately from the combustion of the propellant source.

8. The tool of claim 1 , wherein at least one of the at least one modifying agent is present prior to ignition of the propellant source.

9. The tool of claim 1 , wherein at least one of the at least one modifying agent is present within the propellant source.

10. The tool of any claim 1 , wherein at least one of the at least one modifying agent is aluminum oxide.

11. The tool of claim 1 , wherein at least one of the at least one modifying agent reacts with the environment and/or the tubular to be modified.

12. The tool of claim 1 , wherein at least one of the at least one modifying agent is introduced into the stream of combustion products.

13. The tool of claim 1 , wherein at least one of the at least one modifying agent is drawn into the stream of combustion products by a venturi or similar geometric profile.

14. The tool of claim 1 , wherein at least one of the at least one modifying agent is mechanically or forcibly introduced into the propellant gas and/or stream of combustion products.

15. The tool of claim 1 , wherein at least one of the at least one modifying agent is applied to the surface of the tubular to be manipulated.

16. The tool of claim 1 , wherein at least one of the at least one modifying agent is a flux.

17. A method of manipulating a tubular in a downhole environment, the method comprising:

positioning a tool having a housing defining a chamber, the chamber having at least one outlet; a propellant source located within the chamber; and an ignition mechanism for igniting the propellant source adjacent a tubular to be manipulated,

igniting the propellant source such that at least one stream of combustion products is generated, the chamber directing the/each stream of combustion products through the/each outlet, the outlet directing the/each stream of combustion products towards the tubular to be manipulated, the/each stream of combustion products including a modifying agent to modify the tubular to be manipulated.

Assignments (2)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 20, 2017
From: SPEX ENGINEERING (UK) LIMITED
To: SPEX CORPORATE HOLDINGS LIMITED
Reel/Frame 044449/0587 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 4, 2017
From: OAG, JAMIE; YOUNGER, RAE; JOHNSTON, SIDNEY DANTUMA
To: SPEX ENGINEERING (UK) LIMITED
Reel/Frame 043200/0267 →
Priority Claims (2)
GB 1420491.1 · Nov 18, 2014 · national
GB 1506265.6 · Apr 13, 2015 · national
Continuity (1)
Related Publication 20180163496A1 · Jun 14, 2018
Cited By (4)
US 12,241,326 US 12,312,922 US 12,320,238 US 12,378,833