Claims
- 1. A turbine suitable for use in down-hole drilling, and comprising a tubular casing enclosing a chamber having rotatably mounted therein a rotor comprising at least one turbine wheel blade array with an annular array of angularly distributed blades orientated with drive fluid receiving faces thereof facing generally rearwardly of a forward direction of rotation of the rotor, and a generally axially extending inner drive fluid passage generally radially inwardly of said rotor, said casing having a generally axially extending outer drive fluid passage, one of said inner and outer drive fluid passages constituting a drive fluid supply passage and being provided with at least one outlet nozzle formed and arranged for directing at least one jet of drive fluid onto said blade drive fluid receiving faces of said at least one blade array as said blades traverse said nozzle for imparting rotary drive to said rotor, the other constituting a drive fluid exhaust passage and being provided with at least one exhaust aperture for exhausting drive fluid from said at least one turbine wheel blade array.
- 2. A turbine as claimed in claim 1 wherein said turbine has an array of at least two turbine wheel blade arrays, which array extends longitudinally along the central rotational axis of the turbine, and wherein each one of said turbine wheel blade arrays has associated therewith a respective said outlet nozzle for directing at least one jet of drive fluid onto said blade drive fluid receiving faces of said turbine wheel blade array.
- 3. A turbine as claimed in claim 2 wherein neighbouring turbine wheel blade arrays are axially spaced apart from each other and provided with drive fluid return flow passages therebetween connecting the exhaust passage of an upstream turbine wheel blade array to the supply passage of a downstream turbine wheel blade array for serial interconnection of said turbine wheel blade arrays.
- 4. A turbine as claimed in claim 3 wherein each said turbine wheel blade arrays has associated therewith a plurality of angularly distributed outlet nozzles for directing a plurality of jets of drive fluid onto said blade drive fluid receiving faces of said turbine wheel blade array.
- 5. A turbine as claimed in claim 4 wherein said outlet nozzles are orientated at an angle of from 95 to 70° relative to a radially inward direction.
- 6. A turbine as claimed in claim 5 wherein said outlet nozzles are orientated tangentially relative to said turbine wheel blade array.
- 7. A turbine as claimed in claim 5 wherein said exhaust apertures are orientated at an angle of from 95 to 70° relative to radially inward direction.
- 8. A turbine as claimed in claim 7 wherein said exhaust apertures are orientated tangentially relative to said turbine wheel blade array.
- 9. A bottom hole assembly comprising at least one turbine according to claim 3, which turbine is drivingly connected to a tool.
- 10. A bottom hole assembly according to claim 9, wherein said turbine is drivingly connected to said tool via at least one reducing gearbox.
- 11. A drilling apparatus comprising a drill string, and a bottom hole assembly according to claim 9 wherein the tool comprises a drill bit.
- 12. A drilling apparatus according to claim 11, wherein said drill string comprises coiled tubing.
- 13. A turbine as claimed in claim 3 wherein each said turbine wheel blade array has at least 6 turbine blades.
- 14. A turbine as claimed in claim 3 wherein said turbine blades have an accurate channel section profile.
- 15. A turbine as claimed in claim 3 wherein each said turbine wheel blade array comprises axially spaced apart radially outwardly extending turbine blade supports for mounting of angularly distributed axially extending turbine blade members providing said turbine blades of each said turbine wheel blade array.
- 16. A turbine as claimed in claim 3 wherein is provided at least one reducing gearbox and said turbine is drivingly connected to said at least one gearbox.
- 17. A turbine as claimed in claim 16 wherein said at least one gearbox is an epicyclic gear box.
- 18. A turbine as claimed in claim 17 wherein said at least one gearbox has a reduction ratio of at least 5:1.
- 19. A turbine as claimed in claim 3 drivingly coupled with at least one further said turbine.
- 20. A turbine as claimed in claim 2 wherein said outer drive fluid passage is provided with said outlet nozzles, and said inner drive fluid passage is provided with exhaust apertures.
- 21. A turbine as claimed in claim 2 wherein said inner drive fluid passage is provided with said outlet nozzles, and said outer drive fluid passage is provided with exhaust apertures.
- 22. A turbine suitable for use in down-hole drilling, and comprising a tubular casing enclosing a chamber having rotatably mounted therein a rotor comprising at least one turbine wheel blade array with an annular array of angularly distributed blades orientated with drive fluid receiving faces thereof facing generally rearwardly of a forward direction of rotation of the rotor, and a generally axially extending drive fluid supply passage disposed in a location selected from: radially inwardly of said rotor, and within said casing, and provided with at least one outlet nozzle formed and arranged for directing at least one jet of drive fluid onto said blade drive fluid receiving faces as said blades traverse said at least one nozzle for imparting rotary drive to said rotor, and said chamber having an axial end wall provided with an exhaust aperture for exhausting drive fluid from the turbine.
- 23. A turbine suitable for use in down-hole drilling, and comprising a tubular casing enclosing a chamber having rotatably mounted therein a rotor comprising at least one turbine wheel blade array with an annular array of angularly distributed blades orientated with drive fluid receiving faces thereof facing generally rearwardly of a forward direction of rotation of the rotor, and a generally axially extending inner drive fluid passage generally radially inwardly of said rotor, said casing having generally axially extending, angularly spaced apart, drive fluid supply and exhaust passages, said drive fluid supply passage being provided with at least one outlet nozzle formed and arranged for directing at least one jet of drive fluid onto said blade drive fluid receiving faces as said blades traverse said nozzle for imparting rotary drive to said rotor, and the drive fluid exhaust passage being provided with an exhaust aperture for exhausting drive fluid from the turbine.
- 24. A turbine suitable for use in down-hole drilling, and comprising a tubular casing enclosing a chamber having rotatably mounted therein a rotor having at least two turbine wheel blade arrays each with an annular array of angularly distributed blades orientated with drive fluid receiving faces thereof facing generally rearwardly of a forward direction of rotation of the rotor, and a generally axially extending inner drive fluid passage generally radially inwardly of each said turbine wheel blade array, said casing having a respective generally axially extending outer drive fluid passage associated with each said turbine wheel blade array, one of said inner and outer drive fluid passages constituting a drive fluid supply passage and being provided with at least one outlet nozzle formed and arranged for directing at least one jet of drive fluid onto said blade drive fluid receiving faces as said blades traverse said at least one nozzle for imparting rotary drive to said rotor, the other constituting a drive fluid exhaust passage and being provided with at least one exhaust aperture for exhausting drive fluid from said turbine wheel blade arrays, neighbouring turbine wheel blade arrays being axially spaced apart from each other and provided with drive fluid return flow passages therebetween connecting the exhaust passage of an upstream turbine wheel blade array to the supply passage of a ownstream turbine wheel blade array for serial interconnection of said turbine wheel blade arrays.
Priority Claims (1)
Number |
Date |
Country |
Kind |
9816607 |
Jul 1998 |
GB |
|
CROSS REFERENCES TO RELATED APPLICATIONS
This application is a continuation in part of copending application serial number PCT/GB99/02450 titled “Drilling Turbine” which designated the United States and had an international filing date of Jul. 27, 1999. Demand was timely filed. Application serial number PCT/GB99/02450 had an international publication number of WO 00/08293, an international publication date of Feb. 17, 2000, and a priority date of Jul. 31, 1998 from GB 9816607.7.
US Referenced Citations (4)
Number |
Name |
Date |
Kind |
2371248 |
McNamara |
Mar 1945 |
A |
2750154 |
Boice |
Jun 1956 |
A |
3966369 |
Garrison |
Jun 1976 |
A |
5098258 |
Barnetche-Gonzales |
Mar 1992 |
A |
Continuation in Parts (1)
|
Number |
Date |
Country |
Parent |
PCT/GB99/02450 |
Jul 1999 |
US |
Child |
09/773698 |
|
US |