Patent US633554A successfully refreshed from Google Patents.
Patent US4453604A successfully refreshed from Google Patents.
US4453604A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Turbodrills
Assignee: Individual
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Filing: 1979-07-27
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Granted: 1984-06-12
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Expires: 1999-07-27
Abstract
Abstract The turbodrill disclosed consists of a shell (1) attached to the drilling string and provided with an opening (3) in the side surface, a multistage turbine and a hollow shaft (6) supported in the shell (1) by radial bearings (10) and a thrust bearing (11). The bore (7) of the shaft (6) is hydraulically linked up with the drilling string (2) and with a space (15) provided above the nozzles of the bit (13). Seals (16, 17) keeping the drilling fluid out of the space (12) contained where the thrust bearings (11) are provided in an annular space between the shell (1) and the shaft (6). The present invention can be used to advantage in turbodrills employed for the drilling of deep oil and natural gas wells under difficult geological conditions.
Inventors
- 👤 Jury R. Ioanesian
- 👤 Valery V. Popko
- 👤 Radik S. Subkhangulov
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 23:20
CPC Classifications
E; E21; E21B; E21B4/00; E21B4/003; E21B4/02; F; F03; F03B; F03B13/00; F03B13/02; Y; Y10; Y10S; Y10S277/00; Y10S277/928; Y10S415/00; Y10S415/903
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
212 words
A turbodrill comprising a shell with an opening in the side surface thereof enabling the drilling fluid to pass, a multistage turbine contained in said shell and provided with an inlet chamber and an outlet chamber, said inlet chamber being hydraulically linked up with a drill string, said outlet chamber communicating with an annular space between said shell and the wall of the well by way of said opening in said shell; a hollow shaft supported in said shell by radial bearings and a thrust bearing, the bore of said shaft being hydraulically linked up with the drill string and with a space provided above bit nozzles characterized in that seals (16, 17) are provided in the annular space between said shell (1) and said shaft (6) to seal off the space (12) of the thrust bearing (11) from the drill fluid, every one of said seals being made up of at least three members (28, 29, 30) fitted along the axis of said shaft (6) and successively contacting each other to form a closed cavity (31) communicating with said thrust bearing space (12); means (32) of controlling the pressure of lubricant contained in said thrust bearing space, said means (32) being fitted to at least one of said contacting members (29).
Claim 2
Dependent Claim
212 words
A turbodrill comprising a shell with an opening in the side surface thereof enabling the drilling fluid to pass, a multistage turbine contained in said shell and provided with an inlet chamber and an outlet chamber, said inlet chamber being hydraulically linked up with a drill string, said outlet chamber communicating with an annular space between said shell and the wall of the well by way of said opening in said shell; a hollow shaft supported in said shell by radial bearings and a thrust bearing, the bore of said shaft being hydraulically linked up with the drill string and with a space provided above bit nozzles characterized in that seals (16, 17) are provided in the annular space between said shell (1) and said shaft (6) to seal off the space (12) of the thrust bearing (11) from the drill fluid, every one of said seals being made up of at least three members (28, 29, 30) fitted along the axis of said shaft (6) and successively contacting each other to form a closed cavity (31) communicating with said thrust bearing space (12); means (32) of controlling the pressure of lubricant contained in said thrust bearing space, said means (32) being fitted to at least one of said contacting members (29).
Claim 3
Dependent Claim
200 words
A turbodrill comprising a shell with an opening in the side surface thereof for the passage of the drilling fluid, a multistage turbine contained in said shell and provided with an inlet chamber hydraulically communicating with the drill string and an outlet chamber communicating with the external space by way of said opening in said shell, a hollow shaft supported in said shell by radial bearings and a thrust bearing, the bore of said shaft hydraulically communicating with the drill string and with a space provided above bit nozzles, seals provided in the annular space between said shell and said shaft to seal off the space of the thrust bearing from the drilling fluid, each of said seals incorporating members contacting each other and including at least one means of controlling the pressure of lubricant contained in said thrust bearing space, characterized in that each said seal is made up of at least three members mounted along said shaft and successively contacting each other, which members form a closed cavity communicating with said thrust bearing space by way of said means of controlling pressure in the latter space, said means being placed in at least one of said contacting members.
Claim 4
Dependent Claim
200 words
A turbodrill comprising a shell with an opening in the side surface thereof for the passage of the drilling fluid, a multistage turbine contained in said shell and provided with an inlet chamber hydraulically communicating with the drill string and an outlet chamber communicating with the external space by way of said opening in said shell, a hollow shaft supported in said shell by radial bearings and a thrust bearing, the bore of said shaft hydraulically communicating with the drill string and with a space provided above bit nozzles, seals provided in the annular space between said shell and said shaft to seal off the space of the thrust bearing from the drilling fluid, each of said seals incorporating members contacting each other and including at least one means of controlling the pressure of lubricant contained in said thrust bearing space, characterized in that each said seal is made up of at least three members mounted along said shaft and successively contacting each other, which members form a closed cavity communicating with said thrust bearing space by way of said means of controlling pressure in the latter space, said means being placed in at least one of said contacting members.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-06-12 | 1987-12-12 | 1988-06-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-06-12 | 1991-12-12 | 1992-06-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-06-12 | 1995-12-12 | 1996-06-12 | $7700.00 | Window Closed / Lapsed |