Progressive Cavity Based Control System
US-2015354280-A1 · Dec 10, 2015 · US
US9518462B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9518462-B2 |
| Application number | US-201314397110-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 18, 2013 |
| Priority date | Dec 18, 2013 |
| Publication date | Dec 13, 2016 |
| Grant date | Dec 13, 2016 |
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The turbine ( 100 ) can be used to transmit electrical data signals, for example, sensor data signals, across a down hole turbine using, with the data signals be communicated via a shaft ( 102 ). As a result, a signal can be induced onto the shaft ( 102 ) from a lower end of the shaft ( 102 ), for example, motor shaft, to an upper end of the shaft ( 102 ). The signal can be induced on the shaft ( 102 ) by a first induction loop ( 112 ) and can be picked up by a second induction loop ( 114 ) with the first induction loop ( 112 ) being downhole from the second induction loop ( 114 ). The second induction loop ( 114 ) can be communicatively coupled to a receiver ( 712 ) which can pass the signals passed to a transmitter ( 712 ), for example, a measurement while drilling (MWD) unit. The MWD unit can then process the signal and transmit the signal to the surface.
Opening claim text (preview).
What is claimed is: 1. A downhole turbine having a first end and a second end with the first end and the second end being opposite one another, the turbine comprising: a turbine body; a shaft positioned at about the center of the turbine body; a motor comprising a plurality of rotors, stators and bearings interposed between the shaft and the turbine body, the motor interposed between the first end and the second end of the turbine, the plurality of rotors and stators disposed radially about the circumference of the shaft arranged in alternating successive concentric rows, each row one below the other along a longitudinal length of the shaft, the successive rows of rotors rotatable within apertures formed by the successive rows of stators; and at least one non-conductor insulator assisting in electrically isolating the shaft and the turbine body from one another, wherein the non-conductor insulator is a non-conducting coating extending along an entire length interposed between the turbine body and each of the plurality of rotors, stators and bearings, or extending along an entire length interposed between the shaft and each of the plurality of rotors, stators and bearings. 2. The turbine of claim 1 further comprising: a sensor unit configured to generate sensor data; and a sensor transmitter communicatively coupled to the sensor unit and configured to transmit the generated sensor data to a first end of the motor via the shaft. 3. The turbine of claim 2 further comprising: a first inductive loop interposed between the motor and the sensor transmitter, the first inductive loop configured to induce a current on the shaft; and a second inductive loop interposed between the motor and a receiver, the second inductive loop configured to inversely induce the current from the shaft, with the current representing the generated sensor data. 4. The turbine of claim 3 wherein each of the first inductive loop and the second inductive loop is one of an inductive coil and a slip ring. 5. The turbine of claim 3 further comprising a data transmitter interposed between the second inductive loop and the second end of the turbine, the data transmitter communicatively coupled to the second inductive loop and configured to transmit the generated sensor data. 6. The turbine of claim 5 wherein the data transmitter is a measurement while drilling (MWD) transmitter. 7. The turbine of claim 2 wherein the sensor unit is located at about the motor. 8. The turbine of claim 7 wherein the generated sensor data is related to the motor. 9. The turbine of claim 2 wherein the sensor unit is interposed between the motor and the first end of the turbine with the first end of the turbine being down hole from the second end of the turbine when the turbine is inserted in a down hole. 10. The turbine of claim 9 wherein the generated sensor data represents at least one of formation parameters and tool operating parameters. 11. The turbine of claim 2 wherein the non-conducting coating is on an outer surface of the shaft. 12. The turbine of claim 2 further comprising a first non-conducting spacer covering an outer surface of the shaft at a first distal end of the motor and a second non-conducting spacer covering the outer surface of the shaft at a second distal end of the motor. 13. The turbine of claim 12 further comprising a non-conducting lubricant between contact surfaces of the plurality of rotors, stators and bearings. 14. The turbine of claim 2 wherein the non-conducting coating extending along the entire interface interposed between the turbine body and the plurality of rotors, stators and bearings comprises the non-conducting coating on bores of the rotors. 15. The turbine of claim 14 further comprising a first non-conducting spacer interposed between the turbine body and a first distal end of the motor and a second non-conducting spacer covering the turbine body at a second distal end of the motor. 16. The turbine of claim 15 further comprising a non-conducting lubricant between contact surfaces of the plurality of rotors, stators and bearings. 17. The turbine of claim 2 further comprising a conductor in a channel of the shaft, the conductor communicatively coupled to the sensor transmitter and to a data transmitter, wherein the sensor transmitter is interposed between the motor and the first end of the turbine with the first end of the turbine configured to be down hole from the second end of the turbine and the data transmitter interposed between the motor and the second end of the turbine with the second end of the turbine configured to be up hole from the motor. 18. The turbine of claim 17 wherein the conductor is one of an insulated wire and a plurality of insulated wires. 19. The turbine of claim 1 wherein the shaft is a motor shaft. 20. The turbine of claim 1 wherein the shaft is a rotating shaft.
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