IP Library › Granted Patent US 12,449,195
Granted Patent B2
US 12,449,195 · App. 18/172,790 · Granted Oct 21, 2025

Conditioning gas for a pipeline

Inventors: Jeffrey Earl (Hermosa Beach, CA); Archie Andonian (Huntington Beach, CA); Jeremy Liu (Norwalk, CA)
Assignee: Sapphire Technologies, Inc.
F25J1/0052B01D19/0052E21B34/08F02C7/12F02C9/24F25B29/003
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Quick Facts
Patent No.
US 12,449,195
App. No.
18/172,790
Granted
Oct 21, 2025
Kind
B2
Abstract

Flow from a gas well is conditioned prior to a production pipeline. A flow line is coupled to a gas well to receive the gas and coupled to a production pipeline to direct the received gas away from the production site, the flow line residing at a production site and comprising an electric power generation system. The electric power generation system has a turbine generator. The inlet nozzle and turbine wheel of the turbine generator is configured to reduce the pressure and temperature of the received gas to conditions associated with the production pipeline.

Claims (31)

1. A system for conditioning flow from a gas well prior to a production pipeline, comprising:

an inlet flow line coupled to a wellhead of the gas well to receive gas produced from the gas well;

a flow line coupled to the inlet flow line to receive the gas and coupled to the production pipeline to direct the received gas away from a production site, the flow line residing at the production site and comprising an electric power generation system,

the electric power generation system comprising:

a turbine wheel configured to receive the gas and rotate in response to expansion of the gas flowing into an inlet of the turbine wheel and out of an outlet of the turbine wheel,

a nozzle configured to direct gas into the inlet of the turbine wheel,

an electric rotor coupled to the turbine wheel and configured to rotate with the turbine wheel, and

a stationary electric stator, the electric rotor and electric stator defining an electric generator configured to generate current upon rotation of the electric rotor within the electric stator, and

the turbine wheel configured to have an isentropic efficiency of 80% or lower at the fluid conditions of the received gas when both (i) reducing a pressure of the received gas, at an inlet to the production pipeline downstream of the outlet of the turbine wheel, to at least a specified maximum pressure associated with the pipeline and (ii) reducing a temperature of the received gas, at the inlet to the production pipeline, to no lower than a specified minimum temperature associated with the pipeline.

2. The system of claim 1 , wherein the isenthalpic efficiency of the turbine wheel is selected based on the fluid conditions of the received gas, the specified maximum pressure and the specified minimum temperature.

3. The system of claim 1 , where the nozzle and the turbine wheel is configured to reduce a temperature of the received gas to no lower than a temperature at which hydrates form in the gas at an inlet of the pipeline.

4. The system of claim 1 , where the turbine wheel is configured to reduce a temperature of the received gas from a temperature higher than a specified maximum temperature associated with the pipeline to a temperature lower than the specified maximum temperature.

5. The system of claim 1 , where there is no heater between the turbine wheel and the production pipeline.

6. The system of claim 5 , where the nozzle and the turbine wheel characteristics are selected based on a specified minimum temperature of the pipeline to be above a specified minimum temperature over the operating life of the well.

7. The system of claim 1 , comprising a second flow line coupled to the inlet flow line to receive the gas and provide an alternate flow path for the gas around the first mentioned flow line, the second flow line comprising a pressure control valve, and where the first mentioned flow line and the second flow line are coupled downstream of the electric power generation system to recombine flow from the first mentioned flow line and the second flow line.

8. The system of claim 1 , comprising a hermetically sealed housing from an inlet of the electric power generation system to an outlet of the electric power generation system, the hermetically sealed housing enclosing the turbine wheel, the electric rotor, and the electric stator and hermetically sealed inline in the first mentioned flow line from the inlet to the outlet of the electric power generation system so that the received gas flows through the turbine and over the electric stator.

9. The system of claim 1 , comprising a flow control valve in the flow line upstream of the electric power generation system.

10. The system of claim 1 , where the fluid conditions of the received gas comprise at least one of pressure, temperature, or flow rate of the received gas.

11. A method of conditioning a flow from a gas well for a production pipeline, comprising:

receiving flow from the gas well at a flow line, the flow line comprising an electric power generation system residing on a production site of the well and comprising:

a turbine wheel configured to receive the gas and rotate in response to expansion of the gas flowing into an inlet of the turbine wheel and out of an outlet of the turbine wheel,

a nozzle configured to direct gas to the inlet of the turbine wheel,

an electric rotor coupled to the turbine wheel and configured to rotate with the turbine wheel, and

a stationary electric stator, the electric rotor and electric stator defining an electric generator configured to generate current upon rotation of the electric rotor within the electric stator;

flowing a portion of the flow from the gas well through the flow line and the electric power generation system, with the turbine operating at an isentropic efficiency of 80% or lower; and

(i) reducing a pressure of the gas at an inlet to the production pipeline to at least a specified maximum pressure associated with the production pipeline and (ii) reducing a temperature of the gas at the inlet to the production pipeline to no lower than a specified minimum temperature associated with the production pipeline.

12. The method of claim 11 , wherein reducing a temperature of the gas at the inlet to the production pipeline comprises reducing the temperature of the gas to at least a maximum specified temperature for the gas supplied to the production pipeline.

13. The method of claim 12 , where the maximum specified temperature is 38° C. or lower, the maximum specified temperature being higher than a freezing temperature of the gas.

14. The method of claim 11 , where the specified minimum temperature is a hydrate formation temperature of the gas at an outlet of the flow line.

15. The method of claim 11 , comprising not heating the gas between an inlet to the flow line and the inlet to the pipeline.

16. The method of claim 11 , where the electric power generation system comprises a hermetically sealed housing from an inlet of the electric power generation system to an outlet of the electric power generation system, the hermetically sealed housing enclosing the turbine wheel, the electric stator, and the electric rotor and hermetically sealed to the remainder of the flow line from the inlet to the outlet of the electric power generation system and where flowing a portion of the flow from the gas well through the flow line and the electric power generation system comprises flowing the flow around the electric stator.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 8, 2023
From: EARL, JEFFREY; ANDONIAN, ARCHIE; LIU, JEREMY
To: SAPPHIRE TECHNOLOGIES, INC.
Reel/Frame 062925/0124 →
Continuity (2)
Continuation In Part 17814597 · Jul 25, 2022
Related Publication 20240027128A1 · Jan 25, 2024
References Cited (101)
US 3508090A · Crampton et al. · 1970 [cited by applicant]
US 3667215A · Rao · 1972 [cited by examiner]
US 3808794A · Wood · 1974 [cited by applicant]
US 3895243A · Amend · 1975 [cited by examiner]
US 5689175A · Hanson et al. · 1997 [cited by applicant]
US 5924847A · Scaringe et al. · 1999 [cited by applicant]
US 6073447A · Kawakami et al. · 2000 [cited by applicant]
US 6378330B1 · Minta et al. · 2002 [cited by applicant]
US 6560988B2 · Kimble et al. · 2003 [cited by applicant]
US 6727617B2 · McMullen et al. · 2004 [cited by applicant]
US 6751985B2 · Kimble et al. · 2004 [cited by applicant]
US 7608935B2 · Scherzer · 2009 [cited by examiner]
US 7638892B2 · Myers · 2009 [cited by applicant]
US 7841306B2 · Myers et al. · 2010 [cited by applicant]
US 7861548B2 · Shibata et al. · 2011 [cited by applicant]
US 7966840B2 · Shibata et al. · 2011 [cited by applicant]
US 8146360B2 · Myers et al. · 2012 [cited by applicant]
US 8226358B2 · Matsuo et al. · 2012 [cited by applicant]
US 8384232B2 · Myers et al. · 2013 [cited by applicant]
US 8400005B2 · Huber et al. · 2013 [cited by applicant]
US 8564281B2 · Filatov · 2013 [cited by applicant]
US 8680704B1 · Rooney · 2014 [cited by examiner]
US 8739538B2 · Myers et al. · 2014 [cited by applicant]
US 8839622B2 · Myers et al. · 2014 [cited by applicant]
US 9316433B2 · Mak · 2016 [cited by applicant]
US 9568242B2 · Mak · 2017 [cited by applicant]
US 9932843B2 · Narehood et al. · 2018 [cited by applicant]
US 10280796B2 · Dall'Ara et al. · 2019 [cited by applicant]
US 10815882B2 · Marcucci et al. · 2020 [cited by applicant]
US 10895165B2 · Son · 2021 [cited by applicant]
US 11280169B1 · Bean et al. · 2022 [cited by applicant]
US 11781530B2 · Sharma · 2023 [cited by examiner]
US 20030014981A1 · Kimble et al. · 2003 [cited by applicant]
US 20030177785A1 · Kimble et al. · 2003 [cited by applicant]
US 20050217259A1 · Turchetta · 2005 [cited by applicant]
US 20070000267A1 · Shibata et al. · 2007 [cited by applicant]
US 20080246281A1 · Agrawal et al. · 2008 [cited by applicant]
US 20080252077A1 · Myers · 2008 [cited by applicant]
US 20090110485A1 · Cripps · 2009 [cited by examiner]
US 20090126377A1 · Shibata et al. · 2009 [cited by applicant]
US 20090165461A1 · Klassen et al. · 2009 [cited by applicant]
US 20090220335A1 · Matsuo et al. · 2009 [cited by applicant]
US 20100011809A1 · Mak · 2010 [cited by applicant]
US 20100150713A1 · Stankovic · 2010 [cited by examiner]
US 20100187822A1 · Bivins · 2010 [cited by examiner]
US 20100237619A1 · Pozivil et al. · 2010 [cited by applicant]
US 20100301840A1 · Filatov · 2010 [cited by applicant]
US 20100314880A1 · Cripps · 2010 [cited by examiner]
US 20110239701A1 · Kaart et al. · 2011 [cited by applicant]
US 20110283702A1 · Huber et al. · 2011 [cited by applicant]
US 20110289922A1 · Myers et al. · 2011 [cited by applicant]
US 20120013125A1 · Myers et al. · 2012 [cited by applicant]
US 20120090351A1 · Van De Lisdonk et al. · 2012 [cited by applicant]
US 20120248786A1 · Madison · 2012 [cited by applicant]
US 20130015669A1 · Favilli et al. · 2013 [cited by applicant]
US 20130039740A1 · Hawkins · 2013 [cited by applicant]
US 20130286591A1 · Myers et al. · 2013 [cited by applicant]
US 20130300120A1 · Podrog · 2013 [cited by applicant]
US 20130341929A1 · Ho · 2013 [cited by examiner]
US 20140265328A1 · Van Blerk · 2014 [cited by examiner]
US 20150204603A1 · Sheng et al. · 2015 [cited by applicant]
US 20160187058A1 · Mak · 2016 [cited by applicant]
US 20160230586A1 · King et al. · 2016 [cited by applicant]
US 20160338225A1 · Joshi et al. · 2016 [cited by applicant]
US 20160341014A1 · Flight et al. · 2016 [cited by applicant]
US 20170292350A1 · Weflen · 2017 [cited by applicant]
US 20180030855A1 · Dall'Ara et al. · 2018 [cited by applicant]
US 20180171832A1 · Kubo et al. · 2018 [cited by applicant]
US 20180195427A1 · Pandit · 2018 [cited by examiner]
US 20180306109A1 · Marcucci et al. · 2018 [cited by applicant]
US 20190055899A1 · Munevar et al. · 2019 [cited by applicant]
US 20190101061A1 · DiBenedetto · 2019 [cited by applicant]
US 20190153952A1 · Niergarth et al. · 2019 [cited by applicant]
US 20190366803A1 · Harris · 2019 [cited by applicant]
US 20200059179A1 · Pearson · 2020 [cited by applicant]
US 20200124021A1 · Reil · 2020 [cited by examiner]
US 20210156308A1 · Jones · 2021 [cited by applicant]
US 20220074653A1 · Hoffman · 2022 [cited by applicant]
US 20220154568A1 · Fink et al. · 2022 [cited by applicant]
US 20220195848A1 · Olson et al. · 2022 [cited by applicant]
US 20220268143A1 · Fink et al. · 2022 [cited by applicant]
US 20220268515A1 · Nataraj · 2022 [cited by examiner]
US 20220286020A1 · Sharma · 2022 [cited by applicant]
US 20240026803A1 · Earl et al. · 2024 [cited by applicant]
US 20240026851A1 · Earl et al. · 2024 [cited by applicant]
CN 103104812 · 2013 [cited by applicant]
CN 105401990 · 2016 [cited by applicant]
EP 2096264 · 2009 [cited by applicant]
GB 2084653 · 1982 [cited by applicant]
JP 2004303649 · 2004 [cited by applicant]
WO WO2010142698 · 2010 [cited by applicant]
WO WO2022076846 · 2022 [cited by applicant]
WO WO2023196589 · 2023 [cited by applicant]
WO WO2024072535 · 2024 [cited by applicant]
Maghon et al., “50-Hz Heavy Duty Gas Turbines—Experience and Evolution,” Siemens Power Generation (PG), upon information and belief, available no later than Jun. 8, 2021, retrieved on May 20, 2022, 10 pages. [cited by applicant]
Giardinella et al., “Improve Energy Efficiency Using Expanders,” Chemical Engineering, Apr. 1, 2021, 131(4):28-39. [cited by applicant]
International Search Report and Written Opinion in International Appln. No. PCT/US2023/028467, mailed on Apr. 25, 2024, 21 pages. [cited by applicant]
International Search Report and Written Opinion in International Appln. No. PCT/US2024/016867, mailed on Jun. 24, 2024, 13 pages. [cited by applicant]
International Search Report and Written Opinion in International Appln. No. PCT/US2024/016874, mailed on Jun. 14, 2024, 13 pages. [cited by applicant]
Ristanovic et al., “Turbo-Expander Generators for Supplemental Power Generation in LNG Liquefaction Plants,” IEEE Transactions on Industry Applications, Dec. 2020, 56(6):6094-6103. [cited by applicant]
Sidorov et al., “Numerical Simulation of the Gas Expansion Process in a Turboexpander Unit by the Finite Volume Method,” Thermal Engineering, Aug. 1, 2021, 68(8):604-611. [cited by applicant]