Patent US6962199B1 successfully refreshed from Google Patents.
US6962199B1
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method for removing condensables from a natural gas stream, at a wellhead, downstream of the wellhead choke
Assignee: Shell Research Ltd
•
Filing: 1999-12-29
•
Granted: 2005-11-08
•
Expires: 2019-12-29
Abstract
Abstract The present invention relates to a method for removing condensables from a natural gas stream, at a wellhead, downstream of the wellhead choke thereof. In accordance with the invention there is provided a method for removing condensables from a natural gas stream at a wellhead, the method comprising the steps of: (A) inducing the natural gas stream to flow at supersonic velocity through a conduit of a supersonic inertia separator and thereby causing the fluid to cool to a temperature that is below a temperature/pressure at which the condensables will begin to condense, forming separate droplets and/or particles; (B) separating the droplets and/or particles from the gas; and (C) collecting the gas from which the condensables have been removed, wherein the supersonic inertia separator is part of the wellhead assembly downstream of the wellhead choke. There is also provided a device for removing said condensables from said natural gas that is part of the wellhead assembly downstream of the choke, a wellhead assembly comprising said device.
Inventors
- 👤 Cornelis Antonie Tjeenk Willink
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 19:31
CPC Classifications
E; E21; E21B; E21B43/00; E21B43/34; E21B43/35; B; B01; B01D; B01D45/00; B01D45/12; B01D45/16; B01D51/00; B01D51/02; B01D51/06; B01D51/08; B01D53/00; B01D53/002; E21B34/00; E21B34/02; E21B34/025; E21B43/38; E21B43/385
Claims Analysis
Total Claims: 14
Claim 1
Independent Claim
185 words
A method for removing condensables from a gas stream, the method comprising the steps of: (A) inducing the natural gas stream to flow at supersonic velocity through a conduit of a supersonic inertia separator and thereby causing the fluid to cool to a temperature that is below a temperature/pressure at which the condensables will begin to condense, forming separate droplets and/or particles; (B) separating the droplets and/or particles from the gas; and (C) collecting the gas from which the condensables have been removed, characterized in that the supersonic inertia separator is located in the vicinity of a gas production well for the separation of condensables from the natural gas stream produced through said well and wherein in step (B) a swirling motion is induced to the supersonic stream thereby causing the condensables to flow to a radially outer section of a collecting zone in the stream, followed by the subsonic or supersonic extraction of the condensables into an outlet stream from the radially outer section of the collecting zone, and wherein the swirling motion in imparted by a wing placed in the supersonic flow region.
Claim 2
Independent Claim
185 words
A method for removing condensables from a gas stream, the method comprising the steps of: (A) inducing the natural gas stream to flow at supersonic velocity through a conduit of a supersonic inertia separator and thereby causing the fluid to cool to a temperature that is below a temperature/pressure at which the condensables will begin to condense, forming separate droplets and/or particles; (B) separating the droplets and/or particles from the gas; and (C) collecting the gas from which the condensables have been removed, characterized in that the supersonic inertia separator is located in the vicinity of a gas production well for the separation of condensables from the natural gas stream produced through said well and wherein in step (B) a swirling motion is induced to the supersonic stream thereby causing the condensables to flow to a radially outer section of a collecting zone in the stream, followed by the subsonic or supersonic extraction of the condensables into an outlet stream from the radially outer section of the collecting zone, and wherein the swirling motion in imparted by a wing placed in the supersonic flow region.
Claim 3
Dependent Claim
36 words
The method of claim 1 , further comprising the step of: creating a shock wave in the stream that is upstream of the collecting zone and downstream of the location where the swirling motion is imparted.
Claim 4
Independent Claim
22 words
The method of claim, 2 wherein the shock wave is created by inducing the stream of fluid to flow through a diffuser.
Claim 5
Dependent Claim
27 words
The method of claim 1 , further comprising adding a hydrate inhibition component to the outlet stream extracted from the radially outer section of the collecting zone.
Claim 6
Independent Claim
222 words
A device for removing condensables from natural gas according to a method comprising the steps of: inducing the gas stream to flow at supersonic velocity through a conduit of a supersonic inertia separator and thereby casuing the fluid to cool to a temperature that is below a temperature/pressure at which the condensables will begin to condense, forming separate droplets and/or particles; separating the droplets and/or particles from the gas; and collecting the gas; and collecting the gas from which the condensables have been removed, characterized in that the supersonic inertia separator is located in the vicinity of a production well for the separation of condensables from the natural gas stream produced through said well, the device comprising: an acceleration section wherein gas is accelerated to a supersonic velocity; a swirl imparting section that imparts a swirling motion to the gas; a collection zone from which a gas stream containing reduced content of condensables is removed; a radially outer section of the collecting zone with a radially outer section from which the condensables can be collected, characterized in that the device is located in the vicinity of the wellhead of a natural gas production well and is designed for the separation of condensables from a natural gas stream produced through said well; and a shock wave initiator downstream of the swirl imparting section.
Claim 7
Independent Claim
222 words
A device for removing condensables from natural gas according to a method comprising the steps of: inducing the gas stream to flow at supersonic velocity through a conduit of a supersonic inertia separator and thereby casuing the fluid to cool to a temperature that is below a temperature/pressure at which the condensables will begin to condense, forming separate droplets and/or particles; separating the droplets and/or particles from the gas; and collecting the gas; and collecting the gas from which the condensables have been removed, characterized in that the supersonic inertia separator is located in the vicinity of a production well for the separation of condensables from the natural gas stream produced through said well, the device comprising: an acceleration section wherein gas is accelerated to a supersonic velocity; a swirl imparting section that imparts a swirling motion to the gas; a collection zone from which a gas stream containing reduced content of condensables is removed; a radially outer section of the collecting zone with a radially outer section from which the condensables can be collected, characterized in that the device is located in the vicinity of the wellhead of a natural gas production well and is designed for the separation of condensables from a natural gas stream produced through said well; and a shock wave initiator downstream of the swirl imparting section.
Claim 8
Dependent Claim
25 words
The device of claim 5 wherein the shock wave initiator is a diffuser, located so that the shock wave is upstream of the collecting zone.
Claim 9
Dependent Claim
57 words
The device of claim 6 , wherein the acceleration section comprises a Laval-type inlet of the conduit, and wherein the smallest cross-sectional flow area of the diffuser is larger than the smallest cross-sectional flow area of the Laval-type inlet, and wherein the swirl imparting section that imparts a swirling motion to the stream comprises a wing device.
Claim 10
Dependent Claim
16 words
A wellhead assembly comprising a device as claimed in claim 5 , downstream of the wellhead.
Claim 11
Dependent Claim
13 words
A wellhead assembly as claimed in claim 8 , comprising a sub-sea wellhead.
Claim 12
Dependent Claim
83 words
The device of claim 5 , wherein the radially outer section of the collecting-zone debouches into an annular first outlet for collecting a condensables enriched fluid stream and a central section of the collecting zone debouches into a tubular second outlet for collecting a condensables depleted fluid stream, characterized in that the tubular second outlet is a substantial formed by a substantially straight tubular which remains substantially co-axial to the annular first outlet along at least a substantial portion of the tubular's length.
Claim 13
Dependent Claim
20 words
The device of claim 10 , wherein the annular first outlet has in downstream direction a cylindrical or diverging shape.
Claim 14
Dependent Claim
32 words
The device of claim 11 , wherein the tubular second outlet has in downstream direction a cylindrical or diverging shape and provides a co-axial vortex finder duct within the annular first outlet.
References Cited (Backward Citations)
US3155401A
Cited
US3185181A
Cited
US3725271A
Cited
US3297344A
Cited
GB1103130A
Cited
US3493050A
Cited
US3616596A
Cited
US3559373A
Cited
US3599400A
Cited
US3544170A
Cited
US3626665A
Cited
US3892070A
Cited
US3720263A
Cited
US3894851A
Cited
DE2243926A1
Cited
US3997008A
Cited
US4141701A
Cited
SU593717A1
Cited
US4102401A
Cited
US4194718A
Cited
US4148735A
Cited
GB2037610A
Cited
US4292050A
Cited
US4272499A
Cited
US4308134A
Cited
US4541845A
Cited
SU1172540A1
Cited
US4606557A
Cited
US4531584A
Cited
JPS63165849A
Cited
US4823880A
Cited
JPH0217921A
Cited
US4898235A
Cited
NL8901841A
Cited
US5333684A
Cited
US5444684A
Cited
US5261242A
Cited
EP0496128A1
Cited
WO1995009970A1
Cited
EP0711903B1
Cited
US5682759A
Cited
US5713416A
Cited
US5794697A
Cited
US6237691B1
Cited
WO1999001194A1
Cited
US6372019B1
Cited
US6280502B1
Cited
US20020194988A1
Cited
US6524368B2
Cited
EP1141520B1
Cited
US20030145724A1
Cited
WO2001021286A1
Cited
US6222083B1
Cited
DE10040015A1
Cited
US6447574B1
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 2008-11-07 | 2009-05-09 | 2009-11-08 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2012-11-07 | 2013-05-09 | 2013-11-08 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2016-11-07 | 2017-05-09 | 2017-11-08 | $7700.00 | Window Closed / Lapsed |