초록 ▼

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 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.

대표청구항 ▼

1. 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/pressu

1. 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. 2. 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.3. The method of claim, 2 wherein the shock wave is created by inducing the stream of fluid to flow through a diffuser.4. 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.5. 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. 6. 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.7. 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.8. A wellhead assembly comprising a device as claimed in claim 5, downstream of the wellhead.9. A wellhead assembly as claimed in claim 8, comprising a sub-sea wellhead.10. 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.11. The device of claim 10, wherein the annular first outlet has in downstream direction a cylindrical or diverging shape.12. 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.