Embodiments described generally relate to offshore single point mooring marine terminals. More particularly, such embodiments relate to offshore mooring buoys configured to transfer fluids to and from a vessel moored thereto and systems and processes for using same.
In the drilling, production, and transportation of offshore liquid hydrocarbons, mooring buoys have been used to connect a floating vessel to loading/unloading capabilities away from shore. A single point mooring (SPM) marine terminal includes a loading/unloading buoy anchored offshore that serves as a mooring link between geostatic subsea pipeline end manifold (PLEM) connections and the floating vessel. The buoy includes a material transfer system that transports liquid hydrocarbons between the pipeline end manifold and the vessel, for example from the pipeline end manifold into a vessel storage tank. The buoy connects to the pipeline end manifold using one or more submarine conduits, riser lines, or hoses. The pipeline end manifolds connect to pipelines that carry liquid hydrocarbons to and from near-shore or on-shore facilities or locations for distribution and/or processing.
During loading operations, a vessel is moored to a conventional SPM marine terminal. One or more floating transport lines or hoses are placed in fluid communication with the vessel storage tank and the SPM marine terminal. Liquid hydrocarbons are then conveyed from the pipeline, through the submarine lines, the buoy, the floating transport lines, and into the vessel storage tank(s). Conventional liquid hydrocarbon carrying vessel storage tanks are designed to safely operate within specified pressure ranges. As the liquid hydrocarbon is introduced into the vessel storage tank, fluid, e.g., a gas, within the tank is displaced such that a pressure within the vessel storage tank can be maintained within the specified ranges. Current processes for controlling the pressure within the tank include venting, displacing, or otherwise discharging the fluid directly to the atmosphere.
There is a need, therefore, for improved systems and processes for capturing fluid displaced from vessel storage tanks during loading operations that avoid or substantially reduce the fluid from being introduced into the atmosphere.
Systems and processes for recovering a condensate from a conduit are provided. In some embodiments, a system for recovering a condensate from a conduit can include a buoy, a first surface conduit, a first gas transfer conduit, a second gas transfer conduit, a first liquid transfer conduit, a second liquid transfer conduit, a second surface conduit, and a condensation conduit. The buoy can be configured to float in a body of water. The buoy can include a fluid swivel assembly coupled thereto. The fluid swivel assembly can include a first swivel section rotatably coupled to a second swivel section that can define a first fluid flow path and a second fluid flow path therethrough that can be segregated from one another. The first surface conduit can be configured to float in the body of water and to be in fluid communication with the first gas transfer conduit. The first gas transfer conduit can be disposed on the buoy and can be in fluid communication with the first fluid flow path defined by the first swivel section. The second gas transfer conduit can be in fluid communication with the first fluid flow path defined by the second swivel section. The first liquid transfer conduit can be configured to be in fluid communication with a liquid pipeline located at a subsea location and the second fluid flow path defined by the second swivel section. The second liquid transfer conduit can be disposed on the buoy and can be in fluid communication with the second fluid flow path defined by the first swivel section. The second surface conduit can be configured to float in the body of water and to be in fluid communication with the second liquid transfer conduit. The first surface conduit, the first gas transfer conduit, the first fluid flow path defined by the first swivel section and the second swivel section, and the second gas transfer conduit can be configured to transfer a gas discharged from a vessel storage tank to a gas pipeline located at a subsea location. The first surface conduit can include a low point when floating in the body of water or the first gas transfer conduit can include a low point between the first fluid flow path defined by the first swivel section and the first surface conduit. The first gas transfer conduit can include a high point between the low point of the first surface conduit or the low point of the first gas transfer conduit and the first fluid flow path defined by the first swivel section. In some embodiments, when the first surface conduit has the low point, the condensation conduit can be configured to transfer at least a portion of any condensate that accumulates at the low point to a location downstream of the high point while remaining disposed within the internal volume of the first surface conduit and the first gas transfer conduit. In other embodiments, when the first gas transfer conduit has the low point, the condensation conduit can be configured to transfer at least a portion of any condensate that accumulates at the low point to a location downstream of the high point.
In some embodiments, a system for recovering a condensate from a conduit can include a buoy, a first surface conduit, a first gas transfer conduit, a second gas transfer conduit, a first liquid transfer conduit, and a second surface conduit. The buoy can be configured to float in a body of water. The buoy can include a fluid swivel assembly coupled thereto. The fluid swivel assembly can include a first swivel section rotatably coupled to a second swivel section that define a first fluid flow path and a second fluid flow path therethrough that can be segregated from one another. The first surface conduit can be configured to float in the body of water and to be in fluid communication with the first gas transfer conduit. The first gas transfer conduit can be disposed on the buoy and can be in fluid communication with the first fluid flow path defined by the first swivel section. The second gas transfer conduit can be in fluid communication with the first fluid flow path defined by the second swivel section. The first liquid transfer conduit can be configured to be in fluid communication with a liquid pipeline located at a subsea location and the second fluid flow path defined by the second swivel section. The second liquid transfer conduit can be disposed on the buoy. The second liquid transfer conduit can be in fluid communication with the second fluid flow path defined by the first swivel section. The second surface conduit can be configured to float in the body of water and to be in fluid communication with the second liquid transfer conduit. The first surface conduit, the first gas transfer conduit, the first fluid flow path defined by the first swivel section and the second swivel section, and the second gas transfer conduit can be configured to transfer a gas discharged from a vessel storage tank to a gas pipeline located at a subsea location. In some embodiments, the first surface conduit can include a low point when floating in the body of water and the system can be configured to heat the first surface conduit at the low point or proximate the low point to a temperature that can be sufficient to prevent a condensate from collecting within the first surface conduit at the low point or can be sufficient to evaporate at least a portion of any condensate that collects within the first surface conduit at the low point. In other embodiments, the first gas transfer conduit can include a low point and the system can be configured to heat the first gas conduit at the low point to a temperature that can be sufficient to prevent a condensate from collecting within the first gas conduit at the low point or can be sufficient to evaporate at least a portion of any condensate that collects within the first gas conduit at the low point.
In other embodiments, a system for recovering a condensate from a conduit, can include a buoy, a first surface conduit, a first gas transfer conduit, a second gas transfer conduit, a first liquid transfer conduit, a second liquid transfer conduit, and a second surface conduit. The buoy can be configured to float in a body of water. The buoy can include a fluid swivel assembly coupled thereto. The fluid swivel assembly can include a first swivel section rotatably coupled to a second swivel section that can define a first fluid flow path and a second fluid flow path therethrough that can be segregated from one another. The first surface conduit can be configured to float in the body of water and to be in fluid communication with the first gas transfer conduit. The first gas transfer conduit can be disposed on the buoy and can be in fluid communication with the first fluid flow path defined by the first swivel section. The second gas transfer conduit can be in fluid communication with the first fluid flow path defined by the second swivel section. The first liquid transfer conduit can be configured to be in fluid communication with a liquid pipeline located at a subsea location and the second fluid flow path defined by the second swivel section. The second liquid transfer conduit can be disposed on the buoy and can be in fluid communication with the second fluid flow path defined by the first swivel section. The second surface conduit can be configured to float in the body of water and to be in fluid communication with the second liquid transfer conduit. The first surface conduit, the first gas transfer conduit, the first fluid flow path defined by the first swivel section and the second swivel section, and the second gas transfer conduit can be configured to transfer a gas discharged from a vessel storage tank to a gas pipeline located at a subsea location. The first surface conduit can include a low point when floating in the body of water or the first gas transfer conduit can include a low point between the first fluid flow path defined by the first swivel section and the first surface conduit. The first gas transfer conduit can include a high point between the low point of the first surface conduit or the low point of the first gas transfer conduit and the first fluid flow path defined by the first swivel section. In some embodiments, the system can further include a condensation conduit, where, when the first surface conduit has the low point, the condensation conduit can be configured to transfer at least a portion of any condensate that accumulates at the low point to a location downstream of the high point while remaining disposed within the internal volume of the first surface conduit and the first gas transfer conduit. In other embodiments, the system can further include a condensation conduit, where, when the first gas transfer conduit has the low point, the condensation conduit can be configured to transfer at least a portion of any condensate that accumulates at the low point to a location downstream of the high point. In other embodiments, the system can be configured to heat the first surface conduit or the first gas conduit at the low point to a temperature that can be sufficient to prevent a condensate from collecting within the first surface conduit or the first gas conduit at the low point or can be sufficient to evaporate at least a portion of any condensate that collects within the first surface conduit or the first gas conduit at the low point.
The various aspects and advantages of the preferred embodiment of the present invention will become apparent to those skilled in the art upon an understanding of the following detailed description of the invention, read in light of the accompanying drawings which are made a part of this specification.
A detailed description will now be provided. Each of the appended claims defines a separate invention, which for infringement purposes is recognized as including equivalents to the various elements or limitations specified in the claims. Depending on the context, all references to the “invention”, in some cases, refer to certain specific or preferred embodiments only. In other cases, references to the “invention” refer to subject matter recited in one or more, but not necessarily all, of the claims. It is to be understood that the following disclosure describes several exemplary embodiments for implementing different features, structures, or functions of the invention. Exemplary embodiments of components, arrangements, and configurations are described below to simplify the present disclosure; however, these exemplary embodiments are provided merely as examples and are not intended to limit the scope of the invention. Additionally, the present disclosure may repeat reference numerals and/or letters in the various exemplary embodiments and across the Figures provided herein. This repetition is for the purpose of simplicity and clarity and does not in itself dictate a relationship between the various exemplary embodiments and/or configurations discussed in the Figures. Moreover, the formation of a first feature over or on a second feature in the description that follows includes embodiments in which the first and second features are formed in direct contact and also includes embodiments in which additional features are formed interposing the first and second features, such that the first and second features are not in direct contact. The exemplary embodiments presented below may be combined in any combination of ways, i.e., any element from one exemplary embodiment may be used in any other exemplary embodiment, without departing from the scope of the disclosure. The figures are not necessarily drawn to scale and certain features and certain views of the figures can be shown exaggerated in scale or in schematic for clarity and/or conciseness.
Additionally, certain terms are used throughout the following description and claims to refer to particular components. As one skilled in the art will appreciate, various entities may refer to the same component by different names, and as such, the naming convention for the elements described herein is not intended to limit the scope of the invention, unless otherwise specifically defined herein. Also, the naming convention used herein is not intended to distinguish between components that differ in name but not function. Furthermore, in the following discussion and in the claims, the terms “including” and “comprising” are used in an open-ended fashion, and thus should be interpreted to mean “including, but not limited to.”
All numerical values in this disclosure are exact or approximate values (“about”) unless otherwise specifically stated. Accordingly, various embodiments of the disclosure may deviate from the numbers, values, and ranges disclosed herein without departing from the intended scope.
Further, the term “or” is intended to encompass both exclusive and inclusive cases, i.e., “A or B” is intended to be synonymous with “at least one of A and B,” unless otherwise expressly specified herein. The indefinite articles “a” and “an” refer to both singular forms (i.e., “one”) and plural referents (i.e., one or more) unless the context clearly dictates otherwise. The terms “up” and “down”; “upward” and “downward”; “upper” and “lower”; “upwardly” and “downwardly”; “above” and “below”; and other like terms used herein refer to relative positions to one another and are not intended to denote a particular spatial orientation since the apparatus and methods of using the same may be equally effective at various angles or orientations.
In some embodiments, the gas can be or can include an exhaust gas, air, an inert gas such as nitrogen or carbon dioxide, one or more hydrocarbon gases, ammonia, water vapor, or any mixture thereof. In some embodiments, the gas can primarily be an exhaust gas, e.g., an exhaust gas from a vessel, that can be or can include, but is not limited to, nitrogen, oxygen, carbon monoxide, carbon dioxide, one or more nitrogen oxides (NOx), one or more sulfur oxides (SOx), water vapor, one or more hydrocarbons, particulate matter, e.g., soot, or any mixture thereof. In some embodiments, when the gas is conveyed through the first surface conduit 110, at least a portion of the gas can condense and pool or otherwise collect within a low point 130 of the first surface conduit 110 as the condensate 105. In some embodiments, the condensate 105 can be composed of primarily one component in the gas, e.g., a liquid hydrocarbon, liquid water, liquid ammonia (if conditions are such that liquid ammonia can be present), or the like. In other embodiments, the condensate can be composed of a mixture of two or more components present in the gas, e.g., liquid water and a liquid hydrocarbon, liquid water and ammonia in the form of aqueous ammonia, two or more liquid hydrocarbons having different chemical structures, or liquid water and two or more liquid hydrocarbons.
In some embodiments, the condensation conveyance apparatus 100 can include a first condensation conduit 135, a pump 140, and a second condensation conduit 145. The first condensation conduit 135, the pump 140, and the second condensation conduit 145 can be adapted or configured to convey at least a portion of the condensate 105 from within the first surface conduit 110 to another location. In some embodiments, the condensate 105 can be conveyed from the first surface conduit 110, through the pump 140, into the second condensation conduit 145, and, as shown, via conduit 146 into a second liquid transfer conduit 205 that can be in fluid communication with a second flow path defined by the fluid swivel assembly 117, via conduit 147 into a first gas transfer conduit 120, or via line 148 into a storage tank 107 disposed on the buoy 115 or floating adjacent the buoy (not shown). In some embodiments, the second liquid transfer conduit 205 can transfer a liquid from the second fluid flow path defined by the first swivel section 118 to a vessel storage tank as discussed in more detail below. As such, the particular location along the second liquid transfer conduit 205 that the condensate 105 can be introduced can be at any location between the first swivel section 118 and the vessel storage tank.
In other embodiments, a first portion or quantity of the condensate 105 in line 145 can be transferred via line 146 into the second liquid transfer conduit 205 and/or the second flow path defined by the first swivel section 118 and a second portion or quantity of the condensate 105 in line 145 can be transferred via line 147 into the first gas transfer conduit 120 and/or the first flow path defined by the first swivel section 118, via line 148 into the optional storage tank 107, and/or to a service vessel (not shown).
A first end of the first condensation conduit 135 can be in fluid communication with an internal volume 112 of the first surface conduit 110 such as at the low point 130. In some embodiments, at least a portion of the first condensation conduit 135 can be disposed within the first surface conduit 110. In some embodiments, a weight of the first end of the first condensation conduit 135 can be sufficient to urge the first end of the first condensation conduit 135 toward the low point 130 of the first surface conduit 110. In other embodiments, the first end of the first condensation conduit 135 can be coupled directly to an inner wall of the first surface conduit 110 in fluid communication with the internal volume 112, for example via one or more mechanical fasteners. In some embodiments, a filter 131 can be coupled to the first end of the first condensation conduit 135 such that a filter inlet can be in fluid communication with the internal volume 112 and a filter outlet can be in fluid communication with the first end of the first condensation conduit 135. The filter 131 can be adapted or configured such that the filter inlet can convey condensate 105 from the low point 130, for example by adapting or configuring the filter 131 with sufficient weight to cause the inlet of the filter 131 to face the low point 130.
In other embodiments, the first end of the first condensation conduit 135 can be in fluid communication with the internal volume 112 of the first surface conduit 110 at the low point 130 via an aperture disposed through a wall of the first surface conduit 110. In this embodiment, the first end of the first condensation conduit 135 can be maintained in fluid communication with the low point 130 of the first surface conduit 110 by being coupled directly to the wall of the first surface conduit 110. In other embodiments, an aperture disposed through the wall of the first surface conduit 110 can permit at least a portion of the condensate 105 to drain or otherwise flow, for example by using the pump 140 or a secondary pump, into an external sump volume and the first end of the first condensation conduit 135 can be in fluid communication with the external sump volume.
The pump 140 can include an inlet that can be in fluid communication with a second end of the first condensation conduit 135. The second condensation conduit 145 can have a first end in fluid communication with an outlet of the pump 140 and a second end in fluid communication with the second liquid transfer conduit 205 and/or the second flow path defined by the first swivel section 118 via line 146. In some embodiments, the second condensation conduit 145 can have a first end in fluid communication with the outlet of the pump 140 and a second end in fluid communication with the second liquid transfer conduit 205 and/or the second flow path defined by the first swivel section 118 via line 146 and, optionally, the first gas transfer conduit 120 and/or the first flow path defined by the first swivel section 118 via line 147, the storage tank 107 via line 148, and/or transferred to a service vessel (not shown).
The pump 140 can be a positive displacement pump, a centrifugal pump, or any type of pump. In some embodiments, the pump 140 can be or can include an air driven positive displacement or diaphragm pump, an electric powered pump, a hydraulic driven pump, a hydrocarbon powered pump, and/or any other power source capable of driving the pump. In some embodiments, when the pump is an air driven pump, compressed air to drive the air driven pump can be stored in an air tank 144 disposed on the buoy 115. The air tank 144 can be an accumulator tank and can collect a volume of air at pressures of between about 50 pounds per square inch gauge (psig) to about 100 psig or from about 75 psig to about 150 psig, or greater, for driving the air driven pump. In some embodiments, the air tank 144 can be adapted or configured to contain a volume of compressed air sufficient to operate the air driven pump as needed between maintenance activities on the buoy 115. In other embodiments, an air compressor can be in fluid communication with the air tank 144 and can be adapted or configured to introduce compressed air into the tank 144 when the pressure falls below a pre-determined pressure. In some embodiments, electric power to run safety lights, an electrical driven pump, if present, the air compressor, and/or other equipment can be produced by a solar panel and power storage assembly 142 disposed on the buoy 115, for example on an upper surface of a turntable 116. In other embodiments, the electric power can be provided via a power cable from an alternate location, for example, on-shore, a near-by platform, or a vessel, e.g., a vessel moored to the buoy 115. A hydraulic delivery system can be disposed on the buoy 115 to run a hydraulic driven pump. Natural gas, propane, gasoline, diesel fuel, and/or other hydrocarbons, along with the necessary equipment to provide power to a hydrocarbon driven pump, the air compressor, or any other equipment on the buoy 115, can be stored on the buoy 115 to run the hydrocarbon driven pump.
The first condensation conduit 135 and the second condensation conduit 145 can each be or can include one continuous conduit segment or one or more conduit segments coupled together. The first condensation conduit 135 and the second condensation conduit 145 can convey liquids such as the condensate 105. The first condensation conduit 135 and the second condensation conduit 145 can be made from any suitable material. For example, the condensation conduits can be made from a synthetic fiber such as polyester or nylon filament, rubber, synthetic rubbers, metal alloys, or other suitable materials. It should be understood that the conduits 146, 147, and 148 are called out separately to more clearly describe the location(s) the second end of the conduit 145 can be in fluid communication with. It should also be understood that one or more valves can be located in the second condensation conduit 145 that can be configured to prevent fluid communication between the outlet of the pump 140 and the second end of the conduit 145/146, 145/147, and/or 145/148. If such optional valve is present, the valve can be opened when removal of the condensate 105 from the internal volume 112 of the first surface conduit 110 is carried out and closed when such operation is not being carried out. In some embodiments, the optional valve, if present, can be one or more check valves. In other embodiments, the optional valve, if present, can be a butterfly valve, a ball valve, a gate valve, or other valve that can be operated manually or remotely. For example, as further described below, in some embodiments electric power can be provided to the buoy 115. If such electric power is available, a controller can be disposed on the buoy 115 that can be operated remotely, e.g., from a vessel 305 during transfer of the liquid to the vessel storage tank 310 (see
When a sufficient amount of condensate 105 collects within the first surface conduit 110 at the low point 130, the pump 140 can be operated to cause a suction within the first condensation conduit 135. The suction can convey at least a portion of the condensate 105 from the internal volume 112 to the inlet of the pump 140. The pump 140 can expel the condensate 105 from the outlet and into the second condensation conduit 145 and convey at least a portion of the condensate 105 via line 146 into the second liquid transfer conduit 205 and/or the second flow path defined by the first swivel section 118. In some embodiments, a portion of the condensate 105 expelled from the outlet of the pump 140 can be conveyed via line 148 to the optional storage tank 107, via line 137 to the first gas transfer conduit 120 and/or the flow path including the fluid swivel assembly 117, or a combination thereof. It should be understood that in some embodiments, the second condensation conduit 145 can be the outlet of the pump 140. For embodiments, the outlet of the pump 140 can be coupled directly to and in fluid communication with the second liquid transfer conduit 205 and/or the second flow path defined by the first swivel section 118 and, optionally, the first gas transfer conduit 120 and/or the first flow path defined by the first swivel section 118, and/or the storage tank 107.
Referring now to
In some embodiments, the first pipeline end manifold 315 and/or the second pipeline end manifold 325 can be located at a subsea location, e.g., on the seafloor 301. In other embodiments, the first pipeline end manifold 315 and/or the second pipeline end manifold 325 can be located at or above the surface of the body of water 126. For example, the first pipeline end manifold 315 and/or the second pipeline end manifold 325 can be located on a platform or other structure above the surface of the body of water 126. In some embodiments, the gas pipeline 330 and/or the liquid pipeline 328 can be located at a subsea location, e.g., on the seafloor 301. In other embodiments, the gas pipeline 330 and/or the liquid pipeline 328 can be located on a platform, jetty, or other structure above the surface of the body of water 126.
In some embodiments, the buoy 115 can be a catenary anchor leg mooring (CALM) type buoy, as depicted, or as a single anchor leg mooring (SALM) type buoy as described below with reference to
The buoy 115 can float in the body of water 126 and can be coupled or otherwise secured to the seafloor 301 by one or more anchor legs 303. The buoy 115 can be held in a relatively geostationary condition by the one or more anchor legs 303. As noted above, the fluid swivel assembly 117 can include a first swivel section 118. The first swivel section 118 can be rotatably coupled to a second swivel section 119. The first swivel section 118 rotatably coupled to the second swivel section 119 can define the first fluid flow path and the second fluid flow path therethrough that can be segregated from one another. The first gas transfer conduit 120 can be in fluid communication with the first swivel section 118 and a second gas transfer conduit 125 can be in fluid communication with the second swivel section 119. The first swivel section 118 and the second swivel section 119 can be adapted or configured to maintain fluid communication between the first gas transfer conduit 120 and the second gas transfer conduit 125 during rotation therebetween and when there is no rotation therebetween.
The first surface conduit 110 can be in fluid communication with the vessel storage tank 310. The second gas transfer conduit 125 can be in fluid communication with the first pipeline end manifold 315, e.g., via the gas submarine conduit 340. In some embodiments, the second gas transfer conduit 125 can extend from the second swivel section 119 and transition into two or more second gas transfer conduits 128 (two are shown) and the two or more second gas transfer conduits 128 can be in fluid communication with the first pipeline end manifold 315. The first surface conduit 110, the first gas transfer conduit 120, and the second gas transfer conduit 125 can be adapted or configured to transfer or convey the gas displaced or otherwise conveyed from the vessel 305, for example from the vessel storage tank 310, to the first pipeline end manifold 315 located at a first subsea location 320.
The gas can be displaced from the vessel storage tank 310 to keep a pressure within the vessel storage tank 310 within a specified range when introducing a liquid into the vessel storage tank 310. An end of the first gas transfer conduit 120 can be coupled to an end of the first surface conduit 110. In some embodiments, the end of the first gas transfer conduit 120 coupled to the first surface conduit 110 can have a declination angle ∂ relative to a local horizontal 152 of the buoy 115. Accordingly, a portion of the first surface conduit 110 can have a declination angle ∂. The declination angle ∂ can be from about one degree, about five degrees, or about 10 degrees to about 20 degrees, about 30 degrees, or about forty degrees from the local horizontal 152. The declination angle ∂ can cause the low point 130 within the first surface conduit 110. It should be noted that the local horizontal 152 may stay static with regard to the buoy 115 while a declination angle relative to a surface of the body of water 126 may change with wave action and other perturbations of the buoy 115.
The flow path including the fluid swivel assembly 117 can include the first swivel section 118, the second swivel section 119, the second gas transfer conduit 125, the gas submarine conduit 340, and the first pipeline end manifold 315. In some embodiments, when a portion of the condensate 105 flows via line 145 and 147 into the first gas transfer conduit 105 and/or the first swivel section 118, the second condensation conduit 145 can be coupled to a portion of the first gas transfer conduit 120 and/or the first swivel section 118 via line 147 and located such that any condensate 105 conveyed into the first gas transfer conduit 120 and/or the first swivel section 118 from lines 145 and 147 can fall down the first gas transfer conduit 120 through a path defined by the first swivel section 118 and/or directly into the flow path defined by the first swivel section 118, through the second swivel section 119, and down to the first pipeline end manifold 315. In some embodiments, at least a portion of the condensate 105 can collect or pool within a portion of the first pipeline end manifold 315 or the gas pipeline 330. The gas pipeline 330 can be an elongated conduit. The gas pipeline 330 can be in fluid communication with and span from the first pipeline end manifold 315 to another location, such as a near-shore or on-shore facility or location. The first surface conduit 110, the first gas transfer conduit 120, the fluid swivel assembly 117, the second gas transfer conduit 125, the gas submarine conduit 340, the first pipeline end manifold 315, and the gas pipeline 330 can be adapted or configured to transfer or convey the gas from the floating vessel 305 and/or the vessel storage tank 310 to the near-shore or on-shore location. In some embodiments, if a portion of the condensate 105 flows into the first pipeline end manifold 315, the condensate 105 can be removed from the first pipeline end manifold 315 and/or the gas pipeline 330 utilizing a pipeline pig, for example, during a pigging maintenance operation.
In some embodiments, if the storage tank 107 is used, the storage tank 107 can be disposed on the buoy 115, e.g., on the turntable 116, can float adjacent the buoy 115, or can be located within or adjacent to the first subsea location 320. In some embodiments, when the storage tank 107 is subsea, the storage tank can be in fluid communication with the flow path including the fluid swivel assembly 117. The storage tank 107 can be adapted or configured to contain sufficient amounts of the condensate 105 such that removal of the condensate 105 from the storage tank 107 can be performed during normal maintenance activities for the buoy 115. The storage tank 107 can be made from any suitable material. For example, the storage tank 107 can be made from a synthetic fiber such as polyester or nylon filament, rubber, synthetic rubbers, a steel alloy, a polyvinyl chloride plastic, or other suitable materials.
A first liquid transfer conduit 160 (two are shown) can be in fluid communication with the second swivel section 119 and, as noted above, the second liquid transfer conduit 205 (two are shown) can be in fluid communication with the second flow path defined by the first swivel section 118. The first swivel section 118 and the second swivel section 119 can be adapted or configured to maintain fluid communication between the first liquid transfer conduit 160 and the second liquid transfer conduit 205 during rotation therebetween and when there is no rotation therebetween.
The second pipeline end manifold 325 can be located at a second subsea location 327. The liquid pipeline 328 can be an elongated conduit. The liquid pipeline 328 can be in fluid communication with and span from the second pipeline end manifold 325 to another location, such as the near-shore or on-shore facility or location. The second pipeline end manifold 325 can be in fluid communication with the first liquid transfer conduit 160. The second liquid transfer conduit 205 can be in fluid communication with a second surface conduit 210 (two are shown). The second surface conduit 210 can be in fluid communication with the vessel 305 and/or the vessel storage tank 310. The liquid pipeline 328, the second pipeline end manifold 325, the first liquid transfer conduit 160, the fluid swivel assembly 117, the second liquid transfer conduit 205, and the second surface conduit 210 can be adapted or configured to convey a liquid, for example a liquid hydrocarbon, from the near-shore or on-shore location to the vessel 305 and/or the vessel storage tank 310. It should be understood and as noted above, the second liquid transfer conduit 205 also includes the second surface conduit 210 for purposes of where the condensate 105 can be introduced into. In other words, the second liquid transfer conduit 205 includes the conduit disposed on the buoy 115 and the second surface conduit 210 that is located in the water and not on the buoy 115 that can be in fluid communication with the vessel storage tank 310.
The liquid transferred from the liquid pipeline 328 to the vessel 305 and/or the vessel storage tank 310 can be or can include, but is not limited to, raw hydrocarbons such as crude oil or a fraction thereof, refined hydrocarbons such as, but not limited to, diesel fuel, jet fuel, kerosene, and/or gasoline, water, ammonia, or any mixture thereof. The gas in the vessel storage tank 310 can be displaced from the vessel storage tank 310 simultaneously with the introduction of the liquid into the vessel storage tank 310.
In some embodiments, the gas submarine conduit 340 can be adapted or configured to convey, in addition to the gas, liquids such as a portion of the condensate 105. The gas submarine conduit 340 can include a first submarine conduit 341 and a second submarine conduit 342. The gas submarine conduit 340 can be in fluid communication with the first pipeline end manifold 315 and the second gas transfer conduit 125. The gas submarine conduit 340 can be coupled between the first pipeline end manifold 315 and the second gas transfer conduit 125 for fluid communication therebetween. The gas submarine conduit 340 can be coupled between the first pipeline end manifold 315 and the two or more second gas transfer conduits 128 for fluid communication therebetween.
In some embodiments, the gas submarine conduit 340 can be configured in a Chinese lantern configuration between the buoy 115 and the first subsea location 320. For example, the first and second submarine conduits 341, 342 can each include one or more negatively buoyant members 362 coupled thereto between the first pipeline end manifold 315 and the second gas transfer conduit 125. In some embodiments, the one or more negatively buoyant members 362 can be coupled thereto between the first pipeline end manifold 315 and a midpoint of each of the first and second submarine conduits 341, 342. In other embodiments, the one or more negatively buoyant members 362 can be coupled to the first and second submarine conduits 341, 342 between the first pipeline end manifold 315 and the midpoint of each of the first and second submarine conduits 341, 342 and one or more negatively buoyant members 362 can be coupled to each of the first and second submarine conduits 341, 342 between the midpoint and the second gas transfer conduit 125. In still other embodiments, the first and second submarine conduits 341, 342 can include one or more negatively buoyant members 362 and one or more positively buoyant members 364 coupled thereto between the first pipeline end manifold 315 and the second gas transfer conduit 125. The positively buoyant member(s) 364, if present, can be located between the midpoint and the second gas transfer conduit 125, between the first pipeline end manifold 315 and the midpoint, or a combination thereof. As such, in some embodiments, one or more negatively buoyant members 362 and one or more positively buoyant members 364 can be distributed along the first and second submarine conduits 341, 342 to maintain the first and second submarine conduits 341, 342 in the Chinese lantern configuration.
The one or more negatively buoyant members 362 can urge each of the first and second submarine conduits 341, 342 toward the seafloor 302 to maintain the first and second submarine conduits 341, 342 in the Chinese lantern configuration. In other embodiments, the gas submarine conduit 340 can be adapted or configured in a steep-S configuration or a lazy-S configuration between the buoy 115 and the first subsea location 320. The gas submarine conduit 340 can be adapted or configured to convey the gas from the fluid swivel assembly 117 to the first subsea location 320, e.g., the pipeline end manifold 315. The one or more negatively buoyant members 362 can be made from any suitable material that can sink in water, e.g., sea water. For example, the one or more negatively buoyant members 362 can be made from or include metal chains, cement, lead, natural stone, metal alloy, or other suitable materials. The one or more positively buoyant members 364 can be made from or include syntactic foams, foamed thermoset or thermoplastic materials, thermoset or thermoplastic materials filled with particles (such as glass, plastic, micro-spheres, and/or ceramics), rubber, nylon, composites of these materials, any other material buoyant in water, e.g., sea water, or any combination thereof.
In some embodiments, the liquid submarine conduit 345 can include a third submarine conduit 346 and a fourth submarine conduit 347. The liquid submarine conduit 345 can be in fluid communication with the second pipeline end manifold 325 and the first liquid transfer conduit 160. The liquid submarine conduit 345 can be coupled between the second pipeline end manifold 325 and the first liquid transfer conduit 160. The liquid submarine conduit 345 can be adapted or configured in a Chinese lantern configuration, a steep-S configuration, or a lazy-S configuration between the buoy 115 and the second subsea location 327. For example, one or more negatively buoyant members 362 and one or more positively buoyant members 364 can be distributed along each of the third and fourth submarine conduits 346, 347 to maintain the third and fourth submarine conduits 346, 347 in the Chinese lantern configuration, the steep-S configuration, or the lazy-S configuration. The Chinese Lantern, steep-S, and lazy-S configurations are all well known to people having ordinary skill in the art of subsea engineering or subsea riser engineering.
The gas submarine conduit 340 and the liquid submarine conduit 345 can be adapted or configured to compensate for motions of the buoy 115. The gas submarine conduit 340 and liquid submarine conduit 345 can be flexible and can be any type of elongated conduit. In some embodiments, the gas submarine conduit 340 and the liquid submarine conduit 345 can be comprised of a plurality of conduit segments connected together.
It should be understood that any of the conduits, e.g., the first surface conduit 110, the second surface conduit 210, the gas submarine conduit 340, the liquid submarine conduit 345, etc., can each be or can include a plurality of conduit segments connected thereto. The second surface conduit 210 and the liquid submarine conduit 345 can convey fluids such as the liquid. The first surface conduit 110, the second surface conduit 210, the gas submarine conduit 340, and the liquid submarine conduit 345 can be made from any suitable material. For example, the first surface conduit 110, the second surface conduit 210, the gas submarine conduit 340, and the liquid submarine conduit 345 can be made from a synthetic fiber such as polyester or nylon filament, rubber, synthetic rubbers, metal alloys, or other suitable materials.
In some embodiments, the pressure developed within the vessel storage tank 310 during liquid loading may not be sufficient to push the gas all the way through the gas pipeline 330. Accordingly, one or more blowers 335 (three are shown) can be used to maintain the pressure within the vessel storage tank 310 within specified design ranges. In some embodiments the blower 335 can be located at the first subsea location 320, on the buoy 115, floating adjacent the buoy 115, on the floating vessel 305, on an adjacent platform, and/or on shore in fluid communication with the gas pipeline 330. The blower 335 can be adapted or configured to provide a propulsive force within the conduits to assist the gas conveyance through the pipeline 330. For example, the blower 335 can increase a mass flow of the gas that can be conveyed from the vessel storage tank 310 through the pipeline 330 to another location such as the near-shore or on-shore facility or location. The blower 335 can induce or otherwise produce a partial vacuum and/or increase a pressure within the gas pipeline 330, the first pipeline end manifold 315, the second gas transfer conduit 125, the first surface conduit 110 and/or the first gas transfer conduit 120, to draw or otherwise urge the gas from the vessel 305 such that the gas can be conveyed to another location, such as the near-shore or on-shore facility or location.
The gas, once conveyed to the near-shore or on-shore facility or location, can be processed to reduce or remove at least a portion of one or more contaminants therefrom. In some embodiments, the gas can be an exhaust gas from the vessel that can include water and one or more contaminants. Such contaminants can be or can include, but are not limited to, oxides of sulfur (SOx), oxides of nitrogen (NOx), carbon monoxide, carbon dioxide, hydrocarbons, and carbon particles suspended in the gas, or any mixture thereof.
It should be understood that although the first pipeline end manifold 315 and the second pipeline end manifold 325 are depicted as being located at two locations 320, 327 on two different skids 510, 712 at some distance from one another, the first and second pipeline end manifolds 315, 325 can be located adjacent each other and/or formed or assembled on a single skid adapted or configured to accommodate the first pipeline end conduit 505 and the second pipeline end conduit 705.
The gas submarine conduit 340 can be in fluid communication with the first swivel section 918 and the gas pipeline 330. The liquid submarine conduit 345 can be in fluid communication with the first swivel section 918 and the liquid pipeline 328. The first swivel section 918 and the second swivel section 919 can be adapted or configured to maintain fluid communication between the gas submarine conduit 340 and the gas pipeline 330 during rotation therebetween and when there is no rotation therebetween. The first swivel section 918 and the second swivel section 919 can be adapted or configured to maintain fluid communication between the liquid submarine conduit 345 and the liquid pipeline 328 during rotation therebetween and when there is no rotation therebetween. The liquid can be conveyed from the liquid pipeline 328, through the liquid submarine conduit 345, through the second surface conduit 210 and to the vessel 305 and/or the vessel storage tank 310. Gas discharged from the vessel 305 and/or the vessel storage tank 310 can be conveyed through the first surface conduit 110, through the gas submarine conduit 340, through the gas pipeline 330 to another location, such as the near-shore or on-shore facility or location.
The liquid pipeline 328 can be in fluid communication with and span from the pipeline end manifold 1016 to another location, such as the near-shore or on-shore facility or location. The liquid pipeline 328, the second pipeline end conduit 705, the liquid submarine conduit 345 (two are shown), and the second surface conduit 210 can be adapted or configured to convey the liquid, for example the liquid hydrocarbon, from the near-shore or on-shore location to the floating vessel 305 and/or the vessel storage tank 310. The gas in the vessel storage tank 310 can be displaced from the vessel storage tank 310 simultaneously with the introduction of the liquid into the vessel storage tank 310.
In some embodiments, the gas submarine conduit 340 can be configured in a Chinese lantern configuration between the buoy 1015 and the subsea location 1020. The gas submarine conduit 340 can include one or more negatively buoyant members 162 coupled thereto (ten are shown) between the pipeline end manifold 1016 and the buoy 1015. In some embodiments, the one or more negatively buoyant members 362 can be coupled thereto between the pipeline end manifold 1016 and a midpoint of the gas submarine conduit 340. In other embodiments, one or more negatively buoyant members 362 can be coupled to the gas submarine conduit 340 between the pipeline end manifold 1016 and the midpoint of the gas submarine conduit 340 and one or more negatively buoyant members 362 can be coupled to the gas submarine conduit 340 between the midpoint and the buoy 1015.
The liquid submarine conduit 345 can be adapted or configured in a Chinese lantern configuration. For example, one or more positively buoyant members 364 can be distributed along the third submarine conduit 346 and the fourth submarine conduit 347 to maintain the liquid submarine conduit 345 in the Chinese lantern configuration. One or more positively buoyant members 364 and one or more negatively buoyant members 362 can be distributed along the third submarine conduit 346 and the fourth submarine conduit 347 to maintain the liquid submarine conduit 345 in the Chinese lantern configuration. The liquid submarine conduit 345 can be adapted or configured to convey the liquid from the subsea location 1020, e.g., the pipeline end manifold 1016, to the fluid swivel assembly 117.
In some embodiments, referring to
In the eductor 1203, the liquid or at least a portion thereof transferred from the liquid pipeline 328 to the vessel 305 (see
In some embodiments, in the eductor 1203, the liquid or at least a portion thereof transferred from the liquid pipeline 328 to the vessel 305 via the liquid submarine conduit 345, the first liquid transfer conduit 160, the second fluid flow path defined by the swivel 117, and the second liquid transfer conduit 205 can flow into an inlet of the eductor 1203, through a converging section of the eductor 1203 that can narrow in cross-sectional area, into and through a constricted throat, into and out of a diverging section, and out of the eductor 1203 via an outlet. As the liquid exits the throat and enters the diverging section, a region of low pressure in the eductor 1203 can be created that can draw the condensate 105 into the eductor 1203 through a suction inlet of the eductor 1203 and out of the floating or buoyant conduit 110. The condensate 105 can mix with the liquid and exit the outlet of the eductor 1203. The liquid or the at least a portion thereof introduced into the eductor 1203 as the motive or driving fluid can be at any suitable pressure and/or suitable flow rate that can generate a sufficient vacuum or suction for removing at least a portion of the condensate 105 from the floating or buoyant conduit 110.
In some embodiments, one or more valves 1205 can be in fluid communication with the condensation conduit 135 at a location between the low point 130 of the first floating or buoyant conduit 110 (see
In other embodiments, a pump, e.g., the pump 140 shown in
In still other embodiments, a pressurized gas, e.g., air from air tank 144 (see
In some embodiments, a valve can be located between the pump 140 (or pressurized gas source) and the inlet of the eductor 1203 and/or a valve can be located between the outlet of the eductor 1203 and the liquid submarine conduit 345, the first liquid transfer conduit 160, the second fluid flow path defined by the swivel 117, and/or the second liquid transfer conduit 205. In some embodiments, such valve can be a check valve. In other embodiments, such valve can be a butterfly valve, a ball valve, a gate valve, a globe valve, a needle valve, a pinch valve, a plug valve, or other valve that can be operated manually or remotely.
In some embodiments, the condensation conveyance apparatus 1316 can include a pump 1340 and a condensation conduit 1335. In some embodiments, the pump 1340 can be disposed within the first surface conduit 1310 at a low point 1311 of the first surface conduit 1310. In some embodiments, the condensation conduit 1335 can be connected to the pump 1340 at a first end 1336 and can be configured to be disposed completely within the first surface conduit 1310 and the first gas conduit 1320. In some embodiments, the condensation conduit 1335 can be configured to not penetrate a wall of the first gas conduit 1320 and not penetrate a wall of the first surface conduit 1310. In some embodiments the condensation conduit 1335 can be routed over a high point 1321 of the first gas transfer conduit 1320 such that a second end 1337 of the condensation conduit 1335 can be disposed within the first gas transfer conduit 1320 at a location located downstream of the high point 1321 of the first gas transfer conduit 1320. In other embodiments, the pump 1340 and the condensation conduit 1335 can be configured to convey at least a portion of any condensate 105 from the low point 1311 into the second liquid transfer conduit 205 or the second surface conduit 210 (see
In some embodiments, the pump 1340 can be configured as an air driven pump or an electric driven pump. In some embodiments the condensation conveyance apparatus 1316 can include a power conduit 1350 configured to provide power to the pump 1340. In some embodiments, the pump 1340 can be configured to generate a pressure to convey the condensate 105 through the condensate conduit 1335. In some embodiments, the power conduit 1350 can be routed through a port 1360 that can be disposed on or through a sidewall of the first gas transfer conduit 1320. In some embodiments, the power conduit 1350 can be an air conduit, in the case of an air driven pump, or an electrical cable in the case of an electric driven pump. In some embodiments, the power conduit 1350 can be connected to a power source 1370, e.g., an air source or an electric power source, depending on the type of pump. In some embodiments, the port 1360 can be configured with a grommet 1361 that can be configured to provide a gas tight seal between an outer surface of the power conduit 1350 and an inner surface of the port 1360.
The pump 1340 can be configured to generate a pressure to transfer the condensate from the low point 1321 of the first surface conduit 1310 over the high point 1321 of the gas conduit 120 to the second end 1337 of the condensation conduit 1335. In some embodiments, the pump 1340 can be a submersible pump configured to operate by pushing, as opposed to drawing, the condensate 105 during the pumping process. The condensation conveyance apparatus 1316 can be configured to convey at least a portion of the condensate 105 from the pump 1340 to the second end 1337 of the condensation conduit 1335 while the gas is conveyed through the first surface conduit 1310 and the first gas conduit 1320, for example. while the tanker is loading cargo so as avoid interruptions to the cargo loading operations. In some embodiments, the first surface conduit 1310 and the first gas transfer conduit 1320 can be free of an access port configured to permit the condensation conduit 1335 to pass therethrough or to connect thereto.
In some embodiments, the condensation conveyance apparatus 1316 can be the same or substantially the same as described above with reference to
The condensation conveyance apparatus 1316 can be configured to convey at least a portion of the condensate 105 from the pump 1340 to the second end 1337 of the condensation conduit 1335 while the gas is being conveyed through the first gas transfer conduit 1520 and a first surface conduit 1510, for example while a tanker or other vessel is loading cargo so as avoid interruptions to the cargo loading operations. The first surface conduit 1510 can be configured to float in the body of water 126. The first gas transfer conduit 1520 can be disposed on the buoy 1515 and can be a rigid pipe or other conduit configured to maintain the “U-shaped” condensation collection section 1511. In some embodiments, the first surface conduit 1510 and the first gas transfer conduit 1520 can be free of an access port configured to permit the condensation conduit 1335 to pass therethrough or to connect thereto.
In some embodiments, the condensation conveyance apparatus 1616 can be configured to recover at least a portion of the condensate 105 from the sump 1611. In some embodiments, the condensation conveyance apparatus 1616 can be disposed within an interior of the sump 1611 and the first gas transfer conduit 1620 can receive at least a portion of the condensate 105 via the condensation conveyance apparatus 1616. In some embodiments, the first gas conduit 1620, the sump 1611, the third gas conduit 1622, and the floating gas conduit 1610 can be in fluid communication with the first flow path defined by the first swivel section 118 of the fluid swivel assembly 117 coupled to the buoy 1615.
In some embodiments, the sump 1611 can be configured as a vertically orientated vessel, segment of pipe, conical structure, or other similar structure that can include a low point 1612. In some embodiments, the sump 1611 can be a low point between the first surface conduit 1610, the third gas transfer conduit, and a high point 1621 of the first gas conduit 1620, such that the condensate 105 can be collected within the sump 1611. In some embodiments, a deflector plate 1613 can be disposed within the sump 1611. In some embodiments, the deflector plate 1613 can be configured to direct a gas toward the first gas conduit 1620 and direct the condensate 105 toward the low point 1612 of the sump 1611. In some embodiments, the sump 1611 can include a caisson 1661 that can provide access into the interior of the sump 1611.
In some embodiments, the condensate collection apparatus 1616 can include a pump 1640 and a condensation conduit 1644. In some embodiments, the pump 1640 can include a pump drive motor 1641, a pump shaft 1642, and an impeller 1643 disposed toward the bottom of the sump 1611. In some embodiments, the pump drive motor 1641 can be configured to drive the impeller 1643 via the pump shaft 1642. In some embodiments, the pump 1640 can be powered via a power conduit 1671 that can be connected to a power source 1670. In some embodiments, the pump 1640 can be an electrically powered pump or an air powered or air driven pump.
In some embodiments, the pump shaft 1642 and the impeller 1643 can be disposed within the sump 1611 via a port 1660. In some embodiments, the condensate collection apparatus 1616 can include a grommet 1662. In some embodiments, the port 1660 and the grommet 1662 can be configured to provide a seal between an outer surface of the pump shaft 1642 and an inner surface of the caisson 1661 such that gas and/or condensate can be prevented from escaping from the sump 1611 to the atmosphere.
In some embodiments, the condensation conduit 1644 can be connected to the pump caisson 1661 at a first end 1645 thereof and can be configured to be disposed completely within the first gas conduit 1620 and the sump 1611. In some embodiments, the pump 1640 can be configured to generate a pressure at the impeller 1643 to convey at least a portion of the condensate 105 via the condensation conduit 1644 toward a second end 1646 of the condensation conduit 1644. In some embodiments, the condensation conduit 1644 can be configured to not penetrate a wall of the first gas conduit 1620 or a wall of the sump 1611, or a wall of the third gas conduit 1622. In some embodiments the condensation conduit 1644 can be routed over a high point 1621 of the first gas transfer conduit 1620 such that the second end 1646 of the condensation conduit 1644 can be disposed within the first gas conduit 1620 at a location located downstream of the high point 1621 of the first gas transfer conduit 1620. In other embodiments, the pump 1640 and the condensation conduit 1644 can be configured to convey at least a portion of any condensate 105 that accumulates within the sump 1611 into the second liquid transfer conduit 205 or the second surface conduit 210 (see
The condensation conveyance apparatus 1616 can be configured to convey at least a portion of the condensate 105 from the pump impeller 1643 to the second end 1646 of the condensation conduit 1644 while the gas is being conveyed through the first gas transfer conduit 1620, the third gas conduit 1622, and the first surface conduit 1610, for example while a tanker or other vessel is loading cargo so as avoid interruptions to the cargo loading operations. In some embodiments, a submersible pump can be disposed within the sump 1611 and can be used to covey at least a portion of the condensate 105 into the condensation conduit 1644 instead of the pump 1640. In some embodiments, the first surface conduit 1610, the third gas conduit 1622, the sump 1611, and the first gas transfer conduit 1620 can be free of an access port configured to permit the condensation conduit 1644 to pass therethrough or to connect thereto.
In some other embodiments, the condensation conveyance apparatus 1716 can include the pump 1730 and the second condensation conduit 1731 similar to the condensation conveyance system 1316 shown in
The condensation conveyance apparatus 1716 can be configured to convey at least a portion of the condensate 105 from an interior of the sump 1611 to the second end 1733 of the second condensation conduit 1732 while the gas is flowing through the first gas transfer conduit 1620, the third gas transfer conduit 1622 and the first surface conduit 1610, for example while the tanker is loading cargo, so as avoid interruptions to the cargo loading operations.
In some embodiments, the heated condensation collection section 1812 of the first surface conduit 1810 can be heated via a heater 1830 disposed on the buoy 1815. In some embodiments, the heater 1830 can be configured to heat a heating medium. In some embodiments, the heating medium can be routed through a conduit 1840 that can be disposed on an exterior of the first surface conduit 1810, as shown, or along an interior of the first surface conduit 1810, not shown. In some embodiments, the buoy 1815 can include a circulation pump 1831 to convey the heating medium through the conduit 1840. The heated heating medium in conduit 1840 can circulate therethrough and indirection transfer heat to the heated condensation collection section 1812. In some embodiments, the heater 1830 can be a fired heater that can be heated by burning diesel, gasoline, propane, or another similar fuel. In other embodiments, the heater 1830 can be an electrically powered heater. In such other embodiments, electric power can be provided to the heater 1830 from an onshore location, from a vessel, from one or more batteries disposed on the buoy 1815 that can be charged via one or more solar panels disposed on the buoy 1815, from a generator disposed on the buoy 1815, or any other suitable electric power source.
The heating medium can be or can include any suitable gas, liquid, or combination thereof. In some embodiments, the heating medium can be water, one or more hydrocarbons, ethylene-glycol, or a mixture thereof. In some embodiments, the heating medium can be anti-freeze or other type of fluid. In some embodiments, the heating medium can be heated to any temperature suitable for the particular composition of the heating medium such that the heating medium can transfer sufficient heat to the condensate 105 to cause at least a portion of the condensate to vaporize. In some embodiments, the heating medium can be heated to a temperature sufficient to heat the heated condensate collection section 1812 to a temperature in a range from about 5° C., about 10° C., about 20° C., about 30° C., about 40° C., or about 50° C. to about 60° C., about 70° C., about 80° C., about 90° C., about 100° C., about 110° C., or more.
In some embodiments, the heated condensate collection section 1918 of the first surface conduit 1910 can be heated such that condensate does not condense out of the gas when the gas is conveyed through the first surface conduit 1910. In other embodiments, the heated condensate collection section 1918 can be heated when a condensate 105 is present in the low point 1911 of the first surface conduit 1910 to cause at least a portion of the condensate 105 to vaporize. In some embodiments, the heated condensate collection section 1918 can be heated to a temperature that is above a temperature at which the condensate condenses out of the flowing gas, or above a boiling temperature of the condensate 105. In some embodiments, the heated condensate collection section 1918 can be heated to a temperature in a range from about 5° C., about 10° C., about 20° C., about 30° C., about 40° C., or about 50° C. to about 60° C., about 70° C., about 80° C., about 90° C., about 100° C., about 110° C., or more.
It should be understood that the buoys 1615 described above with reference to
It should be understood that rather than a single point mooring marine terminal, other types of mooring systems can be used to moor the floating vessel during transfer or conveyance of the gas from the vessel to the subsea location. In some embodiments, the vessel can be moored via a spread mooring system during conveyance of the gas from the vessel to the subsea location. A suitable spread mooring system can include the disconnectable spread mooring and riser tower system disclosed in U.S. Pat. No. 11,198,490. In other embodiments, the vessel can be moored via a stabilized mooring system such as the stabilized mooring system disclosed in U.S. Pat. No. 11,319,036. In other embodiments, the vessel can be moored via a disconnectable tower yoke mooring system such as those disclosed in U.S. Pat. Nos. 9,650,110; 11,267,532; and 11,279,446. In other embodiments, the vessel can be moored via a disconnectable submerged yoke mooring system such as the mooring system disclosed in U.S. Pat. No. 11,738,828.
Certain embodiments and features have been described using a set of numerical upper limits and a set of numerical lower limits. It should be appreciated that ranges including the combination of any two values, e.g., the combination of any lower value with any upper value, the combination of any two lower values, and/or the combination of any two upper values are contemplated unless otherwise indicated. Certain lower limits, upper limits and ranges appear in one or more claims below. All numerical values are “about” or “approximately” the indicated value, and take into account experimental error and variations that would be expected by a person having ordinary skill in the art.
Various terms have been defined above. To the extent a term used in a claim can be not defined above, it should be given the broadest definition persons in the pertinent art have given that term as reflected in at least one printed publication or issued patent. Furthermore, all patents, test procedures, and other documents cited in this application are fully incorporated by reference to the extent such disclosure can be not inconsistent with this application and for all jurisdictions in which such incorporation can be permitted.
While certain preferred embodiments of the present invention have been illustrated and described in detail above, it can be apparent that modifications and adaptations thereof will occur to those having ordinary skill in the art. It should be, therefore, expressly understood that such modifications and adaptations may be devised without departing from the basic scope thereof, and the scope thereof can be determined by the claims that follow.
This application claims priority to U.S. Provisional Patent Application No. 63/439,973, filed on Jan. 19, 2023, which is incorporated by reference herein.
Number | Date | Country | |
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63439973 | Jan 2023 | US |