Abstract: A rotatable solar tower with an airfoil structure is described. Solar panels are stacked vertically to create the skin of an airfoil. By installing the airfoil vertically so that its longitudinal axis is perpendicular to the ground and allowing the airfoil to rotate freely 360 degrees into the wind, the horizontal forces on the airfoil from the wind are significantly reduced compared to a round cylinder with the same diameter. This allows the airfoil structure to be lightweight in design while spanning several hundred feet in height and producing several hundred kilowatts of electrical power on a small footprint of land. The solar panels may have 3-axes of rotation, i.e., rotation of the tower about the base, horizontal extension of the solar frame assemblies and vertical extension of the solar panels. Wind turbines may also be provided in or on the tower.

Abstract: Methods of sealing tubulars are disclosed herein, which methods may include: providing a patch plug assembly that includes: a shaft; a wedge coupled to the shaft; a slip coupled to the shaft; a plug slidably coupled to the wedge; and a ferrule disposed between the wedge and the plug; pushing the slip against the tubular; pushing the plug against the ferrule after the slip is pushed against the tubular; pushing the ferrule against the wedge after the plug is pushed against the ferrule; and pushing a plug portion of the plug against an inner surface of the tubular.

Abstract: A rotatable solar tower with an airfoil structure is described. Solar panels are stacked vertically to create the skin of an airfoil. By installing the airfoil vertically so that its longitudinal axis is perpendicular to the ground and allowing the airfoil to rotate freely 360 degrees into the wind, the horizontal forces on the airfoil from the wind are significantly reduced compared to a round cylinder with the same diameter. This allows the airfoil structure to be lightweight in design while spanning several hundred feet in height and producing several hundred kilowatts of electrical power on a small footprint of land. The solar panels may have 3-axes of rotation, i.e., rotation of the tower about the base, horizontal extension of the solar frame assemblies and vertical extension of the solar panels. Wind turbines may also be provided in or on the tower.

Abstract: Methods of sealing tubulars are disclosed herein, which methods may include: providing a patch plug assembly that includes: a shaft; a wedge coupled to the shaft; a slip coupled to the shaft; a plug slidably coupled to the wedge; and a ferrule disposed between the wedge and the plug; pushing the slip against the tubular; pushing the plug against the ferrule after the slip is pushed against the tubular; pushing the ferrule against the wedge after the plug is pushed against the ferrule; and pushing a plug portion of the plug against an inner surface of the tubular.

Abstract: Disclosed herein are downhole landing assemblies including a downhole landing assembly for an oil or gas well, downhole landing assembly may include: an upper seat cylinder capable of being coupled to an upper portion of a tubular string; a lower seat cylinder capable of being coupled to a lower portion of the tubular string, wherein the lower seat cylinder may be coupled to the upper seat cylinder; a landing seat coupled to the lower seat cylinder, the landing seat may have two inner surfaces; and a landing mandrel having two outer surfaces, wherein one outer surface of the two outer surfaces may be capable of being abutted against one inner surface of the two inner surfaces.

Abstract: Various embodiments provide systems, methods, and computer program products for dynamically monitoring transport of a plurality of packages potentially containing regulated goods so as to ensure compliance with one or more regulations within a plurality of jurisdictions. The embodiments utilize one or more computer processors or one or more executable portions to: receive transport data associated with the transport of at least one of the plurality of packages and regulatory data associated with the at least one jurisdiction in which transport occurs; determine whether the one of the plurality of packages contains at least one regulated good; if the presence of at least one regulated good is determined, validate consignor data and the transport data; whereby in response to an unsuccessful validation, at least one report is generated to prevent or otherwise mitigate transport of the one of the plurality of packages in the at least one identified jurisdiction.

Abstract: Disclosed herein are downhole landing assemblies including a downhole landing assembly for an oil or gas well, downhole landing assembly may include: an upper seat cylinder capable of being coupled to an upper portion of a tubular string; a lower seat cylinder capable of being coupled to a lower portion of the tubular string, wherein the lower seat cylinder may be coupled to the upper seat cylinder; a landing seat coupled to the lower seat cylinder, the landing seat may have two inner surfaces; and a landing mandrel having two outer surfaces, wherein one outer surface of the two outer surfaces may be capable of being abutted against one inner surface of the two inner surfaces.

Abstract: Methods of sealing tubulars are disclosed herein, which methods may include: providing a patch plug assembly that includes: a shaft; a wedge coupled to the shaft; a slip coupled to the shaft; a plug slidably coupled to the wedge; and a ferrule disposed between the wedge and the plug; pushing the slip against the tubular; pushing the plug against the ferrule after the slip is pushed against the tubular; pushing the ferrule against the wedge after the plug is pushed against the ferrule; and pushing a plug portion of the plug against an inner surface of the tubular.

Abstract: Methods of sealing tubulars are disclosed herein, which methods may include: providing a patch plug assembly that includes: a shaft; a wedge coupled to the shaft; a slip coupled to the shaft; a plug slidably coupled to the wedge; and a ferrule disposed between the wedge and the plug; pushing the slip against the tubular; pushing the plug against the ferrule after the slip is pushed against the tubular; pushing the ferrule against the wedge after the plug is pushed against the ferrule; and pushing a plug portion of the plug against an inner surface of the tubular.

Abstract: A rotatable solar tower with an airfoil structure is described. Solar panels are stacked vertically to create the skin of an airfoil. By installing the airfoil vertically so that its longitudinal axis is perpendicular to the ground and allowing the airfoil to rotate freely 360 degrees into the wind, the horizontal forces on the airfoil from the wind are significantly reduced compared to a round cylinder with the same diameter. This allows the airfoil structure to be lightweight in design while spanning several hundred feet in height and producing several hundred kilowatts of electrical power on a small footprint of land. The solar panels may have 3-axes of rotation, i.e., rotation of the tower about the base, horizontal extension of the solar frame assemblies and vertical extension of the solar panels. Wind turbines may also be provided in or on the tower.

Abstract: Disclosed herein are downhole landing assemblies including a downhole landing assembly for an oil or gas well, downhole landing assembly may include: an upper seat cylinder capable of being coupled to an upper portion of a tubular string; a lower seat cylinder capable of being coupled to a lower portion of the tubular string, wherein the lower seat cylinder may be coupled to the upper seat cylinder; a landing seat coupled to the lower seat cylinder, the landing seat may have two inner surfaces; and a landing mandrel having two outer surfaces, wherein one outer surface of the two outer surfaces may be capable of being abutted against one inner surface of the two inner surfaces.

Abstract: Disclosed herein are downhole disconnect assemblies for disconnecting downhole tubulars. Those disconnect assemblies may each include: 1) a housing having an inner surface and a groove disposed in the inner surface; 2) a sub disposed in the housing, the sub having a window aligned with the groove; 3) a locking lug extending through the window and having a projection removably disposed in the groove; 4) a prop sleeve disposed in the sub and releasably coupled to the locking lug; and 5) a load transfer sleeve pushing the housing.

Abstract: Disclosed herein are downhole landing assemblies including a downhole landing assembly for an oil or gas well, downhole landing assembly may include: an upper seat cylinder capable of being coupled to an upper portion of a tubular string; a lower seat cylinder capable of being coupled to a lower portion of the tubular string, wherein the lower seat cylinder may be coupled to the upper seat cylinder; a landing seat coupled to the lower seat cylinder, the landing seat may have two inner surfaces; and a landing mandrel having two outer surfaces, wherein one outer surface of the two outer surfaces may be capable of being abutted against one inner surface of the two inner surfaces.

Abstract: A system for operating a downhole system in a wellbore having pressure inlet ports formed in the production tubing, the one or more pressure inlet ports extending through the production tubing between the annular area and the outer surface of the conduit, the one or more pressure inlet ports being situated below a first top sealing device relative to the conduit. The system includes an annular pressure control valve coupled to a metal conduit below the one or more pressure inlet ports in the wellbore, the annular pressure control valve being configurable in an open position and in a closed position, where the annular pressure control valve transitions between the closed position and the open position responsive to the annular pressure. The system includes a second bottom sealing device coupled to a bottom portion of the conduit below the annular pressure control valve.

Abstract: Various embodiments provide systems, methods, and computer program products for dynamically monitoring transport of a plurality of packages potentially containing regulated goods so as to ensure compliance with one or more regulations within a plurality of jurisdictions. The embodiments utilize one or more computer processors or one or more executable portions to: receive transport data associated with the transport of at least one of the plurality of packages and regulatory data associated with the at least one jurisdiction in which transport occurs; determine whether the one of the plurality of packages contains at least one regulated good; if the presence of at least one regulated good is determined, validate consignor data and the transport data; whereby in response to an unsuccessful validation, at least one report is generated to prevent or otherwise mitigate transport of the one of the plurality of packages in the at least one identified jurisdiction.

Abstract: Various embodiments provide systems, methods, and computer program products for dynamically monitoring transport of a plurality of packages potentially containing regulated goods so as to ensure compliance with one or more regulations within a plurality of jurisdictions. The embodiments utilize one or more computer processors or one or more executable portions to: receive transport data associated with the transport of at least one of the plurality of packages and regulatory data associated with the at least one jurisdiction in which transport occurs; determine whether the one of the plurality of packages contains at least one regulated good; if the presence of at least one regulated good is determined, validate consignor data and the transport data; whereby in response to an unsuccessful validation, at least one report is generated to prevent or otherwise mitigate transport of the one of the plurality of packages in the at least one identified jurisdiction.

Abstract: The disclosure herein includes a tubular cutting assembly for cutting a downhole tubular string, which tubular cutting assembly may include: a landing seat capable of being disposed on the downhole tubular string; and a tubular cutting assembly including: a landing mandrel capable of being coupled to the landing seat; a motor disposed below the landing mandrel; and a cutter assembly coupled to the motor.

Abstract: The disclosure herein includes a tubular cutting assembly for cutting a downhole tubular string, which tubular cutting assembly may include: a landing seat capable of being disposed on the downhole tubular string; and a tubular cutting assembly including: a landing mandrel capable of being coupled to the landing seat; a motor disposed below the landing mandrel; and a cutter assembly coupled to the motor.

Abstract: A system for operating a downhole system in a wellbore having pressure inlet ports formed in the production tubing, the one or more pressure inlet ports extending through the production tubing between the annular area and the outer surface of the conduit, the one or more pressure inlet ports being situated below a first top sealing device relative to the conduit. The system includes an annular pressure control valve coupled to a metal conduit below the one or more pressure inlet ports in the wellbore, the annular pressure control valve being configurable in an open position and in a closed position, where the annular pressure control valve transitions between the closed position and the open position responsive to the annular pressure. The system includes a second bottom sealing device coupled to a bottom portion of the conduit below the annular pressure control valve.

Abstract: A downhole shifting sleeve device includes a first segment and a second segment each including a housing, a sleeve, and a seat surface connected to the sleeve. Each seat surface is configured to engage a plug traveling through an inner bore of the device, which transfers the associated sleeve from a first position to a second position. The seat surface of the second segment is formed by a selective seat assembly. When the first sleeve is in the first position, the selective seat assembly is in a retracted position in which an inner diameter of the selective seat assembly is greater than or equal to an inner diameter of the second sleeve. When the first sleeve is in the second position, the selective seat assembly is in a deployed position in which the inner diameter of the selective seat assembly is less than the inner diameter of the second sleeve.