Granted Patent B2

US 12,510,028 · App. 18/298,013 · Granted Dec 30, 2025

Inventors: Tony Yeung (Houston, TX); Ricardo Rodriguez-Ramon (Houston, TX); Joseph Foster (Houston, TX); Nicholas Tew (Houston, TX)

Assignee: BJ Energy Solutions, LLC

F02C7/20E21B43/26E21B43/2607F02C7/32F02C7/36F04B17/00F04B53/22

Abstract

Claims (21)

1 . A method for removal of a direct drive unit (DDU) from an enclosure comprising a base and access doors, the DDU including an engine having a first interface to couple the engine to air inlet ducting and a second interface to couple the engine to air exhaust ducting, wherein the DDU comprises a gas turbine engine cantilever mounted to a gearbox, wherein the gearbox is disposed on and connected to a platform, the method comprising:

providing the platform for the DDU, the platform comprising one or more lift openings and configured to support the engine;

inserting a lifting mechanism through the access doors of the enclosure and into the one or more lift openings of the platform; and

removing the DDU from the enclosure through the access doors via the lifting mechanism, which includes lifting the DDU with the lifting mechanism,

wherein a front of the gearbox couples to a drive shaft, a rear of the gearbox couples to the gas turbine engine, and a centerline of the gearbox extends through the gearbox equidistant from the front and rear of the gearbox, wherein the one or more lift openings comprise a first lift opening proximate the drive shaft and a second lift opening proximate the gas turbine engine, wherein the gearbox is disposed on the platform such that the centerline of the gearbox is located between the first and second lift openings, and wherein a distance between the second lift opening and the centerline is greater than a distance between the centerline and the first lift opening.

2 . The method of claim 1 , further comprising:

detaching one or more fasteners attaching the base to the platform to allow movement of the DDU prior to lifting the DDU with the lifting mechanism; and

operating one or more drive fasteners positioned in contact with the base to move the platform along the base, thereby to position the one or more lift openings for access by the lifting mechanism.

3 . The method of claim 1 , wherein the platform further comprises a first surface supporting the engine, and a second surface in moveable engagement with the base.

4 . The method of claim 1 , further comprising providing lubricant to a lubrication portion of the platform thereby facilitating movement of the platform within the enclosure.

5 . The method of claim 1 , further comprising a pad disposed between the base and the platform.

6 . The method of claim 4 , wherein the lubrication portion is disposed between the base and the platform, and the method further comprises sliding the platform for movement in a selected direction.

7 . A method for removal of a direct drive unit (DDU) from an enclosure comprising a base and access doors, the DDU including an engine having a first interface to couple the engine to air inlet ducting and a second interface to couple the engine to air exhaust ducting, wherein the DDU comprises a gas turbine engine cantilever mounted to a gearbox, wherein the gearbox is disposed on and connected to a platform, the method comprising:

providing the platform for the DDU, the platform comprising one or more lift openings and configured to support the engine;

detaching one or more fasteners attaching the base to the platform to allow movement of the DDU;

operating one or more drive fasteners positioned in contact with the base to move the platform along the base, thereby to position the one or more lift openings for access by the lifting mechanism;

inserting, subsequent to moving the platform, a lifting mechanism through the access doors of the enclosure and into the one or more lift openings of the platform; and

removing the DDU from the enclosure through the access doors via the lifting mechanism, which includes lifting the DDU with the lifting mechanism,

wherein a front of the gearbox couples to a drive shaft, a rear of the gearbox couples to the gas turbine engine, and a centerline of the gearbox extends through the gearbox equidistant from the front and rear of the gearbox, wherein the one or more lift openings comprise a first lift opening proximate the drive shaft and a second lift opening proximate the gas turbine engine, wherein the gearbox is disposed on the platform such that the centerline of the gearbox is located between the first and second lift openings, and wherein a distance between the second lift opening and the centerline is greater than a distance between the centerline and the first lift opening.

8 . The method of claim 7 , wherein the platform comprises the one or more drive fasteners.

9 . The method of claim 7 , further comprising providing lubricant between the base and the platform.

Assignments (3)

Continuity (12)

References Cited (400)