Abstract: A 2×1 multi-shaft power island system is provided. The system includes a first gas turbine (GT)/gas turbine generator (GTG)/heat recovery steam generator (HRSG) island, the GT/GTG/HRSG island. The GT/GTG/HRSG island includes a first gas turbine system configured to produce power by combusting a fuel, and a first turbine generator system mechanically coupled to the first gas turbine system and configured to produce electrical power. The GT/GTG/HRSG island additionally includes a first HRSG system fluidly coupled to the first gas turbine system and configured to generate a first steam. The system further includes a second GT/GTG/HRSG island. The second GT/GTG/HRSG island includes a second gas turbine system configured to produce power by combusting the fuel, and a second turbine generator system mechanically coupled to the second gas turbine system and configured to produce electrical power.

Abstract: Certain embodiments of the present disclosure are related to a supportive apparatus for the head and neck. Embodiments of the invention incorporate a C-shaped apparatus shaped to support the posterior region of the neck. A center region found in certain embodiments of the C-shaped apparatus is placed on the posterior of a neck. Lateral supports found in certain embodiments of the C-shaped apparatus are placed on the lateral aspect of a neck. Embodiments of the invention include an opening across a center region functioning to support the apparatus, and to further act as to ventilate a user's nape.

Abstract: Certain embodiments of the present disclosure are related to a supportive apparatus for the head and neck. Embodiments of the invention incorporate a C-shaped apparatus shaped to support the posterior region of the neck. A center region found in certain embodiments of the C-shaped apparatus is placed on the posterior of a neck. Lateral supports found in certain embodiments of the C-shaped apparatus are placed on the lateral aspect of a neck. Embodiments of the invention include an opening across a center region functioning to support the apparatus, and to further act as to ventilate a user's nape.

Abstract: Solutions for minimizing the impact of servicing a turbo machine are disclosed. In one embodiment, an apparatus for conveying a turbo machine component can include: a motive system for moving the apparatus along a surface; a platform system operably connected to the motive system, the platform system for supporting the component of the turbo machine, the platform system can include: a first portion fixed to the motive system; and a second portion moveably coupled to the first portion, the second portion for modifying a position of the turbo machine component; and a control system operably connected to the platform system, the control system for controlling at least one of a rate of movement or a direction of the second portion of the platform system.

Abstract: Solutions for minimizing the impact of servicing a turbo machine are disclosed. In one embodiment, an apparatus for conveying a turbo machine component can include: a motive system for moving the apparatus along a surface; a platform system operably connected to the motive system, the platform system for supporting the component of the turbo machine, the platform system can include: a first portion fixed to the motive system; and a second portion moveably coupled to the first portion, the second portion for modifying a position of the turbo machine component; and a control system operably connected to the platform system, the control system for controlling at least one of a rate of movement or a direction of the second portion of the platform system.

Abstract: Embodiments include a system having a turbine support key having a set of key segments selectively stackable together in a plurality of combinations to adjust a thickness between turbine supports based solely on a selection of the key segments from the set.

Abstract: Embodiments include a system having a turbine support key having a set of key segments selectively stackable together in a plurality of combinations to adjust a thickness between turbine supports based solely on a selection of the key segments from the set.