Solar Turbines Inc.

Jason Michael Robertson

Daniel James Doll

Ian Trevor Brown

Charles C Cornelius

Danny Ferrel Smith

Gabriel James Glynn

Antonio Acuña

Steven Gastelum

John Raymond Hawley

A gas turbine engine includes a compressor having first annular connection structure at a forward end portion of an air inlet housing of the compressor. The gas turbine engine may also include intake ducting having second annular connection structure adjacent a central passage of the intake ducting. The first annular connection structure and the second annular connection structure may form at least part of an interface between the air inlet housing and the intake ducting during operation of the gas turbine engine. The first and second annular connection structures may have shapes allowing the first annular connection structure to be moved through and beyond the second annular connection structure in a forward direction, the forward direction being opposite a direction of compressed air flow in the compressor during operation.

Gas turbine engine and system for servicing a gas turbine engine

A system for moving an auxiliary component of a gas turbine engine is disclosed. The system may have a mobile support platform configured to support the auxiliary component during operation of the gas turbine engine. The system may further have at least one guide assembly operably connected to the mobile support platform and configured to guide movement of the mobile support platform. The system may also have a drive assembly operably connected to the mobile support platform and configured to impart movement of the mobile support platform between an elevated position and a lowered position.

Mobile platform system for a gas turbine engine

A power system includes a gas turbine engine, which may include a gear box. The gear box may include a pipe connection configured to receive a removable pipe. The power system may also include a moveable support configured to fasten to the pipe connection to at least partially support the gear box.

System for supporting and servicing a gas turbine engine

A modular cart for a gas turbine engine is disclosed. The modular cart may have a first cart with a first connection portion and a first mounting location. The modular cart may further have a second cart with a second connection portion and a second mounting location. The first connection portion of the first cart may be configured to attach to the second connection portion of the second cart. The modular cart may also have a cart component configured to interchangeably mount to either the first mounting location of the first cart or to the second mounting location of the second cart.

Growing community of inventors

San Diego, CA, United States of America

Jason Michael Robertson