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Method and system for moving a gas turbine engine

A gas turbine and engine technology that is applied in the field of power systems and can solve time-consuming and difficult problems

Inactive Publication Date: 2010-12-08
SOLAR TURBINES
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Therefore, it can be difficult and time consuming to separate the different parts of the gas turbine engine from each other to service the gas turbine engine, and to remove one or more parts of the gas turbine engine from the common base independently of the other parts

Method used

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  • Method and system for moving a gas turbine engine
  • Method and system for moving a gas turbine engine
  • Method and system for moving a gas turbine engine

Examples

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Embodiment Construction

[0044] Figures 1A to 1D shown for gas turbine engines with ( Figures 1A to 1D Not shown in the first embodiment of the support system 10 of the power system, the support system 10 is installed with a power transmission unit 12 and a power load 14 . The support system 10 may include a base / mount 16 that supports the power transfer unit 12 and the power load 14 . For example, if Figures 1A to 1D As shown, base / support 16 may be a frame. Base / stand 16 may be supported by a variety of entities including, but not limited to, the ground (not shown), one or more structures supported by the ground (not shown), one or more structures of the vehicle ( not shown), and / or one or more structures of the ship (not shown).

[0045]Support system 10 may include various devices for supporting a gas turbine engine (not shown). For example, the support system 10 may include a frame 28 for supporting the gas turbine engine from the base / mount 16 . The frame 28 may include a standoff 30 an...

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PUM

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Abstract

A method of using a gas turbine engine (182) is provided. The method may include supporting a first portion (184) of the gas turbine engine one or more guide tracks (208) extending in a first direction (276), the first direction being at an angle to a longitudinal axis (192) of the gas turbine engine. The method may also include moving the first portion of the gas turbine engine in the first direction on the guide tracks independently of a second portion (188) of the gas turbine engine.

Description

technical field [0001] The present invention relates to power systems, and more particularly, to power systems having gas turbine engines. Background technique [0002] Many power systems include a gas turbine engine and a power load, such as a pump, compressor, or generator, drivingly connected to the gas turbine engine. Various structural support systems are used to support the gas turbine engine and power loads of this power system. In some such power systems, both the gas turbine engine and the power load are mounted by fixed mounts to a common non-movable support structure. [0003] Unfortunately this support structure may make replacement or repair of the gas turbine engine difficult. Removing the gas turbine engine from the immovable support structure may involve uncoupling the gas turbine engine from multiple fixed mounts, which may require considerable time and effort. Furthermore, after the gas turbine engine is unwound from the support structure, removing the g...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F01D25/28F16M1/04
CPCF01D25/285F05B2230/60F05D2230/60F05D2250/313F05D2230/68F05D2230/70F16M5/00F01D25/28F16M1/04
Inventor I·T·布朗D·J·多尔J·M·罗伯逊
Owner SOLAR TURBINES