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US 9,863,279 B2Granted
Multipurpose support system for a gas turbine
AssigneeGeneral Electric Company
InventorsDonald Gordon Laing, Jose Francisco Estrada, Gerardo Plata Contreras, Mehdi Milani Baladi
Life of this patent
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Abstract
A system includes a gas turbine engine and a multipurpose gas turbine engine support frame couple to the gas turbine engine. The multipurpose gas turbine support frame is configured to support the gas turbine engine during both operation and transport of the gas turbine engine.
Claims15
A system, comprising:
- a gas turbine engine comprising a gas generator portion and a power turbine portion;
- and
- a multipurpose gas turbine support frame;
- and
- a framework directly coupled to and extending from the multipurpose gas turbine support frame, wherein the framework and the multipurpose gas turbine support frame together enclose at least the power turbine portion of the gas turbine engine between the framework and the multipurpose gas turbine support frame;
- wherein the multipurpose gas turbine support frame is coupled to the gas turbine engine and is configured to support the gas turbine engine during both operation and transport of the gas turbine engine, and wherein the framework and the multipurpose gas turbine support frame together enclose a majority of the gas turbine engine along a length of a longitudinal axis of the gas turbine engine between the framework and the multipurpose gas turbine support frame;
- and
- wherein the multipurpose gas turbine support frame comprises at least one rigid support extending vertically relative to the longitudinal axis and configured to restrain the gas turbine engine when exposed to transportation loads during transport of the gas turbine engine and to support the gas turbine engine, the at least one rigid support comprises a first end coupled to the multipurpose gas turbine support frame and a second end directly coupled to the power turbine portion of the gas turbine engine, and wherein the multipurpose gas turbine support frame comprises at least one flexible support extending vertically relative to the longitudinal axis and configured to restrain the gas turbine engine during operation of the gas turbine engine and to support the gas turbine engine, the at least one flexible support comprises a third end coupled to the multipurpose gas turbine support frame and a fourth end directly coupled to the gas generator portion of the gas turbine engine.
5 more elements
A system, comprising:
- a multipurpose gas turbine support frame configured to couple to a gas turbine engine comprising a gas generator portion and a power turbine portion, wherein the multipurpose gas turbine support frame is configured to support the gas turbine engine during at least assembly, operation, transport, overhaul, and removal of the gas turbine engine;
- and
- a framework directly coupled to and extending from the multipurpose gas turbine support frame, wherein the framework and the multipurpose gas turbine support frame together are configured to enclose at least the power turbine portion of the gas turbine engine between the framework and the multipurpose gas turbine support frame, and wherein the framework and the multipurpose gas turbine support frame together are configured to enclose a majority of the gas turbine engine along a length of a longitudinal axis of the gas turbine engine between the framework and the multipurpose gas turbine support frame;
- wherein the multipurpose gas turbine support frame comprises at least one rigid support extending vertically relative to the longitudinal axis and configured to restrain the gas turbine engine when exposed to transportation loads during transport of the gas turbine engine and to support the gas turbine engine, the at least one rigid support comprises a first end coupled to the multipurpose gas turbine support frame and a second end configured to directly couple to the power turbine portion of the gas turbine engine, and wherein the multipurpose gas turbine support frame comprises at least one flexible support extending vertically relative to the longitudinal axis and configured to restrain the gas turbine engine during operation of the gas turbine engine and to support the gas turbine engine, the at least one flexible support comprises a third end coupled to the multipurpose gas turbine support frame and a fourth end configured to directly couple to the gas generator portion of the gas turbine engine.
1 more element
A system, comprising:
- a gas turbine engine comprising a gas generator portion and a power turbine portion;
- a multipurpose gas turbine support frame coupled to the gas turbine engine, wherein the multipurpose gas turbine support frame is configured to support the gas turbine engine during both operation and transport of the gas turbine engine;
- and
- a framework directly coupled to and extending from the multipurpose gas turbine support frame, wherein the framework comprises a first framework portion that together with the multipurpose gas turbine support frame encloses at least a first portion of the gas generator portion of the gas turbine engine between the first framework portion and the multipurpose gas turbine support frame, and the framework comprises a second framework portion that together with the multipurpose gas turbine support frame encloses at least a second portion of the power turbine portion of the gas turbine engine between the second framework portion and the multipurpose gas turbine support frame, and wherein the first framework portion and the second framework portion are configured to directly contact each other when the gas generator portion is coupled to the power turbine portion, and wherein the framework and the multipurpose gas turbine support frame together enclose a majority of the gas turbine engine along a length of a longitudinal axis of the gas turbine engine between the framework and the multipurpose gas turbine support frame;
- wherein the multipurpose gas turbine support frame comprises at least one rigid support extending vertically relative to the longitudinal axis and configured to restrain the gas turbine engine when exposed to transportation loads during transport of the gas turbine engine and to support the gas turbine engine, the at least one rigid support comprises a first end coupled to the multipurpose gas turbine support frame and a second end directly coupled to the power turbine portion of the gas turbine engine, and wherein the multipurpose gas turbine support frame comprises at least one flexible support extending vertically relative to the longitudinal axis and configured to restrain the gas turbine engine during operation of the gas turbine engine and to support the gas turbine engine, the at least one flexible support comprises a third end coupled to the multipurpose gas turbine support frame and a fourth end directly coupled to the gas generator portion of the gas turbine engine.
2 more elements
Dependencies are inferred from the claim text.