Full hoop casing for midframe of industrial gas turbine engine
Abstract
A can annular industrial gas turbine engine, including: a single-piece rotor shaft spanning a compressor section (82), a combustion section (84), a turbine section (86); and a combustion section casing (10) having a section (28) configured as a full hoop. When the combustion section casing is detached from the engine and moved to a maintenance position to allow access to an interior of the engine, a positioning jig (98) is used to support the compressor section casing (83) and turbine section casing (87).
- Inventors:
- Issue Date:
- Research Org.:
- Siemens Energy, Inc., Orlando, FL (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1227362
- Patent Number(s):
- 9,200,565
- Application Number:
- 13/310,855
- Assignee:
- Siemens Energy, Inc
- DOE Contract Number:
- FC26-05NT42644
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 2011 Dec 05
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 33 ADVANCED PROPULSION SYSTEMS
Citation Formats
Myers, Gerald A., and Charron, Richard C. Full hoop casing for midframe of industrial gas turbine engine. United States: N. p., 2015.
Web.
Myers, Gerald A., & Charron, Richard C. Full hoop casing for midframe of industrial gas turbine engine. United States.
Myers, Gerald A., and Charron, Richard C. Tue .
"Full hoop casing for midframe of industrial gas turbine engine". United States. https://www.osti.gov/servlets/purl/1227362.
@article{osti_1227362,
title = {Full hoop casing for midframe of industrial gas turbine engine},
author = {Myers, Gerald A. and Charron, Richard C.},
abstractNote = {A can annular industrial gas turbine engine, including: a single-piece rotor shaft spanning a compressor section (82), a combustion section (84), a turbine section (86); and a combustion section casing (10) having a section (28) configured as a full hoop. When the combustion section casing is detached from the engine and moved to a maintenance position to allow access to an interior of the engine, a positioning jig (98) is used to support the compressor section casing (83) and turbine section casing (87).},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2015},
month = {12}
}
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