Full hoop casing for midframe of industrial gas turbine engine

Myers, Gerald A.; Charron, Richard C.

Title: Full hoop casing for midframe of industrial gas turbine engine

Patent · Tue Dec 01 00:00:00 EST 2015

OSTI ID:1227362

Myers, Gerald A.; Charron, Richard C.

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).

View Patent

Cite

Export

Save

Research Organization:: Siemens Energy, Inc., Orlando, FL (United States)

Sponsoring Organization:: USDOE

DOE Contract Number:: FC26-05NT42644

Assignee:: Siemens Energy, Inc

Patent Number(s):: 9,200,565

Application Number:: 13/310,855

OSTI ID:: 1227362

Resource Relation:: Patent File Date: 2011 Dec 05

Country of Publication:: United States

Language:: English

References (8)

Annular stator structure for a rotary machine Chaplin, Gary F.; Lucas, Jr., Arthur W. https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4722184 US Patent Document 4,722,184	patent	February 1988
Backbone support structure for compressor Balkcum, III, James Tyson; Wilson, Jr., Jack W. https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5354174 US Patent Document 5,354,174	patent	October 1994
Gas Turbine engine casing construction Goodwin, Jeremy P. https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5885056 US Patent Document 5,885,056	patent	March 1999
Shipping system for jet aircraft engine and method of installing and removing jet aircraft engine Rossway, Ronald A.; Hatch, Robert F.; Suroosh, Behzad B. https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6170141 US Patent Document 6,170,141	patent	January 2001
Gas turbine engine with increased fuel efficiency and method for accomplishing the same Montoya, Cesar https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6385959 US Patent Document 6,385,959	patent	May 2002
Combustor apparatus for a gas turbine engine Rice, Edward C.; Pack, Spencer D. https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6401447 US Patent Document 6,401,447	patent	June 2002
Casing of a Gas Turbine Engine Maltson, John David https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20100031673 US Patent Application 12/524766; 20100031673	patent-application	February 2010
Modular Transvane Assembly Wilson, Jody; Nordlund, Raymond; Charron, Richard https://doi.org/https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20100077719 US Patent Application 12/420149; 20100077719	patent-application	April 2010

Similar Records

Swirling midframe flow for gas turbine engine having advanced transitions

Patent · Tue Dec 27 00:00:00 EST 2016 · OSTI ID:1227362

Montgomery, Matthew D.; Charron, Richard C.; Rodriguez, Jose L.; +3 more

High temperature turbine engine structure

Patent · Tue Jul 20 00:00:00 EDT 1993 · OSTI ID:1227362

Carruthers, W D; Boyd, G L

Structural cooling fluid tube for supporting a turbine component and supplying cooling fluid

Patent · Tue Feb 24 00:00:00 EST 2015 · OSTI ID:1227362

Charron, Richard; Pierce, Daniel

Related Subjects

33 ADVANCED PROPULSION SYSTEMS

Title: Full hoop casing for midframe of industrial gas turbine engine

Citation Formats

References (8)

Similar Records

Related Subjects