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Machine translation
1. (WO2014110445) SYSTEM AND METHOD FOR PROTECTING COMPONENTS IN A GAS TURBINE ENGINE WITH EXHAUST GAS RECIRCULATION
Latest bibliographic data on file with the International Bureau   

Pub. No.:    WO/2014/110445    International Application No.:    PCT/US2014/011148
Publication Date: 17.07.2014 International Filing Date: 10.01.2014
Chapter 2 Demand Filed:    13.11.2014    
IPC:
F01D 25/30 (2006.01), F02C 3/34 (2006.01), F02C 7/18 (2006.01)
Applicants: GENERAL ELECTRIC COMPANY [US/US]; 1 River Road Schenectady, New York 12345 (US) (AE, AG, AM, AO, AU, AZ, BB, BF, BH, BJ, BN, BR, BW, BY, BZ, CA, CF, CG, CI, CL, CM, CO, CR, CU, DM, DO, DZ, EC, EG, GA, GD, GE, GH, GM, GN, GQ, GT, GW, HN, ID, IL, IN, IR, KE, KG, KM, KN, KP, KR, KZ, LA, LC, LK, LR, LS, LY, MA, MD, ME, MG, ML, MN, MR, MW, MX, MY, MZ, NA, NE, NG, NI, NZ, OM, PA, PE, PG, PH, QA, RU, RW, SA, SC, SD, SG, SL, SN, ST, SV, SY, SZ, TD, TG, TH, TJ, TM, TN, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW only).
EXXONMOBIL UPSTREAM RESEARCH COMPANY [US/US]; 22777 Springwoods Village Parkway E2.4A.296 Spring, Texas 77389 (US) (AL, AT, BA, BE, BG, CH, CN, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, JP, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR only)
Inventors: BIYANI, Pramod K.; (US).
SAHA, Rajarshi; (IN).
DASOJI, Anil Kumar; (IN).
HUNTINGTON, Richard A.; (US).
MITTRICKER, Franklin F.; (US)
Agent: SWANSON, Tait R.; P.O. Box 692289 Houston, Texas 77269 (US)
Priority Data:
61/751,902 13.01.2013 US
14/135,055 19.12.2013 US
Title (EN) SYSTEM AND METHOD FOR PROTECTING COMPONENTS IN A GAS TURBINE ENGINE WITH EXHAUST GAS RECIRCULATION
(FR) SYSTÈME ET PROCÉDÉ POUR PROTÉGER DES COMPOSANTS DANS UN MOTEUR À TURBINE À GAZ AVEC RECIRCULATION DES GAZ D'ÉCHAPPEMENT
Abstract: front page image
(EN)A system includes a gas turbine engine that includes a turbine section having one or more turbine stages between an upstream end and a downstream end, an exhaust section disposed downstream from the downstream end of the turbine section, and a fluid supply system coupled to the exhaust section. The fluid supply system is configured to route an inert gas to the exhaust section.
(FR)L'invention concerne un système qui comprend un moteur à turbine à gaz qui comprend une section de turbine ayant un ou plusieurs étages de turbine entre une extrémité amont et une extrémité aval, une section d'échappement disposée en aval par rapport à l'extrémité aval de la section de turbine et un système d'alimentation en fluide couplé à la section d'échappement. Le système d'alimentation en fluide est configuré pour acheminer un gaz inerte vers la section d'échappement.
Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, JP, KE, KG, KN, KP, KR, KZ, LA, LC, LK, LR, LS, LT, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SA, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW.
African Regional Intellectual Property Organization (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Organization (AM, AZ, BY, KG, KZ, RU, TJ, TM)
European Patent Office (AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, KM, ML, MR, NE, SN, TD, TG).
Publication Language: English (EN)
Filing Language: English (EN)