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1. (WO2018128791) PROTECTED CORE INLET
Latest bibliographic data on file with the International Bureau    Submit observation

Pub. No.: WO/2018/128791 International Application No.: PCT/US2017/067101
Publication Date: 12.07.2018 International Filing Date: 18.12.2017
IPC:
F02C 3/13 (2006.01) ,F02K 3/075 (2006.01) ,F02K 3/06 (2006.01)
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02
COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
C
GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
3
Gas-turbine plants characterised by the use of combustion products as the working fluid
04
having a turbine driving a compressor
13
having variable working fluid interconnections between turbines or compressors or stages of different rotors
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02
COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
K
JET-PROPULSION PLANTS
3
Plants including a gas turbine driving a compressor or a ducted fan
02
in which part of the working fluid by-passes the turbine and combustion chamber
04
the plant including ducted fans, i.e. fans with high volume, low-pressure outputs, for augmenting jet thrust, e.g. of double-flow type
075
controlling flow ratio between flows
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02
COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
K
JET-PROPULSION PLANTS
3
Plants including a gas turbine driving a compressor or a ducted fan
02
in which part of the working fluid by-passes the turbine and combustion chamber
04
the plant including ducted fans, i.e. fans with high volume, low-pressure outputs, for augmenting jet thrust, e.g. of double-flow type
06
with front fan
Applicants: GENERAL ELECTRIC COMPANY[US/US]; 1 River Road Schenectady, NY 12345, US
Inventors: MONIZ, Thomas, Ory; US
LARICCHIUTA, Mark, John; US
Agent: KACHUR, Pamela, A.; US
DIMAURO, Peter, T.; US
WINTER, Catherine, J.; US
MIDGLEY, Stephen, G.; US
GNIBUS, Michael, M.; US
Priority Data:
15/398,82005.01.2017US
Title (EN) PROTECTED CORE INLET
(FR) ENTRÉE DE NOYAU PROTÉGÉE
Abstract:
(EN) A gas turbine engine defines a radial direction and an axial centerline. The gas turbine engine includes a core turbine engine that defines a core inlet. The core inlet is oriented with respect to the axial centerline and positioned along the radial direction such that the area available to capture foreign object debris is minimized.
(FR) Un moteur à turbine à gaz définit une direction radiale et une ligne centrale axiale. Le moteur à turbine à gaz comprend un moteur à turbine à noyau qui définit une entrée de noyau. L'entrée de noyau est orientée par rapport à la ligne centrale axiale et positionnée le long de la direction radiale de sorte que la zone disponible pour capturer des débris d'objet étrangers est réduite à un minimum.
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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, DJ, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, JO, JP, KE, KG, KH, KN, KP, KR, KW, KZ, LA, LC, LK, LR, LS, 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 (ARIPO) (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Office (AM, AZ, BY, KG, KZ, RU, TJ, TM)
European Patent Office (EPO) (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)