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1. (WO2013123012) GAS TURBINE ENGINE COMPONENT WITH COMPOUND CUSP COOLING CONFIGURATION
Latest bibliographic data on file with the International Bureau   

Pub. No.: WO/2013/123012 International Application No.: PCT/US2013/025887
Publication Date: 22.08.2013 International Filing Date: 13.02.2013
IPC:
F02C 7/12 (2006.01) ,F01D 25/12 (2006.01) ,F01D 5/18 (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
7
Features, component parts, details or accessories, not provided for in, or of interest apart from, groups F02C1/-F02C6/158; Air intakes for jet-propulsion plants
12
Cooling of plants
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
01
MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
D
NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
25
Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
08
Cooling; Heating; Heat insulation
12
Cooling
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
01
MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
D
NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
5
Blades; Blade-carrying members; Heating, heat-insulating, cooling, or antivibration means on the blades or the members
12
Blades
14
Form or construction
18
Hollow blades; Heating, heat-insulating, or cooling means on blades
Applicants:
UNITED TECHNOLOGIES CORPORATION [US/US]; One Financial Plaza Hartford, CT 06101, US
Inventors:
XU, JinQuan; US
Agent:
NELSON, Stuart; Kinney & Lange, P.A. 312 So. Third St. Minneapolis, MN 55415, US
Priority Data:
13/544,22709.07.2012US
61/599,35015.02.2012US
Title (EN) GAS TURBINE ENGINE COMPONENT WITH COMPOUND CUSP COOLING CONFIGURATION
(FR) COMPOSANT POUR MOTEUR À TURBINE À GAZ À CONFIGURATION DE REFROIDISSEMENT À POINTS DE REBROUSSEMENT COMPOSITES
Abstract:
(EN) A component for a gas turbine engine including a gas path wall having a first surface and a second surface. A cooling hole extends through the gas path wall from an inlet in the first surface through a transition to an outlet in the second surface. Cusps are formed on the transition.
(FR) L’invention concerne un composant pour un moteur à turbine à gaz comprenant une paroi de chemin de gaz présentant une première surface et une seconde surface. Un orifice de refroidissement s’étend à travers la paroi de chemin de gaz depuis une entrée au niveau de la première surface, à travers une partie de transition, jusqu’à une sortie au niveau de la seconde surface. Des points de rebroussement sont formés sur la partie de transition.
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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, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IS, JP, KE, KG, KM, 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, 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, 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, ML, MR, NE, SN, TD, TG)
Publication Language: English (EN)
Filing Language: English (EN)