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Machine translation
1. (WO2012109421) JOINING MECHANISM AND METHOD FOR INTERLOCKING MODULAR TURBINE ENGINE COMPONENT WITH A SPLIT RING
Latest bibliographic data on file with the International Bureau   

Pub. No.:    WO/2012/109421    International Application No.:    PCT/US2012/024438
Publication Date: 16.08.2012 International Filing Date: 09.02.2012
IPC:
F01D 9/04 (2006.01), F01D 5/14 (2006.01)
Applicants: SIEMENS ENERGY, INC. [US/US]; 4400 Alafaya Trail Orlando, Florida 32826-2399 (US) (For All Designated States Except US).
MIKRO SYSTEMS, INC. [US/US]; 1180 Seminole Trail, Suite 220 Charlottesville, Virginia 22901 (US) (For All Designated States Except US).
MERRILL, Gary B. [US/US]; (US) (For US Only).
JAMES, Allister W. [GB/US]; (US) (For US Only).
FRASER, Iain A. [US/US]; (US) (For US Only)
Inventors: MERRILL, Gary B.; (US).
JAMES, Allister W.; (US).
FRASER, Iain A.; (US)
Agent: SWANSON, Erik C.; Siemens Corporation Intellectual Property Dept. 170 Wood Avenue South Iselin, New Jersey 08830 (US)
Priority Data:
13/023,721 09.02.2011 US
Title (EN) JOINING MECHANISM AND METHOD FOR INTERLOCKING MODULAR TURBINE ENGINE COMPONENT WITH A SPLIT RING
(FR) MÉCANISME DE LIAISON ET PROCÉDÉ PERMETTANT D'ENCLENCHER UNE PIÈCE MODULAIRE DE MOTEUR À TURBINE AVEC UNE BAGUE FENDUE
Abstract: front page image
(EN)A modular airfoil assembly (200) and related method for interlocking components of an airfoil structure (210) including a platform (220), an airfoil (210) having a shoulder (230) and a stem (232) extending outward from the shoulder. A ring element (100) positioned against the stem (232) secures the shoulder (230) against the platform (210). First and second members (100a, 100b) of the ring element (100) are bonded together with a portion (128j) of a surface (112a) of the second member (100b) extending within and bonded to a portion (128i) of a surface (112b) of the first member (100a).
(FR)L'invention concerne un ensemble de profil aérodynamique modulaire (200) et un procédé associé permettant d'enclencher des composants d'une structure de profil aérodynamique (210) comprenant une plate-forme (220), un profil aérodynamique (210) ayant un épaulement (230) et une tige (232) s'étendant vers l'extérieur depuis l'épaulement. Un élément de type bague (100) positionné contre les tiges (232) assujettit l'épaulement (230) contre la plate-forme (220). Des premier et second éléments (100a, 100b) de l'élément de type bague (100) sont reliés ensemble, une partie (128j) d'une surface (112a) du second élément (100b) s'étendant à l'intérieur d'une et étant reliée à une partie (128i) d'une surface (112b) du premier élément (100a).
Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, 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, 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 (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, MD, 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, ML, MR, NE, SN, TD, TG).
Publication Language: English (EN)
Filing Language: English (EN)