Patent SG-11201810589R-A (SG)
Title: System and method for performing an in situ repair of an internal component of a gas turbine engine
Inventor: ROBERTS HERBERT CHIDSEY
IPC: B29C73/02
Filed: 2017-06-12
Abstract: 117 119 In 00 00 N O C (12) INTERNATIONAL APPLICATION PUBLISHED UNDER THE PATENT COOPERATION TREATY (PCT) (19) World Intellectual Property Organization International Bureau (43) International Publication Date 21 December 2017 (21.12.2017) WIP0 I PCT ill~~~~~~~~ 011101110VIIIVIIInn Hol Hull 111111111mm oimIE (10) International Publication Number WO 2017/218385 Al (51) International Patent Classification: B29C 73/02 (2006.01) B29L 31/30 (2006.01) B23P 6/00 (2006.01) (21) International Application Number: PCT/US2017/036966 (22) International Filing Date: 12 June 2017 (12.06.2017) (25) Filing Language: English (26) Publication Language: English (30) Priority Data: 15/185,194 17 June 2016 (17.06.2016) US (71) Applicant: GENERAL ELECTRIC COMPANY [US/US]; 1 River Road, Schenectady, NY 12345 (US). (72) Inventors: ROBERTS, Herbert Chidsey; 1 Neumann Way, Cincinnati, OH 45215 (US). ANTOLINO, Nicholas Edward; 1 Research Circle, Niskayuna, NY 12309 (US). (74) Agent: OVERBECK, Brian P. et al.; General Electric Company, Global Patent Operation, 901 Main Avenue, 3rd Floor, Norwalk, CT 06851 (US). (81) Designated States (unless otherwise indicated, for every kind of national protection available): 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, (54) Title: SYSTEM AND METHOD FOR PERFORMING AN IN SITU REPAIR OF AN INTERNAL COMPONENT OF A GAS TURBINE ENGINE (57) : In one aspect, a method for performing in situ repairs of internal components of a gas turbine engine (10) may generally include inserting a repair tool (102) within an interior of the gas turbine engine such that a tip end (118) of the repair tool is positioned within the gas turbine engine and an exterior end (116, 120) is positioned outside the gas turbine engine. The method may also include positioning the tip end of the repair tool adjacent to a defect (106) of an internal component (104), wherein the defect defines a fi liable volume (108) along a portion of the internal component. In addition, the method may include intermixing two or more constituents of a repair agent (128) within the repair tool at a mixing location (113) defined within the gas turbine engine, and expelling the repair agent from the tip end such that the fillable volume is at least partially filled with the repair agent. [Continued on next page] WO 2017/218385 Al MIDEDIMOMOIDEIRMEM00110EMIOMMODEVOIMIE 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. (84) Designated States (unless otherwise indicated, for every kind of regional protection available): ARIPO (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW), Eurasian (AM, AZ, BY, KG, KZ, RU, TJ, TM), European (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), OAPI (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, KM, ML, MR, NE, SN, TD, TG). Declarations under Rule 4.17: as to applicant's entitlement to apply for and be granted a patent (Rule 4.17(H)) as to the applicant's entitlement to claim the priority of the earlier application (Rule 4.17(iii)) Published: — with international search report (Art. 21(3))