B23P 9/04

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Patent/Pub #TitleFiling DateIssue/Publication DatePatent Owner
9885240 Repair article of a gas turbine engineAug 22, 13Feb 06, 18UNITED TECHNOLOGIES CORPORATION
9789582 Method and compression apparatus for introducing residual compression into a component having a regular or an irregular shaped surfaceMar 15, 13Oct 17, 17SURFACE TECHNOLOGY HOLDINGS, LTD.
9739695 Water jet peening compressive residual stress test method, test device, and test facilityFeb 10, 14Aug 22, 17MITSUBISHI HEAVY INDUSTRIES, LTD.
9573184 Deep rolling tool for processing blade rootDec 11, 14Feb 21, 17UNITED TECHNOLOGIES CORPORATION
9533371 Apparatus and method for on line surface enhancement of a workpieceJan 17, 12Jan 03, 17UNITED TECHNOLOGIES CORPORATION
9517537 Method for reshaping a turbomachine blade that has at least one zone that has become deformed using peeningDec 05, 12Dec 13, 16SNECMA
9200341 Systems and methods of cavitation peening a workpieceJul 18, 14Dec 01, 15THE BOEING COMPANY
8906181 Fan blade finishingJun 30, 11Dec 09, 14UNITED TECHNOLOGIES CORPORATION
8834126 Fan blade protection systemJun 30, 11Sep 16, 14UNITED TECHNOLOGIES CORPORATION
5443201 Method and device for repairing a defective zone of the wall of a metal part and in particular of a tubular partNov 29, 93Aug 22, 95Framatome
4666380 Scroll type fluid machine with prevention of stress concentrationJun 14, 85May 19, 87Mitsubishi Jukogyo Kabushiki Kaisha
4599879 Conveyor system for a shot peening machineAug 26, 85Jul 15, 86ROCKWELL INTERNATIONAL SUSPENSION SYSTEMS COMPANY