发明名称 SYSTEM AND METHOD FOR ENGINE INSPECTION
摘要 An optical imaging and processing system includes an optical connection and an optical element disposed at a first end of the optical connection. The first end of the optical connection is configured to extend into a turbine component interior such that the optical element is disposed within the turbine component interior. The system also includes a photodiode array disposed at a second end of the optical connection, where the optical element is configured to transmit a video stream of the turbine component interior to the photodiode array as the optical element is moved within the turbine component interior between multiple vantage points. The system also includes a processor coupled to the photodiode array, wherein the processor is configured to process the video stream to generate a three-dimensional model of at least a portion of the turbine component interior without utilizing a previously defined three-dimensional model input of the turbine component interior.
申请公布号 US2016178532(A1) 申请公布日期 2016.06.23
申请号 US201414577255 申请日期 2014.12.19
申请人 GENERAL ELECTRIC COMPANY 发明人 Lim Ser Nam;Pawlowski Joseph Vincent;Guan Li;Agarwal Yogesh;Pandey Binod;Dhanvantri Srivatsa
分类号 G01N21/88;G01N21/954 主分类号 G01N21/88
代理机构 代理人
主权项 1. An optical imaging and processing system, comprising: an optical connection and an optical element disposed at a first end of the optical connection, wherein the first end of the optical connection is configured to extend into a turbine component interior such that the optical element is disposed within the turbine component interior; a photodiode array disposed at a second end of the optical connection, wherein the optical element is configured to transmit a video stream of the turbine component interior to the photodiode array as the optical element is moved within the turbine component interior between multiple vantage points; a processor coupled to the photodiode array, wherein the processor is configured to process the video stream to generate a three-dimensional model of at least a portion of the turbine component interior without utilizing a previously defined three-dimensional model input of the turbine component interior.
地址 SCHENECTADY NY US