Patent application number | Description | Published |
20080270070 | Methods and systems for computing gear modifications - A method of computing gear modifications from a gear inspection chart is provided. The method includes extracting a gear profile from the gear inspection chart. The method also includes quantifying the gear profile. The method also includes determining a gear modification based on a quantified gear profile. The method also includes qualifying a gear based on the gear modification. | 10-30-2008 |
20100158349 | METHOD AND SYSTEM FOR ESTIMATING CONTACT PATTERNS - A gear inspection system and method for a gearbox, wherein an image acquisition unit is oriented proximate the gearbox with a field of view of a section of the gears. The image acquisition unit obtains images of a gear tooth and corresponding contact pattern. In one embodiment a processing unit transforms the images to a gear tooth model so that the gear tooth image and contact pattern image matches the model gear tooth. Metrics are computed for the contact pattern, and based on threshold values, a determination is made as to whether the gearbox is acceptable. | 06-24-2010 |
20110211940 | SYSTEM AND METHOD FOR INSPECTION OF STATOR VANES - Embodiments of the invention include an inspection system to inspect internal components of a compressor of a gas turbine engine. The inspection system includes an image recording assembly having one or more image recording devices, light sources, storage devices, and power supplies. The image recording assembly may be inserted into a compressor without removal of the compressor housing or disassembly of the compressor. The image recording assembly may be removably coupled to a rotary component of the compressor, e.g., a rotor blade, and used to record images of stationary components, e.g., stator vanes, of the compressor. The images may be inspected to identify wear and/or defects in the stationary components, e.g., stator vanes | 09-01-2011 |
20110267428 | SYSTEM AND METHOD FOR MAPPING A TWO-DIMENSIONAL IMAGE ONTO A THREE-DIMENSIONAL MODEL - In one embodiment, a system includes a turbine comprising multiple components in fluid communication with a working fluid. The system also includes an imaging system in optical communication with at least one component. The imaging system is configured to receive a two-dimensional image of the at least one component during operation of the turbine, and to map the two-dimensional image onto a three-dimensional model of the at least one component to establish a composite model. | 11-03-2011 |
20120026306 | Image Recording Assemblies and Coupling Mechanisms For Stator Vane Inspection - A system is disclosed that includes an image recording assembly for recording images of a stator vane of a compressor and a mechanism configured to magnetically couple the image recording assembly to a rotor blade of a compressor. Additional systems are provided that include image recording assemblies. Methods implementing the disclosed systems are also provided. | 02-02-2012 |
20120026323 | SYSTEM AND METHOD FOR MONITORING STRESS ON A WIND TURBINE BLADE - A method for monitoring stress on a wind turbine blade during loading is disclosed. The method includes capturing multiple images at respective locations of the blade. The method also includes measuring temperature at the respective locations based upon captured images. The method further includes calculating stress applied on the blade at the respective locations based upon the measured temperature. | 02-02-2012 |
20120029840 | SYSTEM AND METHOD FOR DETERMINING LIFETIME OF WIND TURBINE BLADE - A method for monitoring stress on a wind turbine blade during loading is disclosed. The method includes capturing multiple images at respective locations of the blade. The method also includes measuring temperature at the respective locations based upon captured images. The method further includes calculating stress applied on the blade at the respective locations based upon the measured temperature. The method also includes calculating stress applied on the blade at the respective locations based upon the measured temperature. The method further includes comparing the calculated stress with respective theoretical stress in a finite element model to predict lifetime of the blade. The method also includes alerting an operator in event that the calculated stress at one or more of the respective locations is above a pre-determined limit. | 02-02-2012 |
20120194667 | TURBINE ENGINE THERMAL IMAGING SYSTEM - In one embodiment, a system includes an imaging system configured to capture a first image of a rotating component within an interior of a turbine using a first integration time, to capture a second image of the rotating component within the interior of the turbine using a second integration time, different than the first integration time, and to subtract the first image from the second image to obtain a differential image. | 08-02-2012 |
20140198946 | METHOD SYSTEM AND COMPUTER PRODUCT FOR NON-DESTRUCTIVE OBJECT ANALYSIS - Aspects of the invention provide a solution for analyzing an object, such as a part of a turbo machine. A planar surface is generated using a curved reformat function based on a surface of a three-dimensional (3D) image of an object. A peel of the 3D image that is adjacent to the surface is determined. Based on the peel, a second planar surface is generated. These two, and/or other similarly generated planar surfaces can be analyzed to determine characteristics of the original object. | 07-17-2014 |