| contributor author | A. G. Sheard | |
| contributor author | B. Killeen | |
| date accessioned | 2017-05-08T23:47:14Z | |
| date available | 2017-05-08T23:47:14Z | |
| date copyright | April, 1995 | |
| date issued | 1995 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26738#326_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/115317 | |
| description abstract | It is difficult to make a reliable measurement of running clearance in the hostile environment over the blading of a modern gas turbine. When engine manufacturers require the measurement to be made over every blade during live engine tests, system reliability, ruggedness, and ease of operation are of primary importance. This paper describes a tip clearance measurement system that can measure clearance over every blade around a rotor. The measurement system concept is presented, and the system design described in detail. Commissioning of the measurement system on a compressor test facility, and the results obtained are discussed. An analysis of system performance during the commissioning trials concludes the paper. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A Blade-by-Blade Tip Clearance Measurement System for Gas Turbine Applications | |
| type | Journal Paper | |
| journal volume | 117 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.2814098 | |
| journal fristpage | 326 | |
| journal lastpage | 331 | |
| identifier eissn | 0742-4795 | |
| keywords | Clearances (Engineering) | |
| keywords | Gas turbines | |
| keywords | Blades | |
| keywords | Measurement systems | |
| keywords | Engines | |
| keywords | Compressors | |
| keywords | Reliability | |
| keywords | Design | |
| keywords | Test facilities | |
| keywords | Rotors AND Systems analysis | |
| tree | Journal of Engineering for Gas Turbines and Power:;1995:;volume( 117 ):;issue: 002 | |
| contenttype | Fulltext | |