| contributor author | J. P. Van Buijtenen | |
| contributor author | W. M. Farrell | |
| date accessioned | 2017-05-08T23:13:12Z | |
| date available | 2017-05-08T23:13:12Z | |
| date copyright | July, 1982 | |
| date issued | 1982 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26776#707_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/95776 | |
| description abstract | This paper describes the mechanical design features on TF-10 gas turbine. The TF-10 gas turbine features an intercooled centrifugal compressor and an annular combustor. A regenerator is added as a standard item. The ISO rating is 7.5 MW (10,000 hp) with a rotor inlet temperature (RIT) of 1116°C (2042°F) and a thermal efficiency of approximately 44 percent. Description of the combustion, rotors, stators, bearings, and shafting is presented. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Mechanical Design of a High-Efficiency 7.5-MW (10,000-hp) Gas Turbine | |
| type | Journal Paper | |
| journal volume | 104 | |
| journal issue | 3 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3227335 | |
| journal fristpage | 707 | |
| journal lastpage | 714 | |
| identifier eissn | 0742-4795 | |
| keywords | Design engineering | |
| keywords | Gas turbines | |
| keywords | Rotors | |
| keywords | Stators | |
| keywords | Temperature | |
| keywords | Combustion | |
| keywords | Compressors | |
| keywords | Combustion chambers AND Bearings | |
| tree | Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 003 | |
| contenttype | Fulltext | |
