| contributor author | C. C. Chamis | |
| contributor author | R. F. Lark | |
| contributor author | J. H. Sinclair | |
| date accessioned | 2017-05-08T23:10:59Z | |
| date available | 2017-05-08T23:10:59Z | |
| date copyright | October, 1981 | |
| date issued | 1981 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26769#731_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/94476 | |
| description abstract | An investigation was conducted to determine the feasibility of superhybrid composite blades for meeting the mechanical design and impact resistance requirements of large fan blades for aircraft turbine engine applications. Two design concepts were evaluated: (1) leading edge spar (TiCom) and (2) center spar (TiCore), both with superhybrid composite shells. The investigation was both analytical and experimental. The results obtained show promise that superhybrid composites can be used to make light-weight, high-quality, large fan blades with good structural integrity. The blades tested successfully demonstrated their ability to meet steady-state operating conditions, overspeed, and small bird impact requirements. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Superhybrid Composite Blade Impact Studies | |
| type | Journal Paper | |
| journal volume | 103 | |
| journal issue | 4 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3230796 | |
| journal fristpage | 731 | |
| journal lastpage | 738 | |
| identifier eissn | 0742-4795 | |
| keywords | Composite materials | |
| keywords | Blades | |
| keywords | Spar platforms | |
| keywords | Steady state | |
| keywords | Shells | |
| keywords | Electrical resistance | |
| keywords | Design | |
| keywords | Design engineering | |
| keywords | Gas turbines | |
| keywords | Aircraft AND Weight (Mass) | |
| tree | Journal of Engineering for Gas Turbines and Power:;1981:;volume( 103 ):;issue: 004 | |
| contenttype | Fulltext | |
