原文传递
Statistics on Aircraft Gas Turbine Engine Rotor Failures That Occurred in U.S Commercial Aviation During 1988.
| 题名： | Statistics on Aircraft Gas Turbine Engine Rotor Failures That Occurred in U.S Commercial Aviation During 1988. |
| 作者： | Chapdelaine, E. R.;Fenton, B. C.;Delucia, R. A.; |
| 关键词： | FAILURE, GAS TURBINES, AIRCRAFT ENGINES, AIR, AIR TRANSPORTATION, AIRCRAFT, BENEFITS, BLADES, COMMERCIAL AVIATION, COSTS, DISKS, ENGINES, FLIGHT, FRAGMENTS, HAZARDS, ROTORS, SAFETY, STANDARDS, TAKEOFF, TRANSPORTATION, TURBINES. |
| 摘要： | This report presents statistical information relating to gas turbine engine rotor failures which occurred during 1988 in U.S. commercial aviation service use. Four hundred and thirteen failures occurred in 1988. Rotor fragments were generated in 175 of the failures, and of these 14 were uncontained. The predominant failure involved blade fragments, 95 percent of which were contained. Five disk failures occurred and all were uncontained. Forty-two percent of the 413 failures occurred during the takeoff and climb stages of flight. This service data analysis is prepared on a calendar year basis and published yearly. The data are useful in support of flight safety analyses, proposed regulatory actions, certification standards, and cost benefit analyses. Air Transportation, Aircraft Hazards, Aircraft Safety, Gas Turbine Engine Rotor Failures, Containment. |
| 总页数： | 30 |
| 报告类型： | 科技报告 |
相关文献
- Rotor fragment protection program: Statistics on aircraft gas turbine engine rotor failures that occurred in US commercial aviation during 1979
- Hybrid Vehicle Turbine Engine Technology Support (HVTE-TS) ceramic design manual
- Cold-air performance of compressor-drive turbine of department of energy upgraded automobile gas turbine engine. 3: Performance of redesigned turbine
- Advanced Gas Turbine (AGT) Technology Project
- Advanced Turbine Technology Applications Project (ATTAP) Hybrid Vehicle Turbine Engine Technology Support Project (HVTE-TS)
- Cold-air performance of a 15.41-cm-tip-diameter axial-flow power turbine with variable-area stator designed for a 75-kW automotive gas turbine engine
检索历史
应用推荐
