Design with the Big D¶
Gas Turbine Engines (GTEs)
- Turbojet
- 燃烧室
- Turboprop
- 加速度比 turbojet 小
- Turbofan
- 长距离飞行
- 大部分推力来自 bypass air
- 为了使压缩机工作,还有部分空气
2000 \(^\circ\)C
Structural Integrity of GTEs¶
Constituents of GTEs
Blade attachment
- Compressor Disc
- Dove Tail
- Fatigue
- Turbine Disc
- Fir-tree rim
- Creep + Corrosion
Two alternative failures:
- Bursting of a disc
- Blade shedding
Contact stress between blade and disc (Dovetail region)
Blade shedding in Aviation GTEs¶
Rolls Royce 测试:使用爆炸物把叶片炸掉,发动机还能支撑十几秒
Bird Strikes¶
Bird strikes represents 90% of FOD (Foreign Object Damage).
Aerial Refueling¶
Hose instability
explosive decompression:类似于扎破气球,应力瞬间释放。解决方法:在气球上粘上一段胶带,应力传递到胶带上 \(\implies\) Fuselage 的壳层有两层

