疲劳
材料(或结构)因反复循环应力引起的裂纹逐渐扩展而失效的过程。循环应力通常远低于材料的屈服强度。
许多因素会影响疲劳过程。(见 Juvinall,第 193–369 页。)这些因素包括:
- 材料本身。
- 材料的加工历史。
- 应力的施加方式(轴向、弯曲、旋转弯曲等)。
- 应力水平(受几何形状影响)。
- 是否存在残余应力或静应力。
- 材料的缺口敏感性。
- 试验频率。
- 试验方向相对于材料晶粒方向的关系。
- 加工试样所用原材料的尺寸。
- 表面光洁度。
- 镀层。
- 环境(包括温度、湿度、腐蚀介质等)。
因此,在确定疲劳性能时必须谨慎。
疲劳是变幅杆和增幅杆最常见的失效模式。
另见 —
疲劳寿命(N)
疲劳极限
疲劳缺口系数(Kf)
疲劳缺口敏感度(q)
疲劳强度
疲劳试验
疲劳试验变幅杆
Gerber 抛物线
S‑N 曲线
S‑N 试验
Fatigue
A process where a material (or structure) fails because of progressive crack growth due to repeated cyclic stress. The cyclic stress is usually considerably below the material's yield strength.
Many factors affect the fatigue process. (See Juvinall, pp. 193 - 369.) These factors include:
- The material.
- The material's processing history.
- The method of stress application (axial, bending, rotating bending, etc.).
- The stress level (which is influenced by geometry).
- The presence of residual stresses or static stresses.
- The material's notch sensitivity.
- The test frequency.
- The test direction relative to the material's grain direction.
- The size of the raw stock from which the sample has been machined.
- The surface finish.
- Plating.
- The environment (including temperature, humidity, corrosives, etc.).
Thus, caution must be used when determining fatigue performance.
Fatigue is the most common failure mode for horns and boosters.
Also see —
Fatigue life (N)
Fatigue limit
Fatigue notch factor (Kf)
Fatigue notch sensitivity (q)
Fatigue strength
Fatigue test
Fatigue test horn
Gerber parabola
S‑N curve
S‑N test