| 1. | The manufacture of the heavy duty gh36 alloy turbine plate forging
36合金大型涡轮盘锻件的制造 |
| 2. | Turbine disk is one of the key parts of aero - engine
涡轮盘是航空发动机具有关键特性的核心部件之一。 |
| 3. | This cavity is composed of an upstream disc , a downstream disc , a hub and a shroud
该旋转盘腔由上、下游涡轮盘和内、外围屏组成。 |
| 4. | Two - row disk
双排涡轮盘 |
| 5. | Preliminary investigation of fatigue life probability distribution for two domestic turbine disc materials
两种国产涡轮盘材料疲劳寿命概率分布规律初探 |
| 6. | A low - cycle fatigue life model for simplified turbine disk simulation specimens of powder metallurgy superalloys
粉末冶金涡轮盘简单模拟件低周疲劳寿命研究 |
| 7. | Failure state random function method for digital simulation of turbine disc crack initiation and propagation
涡轮盘裂纹萌生扩展数字仿真的故障状态随机函数法 |
| 8. | So it is essential to study the effect of inclusion on the strength and life of pm superalloy turbine disks
因此研究夹杂对粉末高温合金涡轮盘强度与寿命的影响十分必要。 |
| 9. | For a turbine disk , the growth life of crack is the shortest when the inclusions are at the edge of the center hole
对某发动机涡轮盘而言，中心孔边存在夹杂时，裂纹扩展寿命最短。 |
| 10. | The main work of this paper is the heat transfer experiment in rotating cavity of an advanced aero - engine of rrd company
本文工作围绕rrd公司某型先进发动机高压涡轮盘腔内换热实验进行。 |
