2) aero turbine engine
航空涡轮发动机
1.
The convergence problems of solving the nonlinear equations of aero turbine engines were study in detail,the common non-convergence cases were given and the mechanism was analyzed,based on Newton method,an advanced solutions for overcoming the common non-convergence problems was presented:variable step Newton method(VSN).
详细分析了航空涡轮发动机部件共同工作的非线性方程组的求解收敛性问题,并对计算中常见的迭代不收敛问题的机理进行了研究总结。
3) aeroengine blade
航空发动机叶片
1.
Manufacturability evaluation method for aeroengine blade
面向航空发动机叶片的可制造性评价方法
4) turbofan jet
航空涡轮风扇发动机
5) turbine shaft aeroengine
航空涡轮轴发动机
1.
With the development of science and technology, the performance of turbine shaft aeroengine is constantly improved, its power turbine rotor is developing towards high speed and large length-to-diameter ratio, specified operating speed is generally over bending critical speed, structure is becoming more and more complex.
随着科学技术的发展,航空涡轮轴发动机的性能不断提高,其动力涡轮转子正朝着高转速、大长径比的方向发展,工作转速往往高于弯曲临界转速,结构日益复杂。
补充资料：航空发动机推重比(见航空发动机推力)
航空发动机推重比(见航空发动机推力)
thrust to weight ratio of aeroengine
hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条