Thermodynamic Features of Aircraft Diagonal Gas Turbines

E. N. Bogomolov; P. V. Kashcheeva

首页> 外文期刊>Russian Aeronautics >Thermodynamic Features of Aircraft Diagonal Gas Turbines

【24h】

Thermodynamic Features of Aircraft Diagonal Gas Turbines

机译：飞机对角燃气轮机的热力学特征

获取原文

获取原文并翻译 | 示例

掌桥外文数据库（机构版） >>

开具论文收录证明 >>

文献代查 >>

页面导航

摘要
著录项
相似文献
相关主题

摘要

An effect of the Coriolis forces on the process of gas expansion in the turbine stage is considered. Expressions for efficiency with regard for the radial flow passage are derived. The calculation results and statistical data on the geometric parameters of diagonal stages are presented.

机译：考虑了科里奥利力对涡轮级中气体膨胀过程的影响。得出关于径向流道的效率的表达式。给出了对角位移台几何参数的计算结果和统计数据。

著录项

来源
《Russian Aeronautics》 |2009年第2期|共5页
作者
E. N. Bogomolov; P. V. Kashcheeva;
展开▼
作者单位

展开▼
收录信息
原文格式 PDF
正文语种 eng
中图分类航空;
关键词
Coriolis acceleration; Enthalpy; Entropy; Turbine; Work; Efficiency;

机译：科里奥利加速焓熵涡轮功效率;

相似文献

外文文献
中文文献
专利

1. Thermodynamic Features of Aircraft Diagonal Gas Turbines [J] . E. N. Bogomolov, P. V. Kashcheeva Russian Aeronautics . 2009,第2期

机译：飞机对角燃气轮机的热力学特征
2. Research and development activities in aircraft gas turbine at the gas Gas Turbine Research Establishment [J] . Prasad Arun Current science . 1990,第08期

机译：燃气轮机研究机构在飞机燃气轮机上的研发活动
3. Aero-thermodynamic and chemical process interactions in an axial high-pressure turbine of aircraft engines [J] . Trung Hieu Nguyen, Phuong Nguyen-Tri, Vancassel Xavier, International journal of engine research . 2019,第6期

机译：航空发动机轴向高压涡轮机的航空热力学和化学工艺相互作用
4. Thermodynamic Analysis of Solid Oxide Fuel Cell Gas Turbine Hybrid System for Aircraft Power Generation [C] . Tushar Choudhary, Mithilesh Sahu, Shreya KRISHNA SAE AeroTech Congress and Exhibition . 2017

机译：用于飞机发电的固体氧化物燃料电池燃气轮发系统的热力学分析
5. AN INVESTIGATION OF ALUMINA - CHROMIUM AND ALUMINA - CHROMIUM - MOLYBDENUM CERMETS FOR USE IN AIRCRAFT GAS TURBINES. [D] . SHEVLIN, THOMAS SMITHBERGER. 1954

机译：用于飞机燃气涡轮的铝-铬和铝-铬-钼金属陶瓷的研究。
6. The NMR Structures of (rGCUGAGGCU)2 and (rGCGGAUGCU)2: Probing the Structural Features that Shape the Thermodynamic Stability of GA Pairs [O] . Blanton S. Tolbert, Scott D. Kennedy, Susan J. Schroeder, -1

机译：（rGCUGAGGCU）2和（rGCGGAUGCU）2的NMR结构：探索塑造GA对的热力学稳定性的结构特征
7. Closure to “Discussions of ‘Endurance of Aircraft Gas Turbine Mainshaft Ball Bearings-Analysis Using Improved Fatigue Life Theory: Part 1—Application to a Long-Life Bearing’ and ‘Endurance of Aircraft Gas Turbine Mainshaft Ball Bearings-Analysis Using Improved Fatigue Life Theory: Part 2—Application to a Bearing Operating Under Difficult Lubrication Conditions’” (1990, ASME J. Tribol., 112, pp. 312–314) [O] . T. Harris, E. Ioannides, M. Ragen, 1990

机译：用改善的疲劳寿命理论关闭“讨论”飞机燃气轮机主轴球轴承 - 分析：第1部分 - 应用于长寿命的应用“飞机燃气轮机主轴球轴承的耐力 - 利用改进的疲劳寿命理论分析：第2部分 - 应用于困难润滑条件下的轴承'“（1990，Asme J. Trick。，112，PP。312-314）
8. An Introduction to Thermodynamic Performance Analysis of Aircraft Gas Turbine Engine Cycles Using the Numerical Propulsion System Simulation Code [R] . Jones, Scott M. 2007

机译：用数值推进系统仿真程序对飞机燃气轮机发动机循环热力性能分析的介绍

Thermodynamic Features of Aircraft Diagonal Gas Turbines

摘要

著录项

相似文献

相关主题

期刊订阅