Structural Analysis of Jet Engine Rotor
نویسندگان
چکیده
منابع مشابه
Non-linear Observer of Single-rotor Single-flow Jet Turbine Engine during Operation
The paper presents a type of observer based on reduced to minimum set of engine parameters measured directly: turbine-compressor rotational speed, engine inlet air pressure and temperature and atmospheric pressure. Results of application in analysis of data recorded during engine operation in non-stationary states of SO-3 engine (powering TS-11 Iskra aircraft) are presented. Possibilities of th...
متن کاملDynamical Analysis and Control of Jet Engine Systems
In the recent years, the main obstacles for raising the operating efficiency are instabilities of the compressor system. The related dynamics and control schemes then cause lots of interests among engineers and researchers. Two main phenomena, which cause the instabilities, are the “surge” and the “stall” behaviors of the compressed gas. The so-called “surge” is characterized as a one-dimension...
متن کاملComparison of Rotor Structural Loads Calculated Using Comprehensive Analysis
Blade flap and chord bending and torsion moments are investigated for six rotors operating at transition and high speed: H-34 in flight and wind tunnel, SA 330 (research Puma), SA 349/2, UH-60A full-scale, and BO 105 model (HART-I). The measured data from flight and wind tunnel tests are compared with calculations obtained using the comprehensive analysis CAMRAD II. The calculations were made ...
متن کاملExperience in Rotor Balancing of Large Commercial Jet Engines
Experienceouerthepasttenyearsinvibration and cabin noise control of new airplane jemgine systems Is summarized. why the newer systems required more stigent control is discussed. he transitionfrom single plane balance methods, in cmnnwn use on older systems, to conventional 2.plane influence coefFcient @.C.J methods, and then to optimized 2-p&e LC. methods is described. Examples of residual unba...
متن کاملNovelty detection in jet engine vibration spectra
This paper presents a principled method for detecting “abnormal” content in vibration spectra obtained from rotating machinery. We illustrate the use of the method in detecting abnormality in jet engine vibration spectra corresponding to unforeseen engine events. We take a novelty detection approach, in which a model of normality is constructed from the typically large numbers of examples of “n...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series A
سال: 1982
ISSN: 0387-5008,1884-8338
DOI: 10.1299/kikaia.48.1269