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Autor/inn/enFalaleev, Sergei V.; Melentjev, Vladimir S.; Gvozdev, Alexander S.
TitelMethodology of Computer-Aided Design of Variable Guide Vanes of Aircraft Engines
QuelleIn: International Journal of Environmental and Science Education, 11 (2016) 10, S.3847-3860 (14 Seiten)
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Spracheenglisch
Dokumenttypgedruckt; online; Zeitschriftenaufsatz
ISSN1306-3065
SchlagwörterComputer Assisted Design; Aviation Technology; Engines; Models
AbstractThe paper presents a methodology which helps to avoid a great amount of costly experimental research. This methodology includes thermo-gas dynamic design of an engine and its mounts, the profiling of compressor flow path and cascade design of guide vanes. Employing a method elaborated by Howell, we provide a theoretical solution to the task of assessing the influence of the VGV blades' angle of rotation on the characteristic of a compressor. The finite element model of a VGV blade helps to solve some problems of strength and tune-out of resonance in the domain of a compressor's operating frequencies as well as the problem of determining the position of the pressure center and the location of a blade's pivotal point. Cinematic and dynamic analysis of the control linkage of VGVs is carried out in a MSC.ADAMS package. The investigation is based on geometric 2D and 3D models, gas-dynamic and strength analysis taking into account geometrical nonlinearity and based on the finite element method. The study is also based on the dynamic analysis according to the Euler-Lagrange equation, which describes the behavior of mechanical systems comprised of markers and the Craig-Bampton method implying the theory of superposition of vibrational modes. (As Provided).
AnmerkungenLOOK Academic Publishers. Knobbelzwaansingel 211 Den Haag 2496LN, Netherlands. Tel: 31-20-217-0912; e-mail: editor@lookacademy.nl; Web site: http://www.ijese.net
Erfasst vonERIC (Education Resources Information Center), Washington, DC
Update2020/1/01
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