Optimization of axial volumetric drive aviation pump

Annotation This article discusses a volumetric drive aircraft axial pump and solves the problem of its optimization by the Sobol method. The optimization criteria were the radial dimension and the power expended. In this case, the non-uniformity of the pump operation over time and the variable value...

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Bibliographic Details
Published in:IOP conference series. Materials Science and Engineering 2019-08, Vol.589 (1), p.12004
Main Authors: Protopopov, A, Mukhlaeva, A, Melnichuk, E
Format: Article
Language:English
Subjects:
Axial flow pumps
Nonuniformity
Optimization
Parameters
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Summary:Annotation This article discusses a volumetric drive aircraft axial pump and solves the problem of its optimization by the Sobol method. The optimization criteria were the radial dimension and the power expended. In this case, the non-uniformity of the pump operation over time and the variable value of the pressure consumed by the network were taken into account. The last two parameters act as constructive variable parameters. As a result of the work, we obtained a compromise curve. The radial dimension is the power expended.
ISSN:1757-8981
1757-899X
DOI:10.1088/1757-899X/589/1/012004