Development of a method for geometric modeling of centrifugal compressor impellers

نویسندگان

چکیده

The practice of designing centrifugal compressors in which impellers are the main components shows that there reserves for their further improvement. One consists improving flow conditions compressed medium compressor setting and, above all, impeller. A method geometric modeling settings was proposed involves construction meridional boundaries and blade profile on an involute cylindrical surface outer radius is represented by ruled surfaces. boundary impeller described a curve natural parameterization using cubic dependence curvature arc length. Dependences length determined process based set source data. problem solved minimizing deviations intermediate curves from endpoint. inner obtained as envelope circles inscribed channel Radii taking into account areas channel. midline modeled presented with quadratic law distribution. computer code developed Fortran Power Station programming environment visualizes numerical results graphically display addition to digital information profile. Graphical were presented. They confirmed efficiency impellers. can be useful offices involved design

برای دانلود رایگان متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

investigating the feasibility of a proposed model for geometric design of deployable arch structures

deployable scissor type structures are composed of the so-called scissor-like elements (sles), which are connected to each other at an intermediate point through a pivotal connection and allow them to be folded into a compact bundle for storage or transport. several sles are connected to each other in order to form units with regular polygonal plan views. the sides and radii of the polygons are...

Assessing Liquid Droplet Erosion Potential in Centrifugal Compressor Impellers

This paper presents a method for estimating the potential for liquid droplet erosion in compression system components, such as the impeller of centrifugal compressors. The erosion model selected is used to calculate a threshold velocity that represents the limit for the onset of erosion damage. The parameters used in the model include the liquid phase density and viscosity, impeller geometry, s...

متن کامل

Manufacturing and Testing Experience with Direct Metal Laser Sintering for Closed Centrifugal Compressor Impellers

Direct Metal Laser Sintering (DMLS) is an additive manufacturing process that utilizes a high-powered laser to build up a metal part by selectively melting thin layers of metal powder. This process is attractive for the manufacturing of parts with complex geometry such as closed centrifugal compressor impellers. DMLS allows closed impellers to be made in a single piece and eliminates the shroud...

متن کامل

Impact of Geometric Scaling on Centrifugal Compressor Performance

Compressor performance for liquefied natural gas (LNG) main refrigeration units is very important due to the direct link between compressor efficiency and LNG production for a fixed amount of power. Dresser-Rand recently designed a series of new stages for the LNG market that provided improved efficiency and a wider range of operation. Industry practice is to rig test new stages prior to applic...

متن کامل

Centrifugal Compressor Surge, Modeling and Identification for Control

In this chapter a general introduction of centrifugal compression systems is presented. The unstable surge phenomenon in compressors is discussed, as well as possible means to avoid or suppress this instability. From an assessment of the current state of the art in control-oriented modeling and identification, the research objectives are formulated. 1.1 General introduction The general topic of...

متن کامل

ذخیره 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: Eastern-European Journal of Enterprise Technologies

سال: 2021

ISSN: ['1729-3774', '1729-4061']

DOI: https://doi.org/10.15587/1729-4061.2021.224924