About: New Design Concept of Centrifugal Compressor Impellers of Turbojet Engines

Facets (new session)
Description
Metadata
Settings
- owl:sameAs
- Inference Rule:

About: New Design Concept of Centrifugal Compressor Impellers of Turbojet Engines Goto Sponge NotDistinct Permalink

An Entity of Type : http://linked.opendata.cz/ontology/domain/vavai/Vysledek, within Data Space : linked.opendata.cz associated with source document(s)

Attributes	Values
rdf:type	skos:Concept http://linked.opendata.cz/ontology/domain/vavai/Vysledek
Description	Koncept nového designu rotoru odstředivého kompresoru u proudových motorů (cs) In the paper a new innovative design of the centrifugal compressor impeller blades with the aim to improve the centrifugal compressor stage performance characteristics, namely its efficiency and the range of stable work is described. The new design concept consists in the division of the of the impeller blades into two parts. First part of the rotor blades is formed by highly aerodynamic loaded axial flow cascade. The second part is formed by axial/radial cascade with double blades then the first part. The new design has been applied to the advanced centrifugal compressor stage of Walter Aero Engine Company. Performance characteristics of both stages have been calculated using Fluent code at design speed of the rotor. Results obtained by numerical experiment and based on the relative comparison of the two designs show considerable improvement of performance characteristics of the new centrifugal compressor stage design. In the paper a new innovative design of the centrifugal compressor impeller blades with the aim to improve the centrifugal compressor stage performance characteristics, namely its efficiency and the range of stable work is described. The new design concept consists in the division of the of the impeller blades into two parts. First part of the rotor blades is formed by highly aerodynamic loaded axial flow cascade. The second part is formed by axial/radial cascade with double blades then the first part. The new design has been applied to the advanced centrifugal compressor stage of Walter Aero Engine Company. Performance characteristics of both stages have been calculated using Fluent code at design speed of the rotor. Results obtained by numerical experiment and based on the relative comparison of the two designs show considerable improvement of performance characteristics of the new centrifugal compressor stage design. (en)
Title	New Design Concept of Centrifugal Compressor Impellers of Turbojet Engines Koncept nového designu rotoru odstředivého kompresoru u proudových motorů (cs) New Design Concept of Centrifugal Compressor Impellers of Turbojet Engines (en)
skos:prefLabel	New Design Concept of Centrifugal Compressor Impellers of Turbojet Engines Koncept nového designu rotoru odstředivého kompresoru u proudových motorů (cs) New Design Concept of Centrifugal Compressor Impellers of Turbojet Engines (en)
skos:notation	RIV/68407700:21260/08:06148892!RIV09-MSM-21260___
http://linked.open...avai/riv/aktivita	P S
http://linked.open...avai/riv/aktivity	P(GA101/06/1440), S
http://linked.open...vai/riv/dodaniDat	2009
http://linked.open...aciTvurceVysledku	Hanus, Daniel
http://linked.open.../riv/druhVysledku	D - Článek ve sborníku
http://linked.open...iv/duvernostUdaju	S - Úplné a pravdivé údaje nepodléhající ochraně podle zvláštních právních předpisů
http://linked.open...titaPredkladatele	České vysoké učení technické v Praze / Fakulta dopravní
http://linked.open...dnocenehoVysledku	382530
http://linked.open...ai/riv/idVysledku	RIV/68407700:21260/08:06148892
http://linked.open...riv/jazykVysledku	eng - angličtina
http://linked.open.../riv/klicovaSlova	CFD; Centrifugal compressor; internal aerodynamics; performance characteristics; tandem blade (en)
http://linked.open.../riv/klicoveSlovo	performance characteristics Centrifugal compressor CFD internal aerodynamics tandem blade
http://linked.open...ontrolniKodProRIV	[5BC5E71444EF]
http://linked.open...v/mistoKonaniAkce	Praha
http://linked.open...i/riv/mistoVydani	Praha
http://linked.open...i/riv/nazevZdroje	Nové trendy v civilním letectví
http://linked.open...in/vavai/riv/obor	JU
http://linked.open...ichTvurcuVysledku	1 (xsd:int)
http://linked.open...cetTvurcuVysledku	1 (xsd:int)
http://linked.open...vavai/riv/projekt	Improvement of the IGCC using brown coal for obtaining maximum thermic efficiency and minimum CO2 emissions
http://linked.open...UplatneniVysledku	2008
http://linked.open...iv/tvurceVysledku	Hanus, Daniel
http://linked.open...vavai/riv/typAkce	EUR - Evropská
http://linked.open.../riv/zahajeniAkce	2008-09-25 (xsd:date)
number of pages	14 (xsd:int)
http://purl.org/ne...btex#hasPublisher	České vysoké učení technické v Praze. Fakulta dopravní
https://schema.org/isbn	978-80-7204-604-1
http://localhost/t...ganizacniJednotka	21260
is http://linked.open...avai/riv/vysledek of	New Design Concept of Centrifugal Compressor Impellers of Turbojet Engines New Design Concept of Centrifugal Compressor Impellers of Turbojet Engines New Design Concept of Centrifugal Compressor Impellers of Turbojet Engines New Design Concept of Centrifugal Compressor Impellers of Turbojet Engines

Faceted Search & Find service v1.16.116 as of Feb 22 2024

Alternative Linked Data Documents: ODE Content Formats:

RDF

ODATA

Microdata

About

OpenLink Virtuoso version 07.20.3239 as of Feb 22 2024, on Linux (x86_64-pc-linux-gnu), Single-Server Edition (126 GB total memory, 82 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software