About: Design Optimization and Technology of Carbon Composite Axial Flow Fan Rotor Blade of Light Aircraft Propulsion System

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About: Design Optimization and Technology of Carbon Composite Axial Flow Fan Rotor Blade of Light Aircraft Propulsion System Goto Sponge NotDistinct Permalink

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rdf:type	skos:Concept http://linked.opendata.cz/ontology/domain/vavai/Vysledek
Description	The paper is focused on design of carbon composite fan rotor blade. The fan is a part of propulsion system for small aircrafts, which is composed from four-stroke four-piston motorcycle engine (108 kW @ 7605 rpm) and fan connected with the engine by composite driveshaft. Aerodynamic and strength design was done to obtain proper shape and reinforcement layup. In the work technological design is mainly examined aimed to find the most suitable structure with respect to required mechanical properties of the whole system and its dynamic behavior. The SP Systems SPRINT technology is analyzed with the aim to apply it for manufacturing of the blade as an alternative to RTM, which is usualy used for different parts like blades. The paper is focused on design of carbon composite fan rotor blade. The fan is a part of propulsion system for small aircrafts, which is composed from four-stroke four-piston motorcycle engine (108 kW @ 7605 rpm) and fan connected with the engine by composite driveshaft. Aerodynamic and strength design was done to obtain proper shape and reinforcement layup. In the work technological design is mainly examined aimed to find the most suitable structure with respect to required mechanical properties of the whole system and its dynamic behavior. The SP Systems SPRINT technology is analyzed with the aim to apply it for manufacturing of the blade as an alternative to RTM, which is usualy used for different parts like blades. (en)
Title	Design Optimization and Technology of Carbon Composite Axial Flow Fan Rotor Blade of Light Aircraft Propulsion System Design Optimization and Technology of Carbon Composite Axial Flow Fan Rotor Blade of Light Aircraft Propulsion System (en)
skos:prefLabel	Design Optimization and Technology of Carbon Composite Axial Flow Fan Rotor Blade of Light Aircraft Propulsion System Design Optimization and Technology of Carbon Composite Axial Flow Fan Rotor Blade of Light Aircraft Propulsion System (en)
skos:notation	RIV/68407700:21220/06:00128678!RIV11-MSM-21220___
http://linked.open...avai/riv/aktivita	P S
http://linked.open...avai/riv/aktivity	P(1M0501), P(LN00B051), S
http://linked.open...vai/riv/dodaniDat	2011
http://linked.open...aciTvurceVysledku	Poul, Robin 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 strojní
http://linked.open...dnocenehoVysledku	470974
http://linked.open...ai/riv/idVysledku	RIV/68407700:21220/06:00128678
http://linked.open...riv/jazykVysledku	eng - angličtina
http://linked.open.../riv/klicovaSlova	Axial-flow fan; Composite rotor blade; Ducted fan; Ultralight propulsor (en)
http://linked.open.../riv/klicoveSlovo	Composite rotor blade Ducted fan Axial-flow fan Ultralight propulsor
http://linked.open...ontrolniKodProRIV	[D8739DD3BBB2]
http://linked.open...v/mistoKonaniAkce	Hamburg
http://linked.open...i/riv/mistoVydani	Edinburgh
http://linked.open...i/riv/nazevZdroje	Proceedings, ICAS 2006, Hamburg
http://linked.open...in/vavai/riv/obor	JI
http://linked.open...ichTvurcuVysledku	2 (xsd:int)
http://linked.open...cetTvurcuVysledku	2 (xsd:int)
http://linked.open...vavai/riv/projekt	Aerospace research centre (ARC) Aerospace Research Centre
http://linked.open...UplatneniVysledku	2006
http://linked.open...iv/tvurceVysledku	Hanus, Daniel Poul, Robin
http://linked.open...vavai/riv/typAkce	WRD - Světová
http://linked.open.../riv/zahajeniAkce	2006-09-03 (xsd:date)
number of pages	6 (xsd:int)
http://purl.org/ne...btex#hasPublisher	Optimage
https://schema.org/isbn	0-9533991-7-6
http://localhost/t...ganizacniJednotka	21220

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