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Statements

Subject Item
n2:RIV%2F68407700%3A21220%2F06%3A00128678%21RIV11-MSM-21220___
rdf:type
n13:Vysledek skos:Concept
dcterms: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.
dcterms: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
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
skos:notation
RIV/68407700:21220/06:00128678!RIV11-MSM-21220___
n3:aktivita
n10:S n10:P
n3:aktivity
P(1M0501), P(LN00B051), S
n3:dodaniDat
n21:2011
n3:domaciTvurceVysledku
n4:6730310 n4:5514495
n3:druhVysledku
n7:D
n3:duvernostUdaju
n19:S
n3:entitaPredkladatele
n18:predkladatel
n3:idSjednocenehoVysledku
470974
n3:idVysledku
RIV/68407700:21220/06:00128678
n3:jazykVysledku
n6:eng
n3:klicovaSlova
Axial-flow fan; Composite rotor blade; Ducted fan; Ultralight propulsor
n3:klicoveSlovo
n16:Axial-flow%20fan n16:Ultralight%20propulsor n16:Composite%20rotor%20blade n16:Ducted%20fan
n3:kontrolniKodProRIV
[D8739DD3BBB2]
n3:mistoKonaniAkce
Hamburg
n3:mistoVydani
Edinburgh
n3:nazevZdroje
Proceedings, ICAS 2006, Hamburg
n3:obor
n9:JI
n3:pocetDomacichTvurcuVysledku
2
n3:pocetTvurcuVysledku
2
n3:projekt
n15:LN00B051 n15:1M0501
n3:rokUplatneniVysledku
n21:2006
n3:tvurceVysledku
Poul, Robin Hanus, Daniel
n3:typAkce
n14:WRD
n3:zahajeniAkce
2006-09-03+02:00
s:numberOfPages
6
n12:hasPublisher
Optimage
n20:isbn
0-9533991-7-6
n11:organizacniJednotka
21220