About: Ultra and Very Light Ducted Fan Propulsion System Complex Design Optimization     Goto   Sponge   Distinct   Permalink

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Description
  • Není k dispozici (cs)
  • The propulsion system is being developed for the application to the full composite ultra-light two-seated airplane with maximum take off weight of 450 kg. The propulsion systém consists of the piston engine of the power output of 150 HP at 10500 rpm, the composite fan driven by the lightweight aluminium alloy or composite shaft, the composite inlet channel and the composite jet nozzle with a by-pass cooling duct containing the engine radiators. The system is optimized to meet all airworthiness requirements for the VLA category with a minimum weight and maximum propulsive efficiency.
  • The propulsion system is being developed for the application to the full composite ultra-light two-seated airplane with maximum take off weight of 450 kg. The propulsion systém consists of the piston engine of the power output of 150 HP at 10500 rpm, the composite fan driven by the lightweight aluminium alloy or composite shaft, the composite inlet channel and the composite jet nozzle with a by-pass cooling duct containing the engine radiators. The system is optimized to meet all airworthiness requirements for the VLA category with a minimum weight and maximum propulsive efficiency. (en)
Title
  • Není k dispozici (cs)
  • Ultra and Very Light Ducted Fan Propulsion System Complex Design Optimization
  • Ultra and Very Light Ducted Fan Propulsion System Complex Design Optimization (en)
skos:prefLabel
  • Není k dispozici (cs)
  • Ultra and Very Light Ducted Fan Propulsion System Complex Design Optimization
  • Ultra and Very Light Ducted Fan Propulsion System Complex Design Optimization (en)
skos:notation
  • RIV/68407700:21220/04:02102572!RIV/2005/MSM/212205/N
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  • P(LN00B051)
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  • 591306
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  • RIV/68407700:21220/04:02102572
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  • Aerodynamic; Aircraft; Ducted Fan; Power Unit (en)
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  • [1B7AFEE5B91E]
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  • Edinburgh
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  • neuvedeno
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  • Hanus, Daniel
  • Ritschl, Erik
  • Theiner, Robert
https://schema.org/isbn
  • 0-9533991-6-8
http://localhost/t...ganizacniJednotka
  • 21220
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