Composite Axial Flow Propulsor of Small Aircraft

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F04%3A02102567" target="_blank" >RIV/68407700:21220/04:02102567 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Composite Axial Flow Propulsor of Small Aircraft

Original language description

Work is focused on many aspects of design of axial flow, one stage, ducted fan driven by four stroke, four cylinder reciprocating engine Yamaha with the power output of 110 kW. Airplane with this propulsion is expected to be of considerably low drag, because of location of fan inside the hull which will make the airplane aerodynamically smoother compared with classic airplanes with tractor propeller. Such solution minimizes turbulization (disturbance) of the flow around the aircraft so significant partof the airplane wetted surface is expected to work in laminar regime. This fan is of rotor - stator configuration. The need of low weight of fan is reason for choice of carbon/epoxy composite material for blades and driving shaft connecting engine with the fan.

Czech name

Není k dispozici

Czech description

Není k dispozici

Type

A - Audiovisual production

CEP classification

JI - Composite materials

OECD FORD branch

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Project

<a href="/en/project/LN00B051" target="_blank" >LN00B051: Aerospace research centre (ARC)</a><br>

Continuities

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year

2004

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

ISBN

80-86059-41-3

Place of publication

Praha

Publisher/client name

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Version

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Carrier ID

neuvedeno