Dynamic Model of Aircraft Passenger Seats for Vibration Comfort Evaluation and Control

Kód výsledku v IS VaVaI

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Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

Dynamic Model of Aircraft Passenger Seats for Vibration Comfort Evaluation and Control

Popis výsledku v původním jazyce

The paper deals with the development of the seat dynamical model for vibration comfort evaluation and control. The aircraft seats have been tested extensively by vibrations on the 6 DOF vibrating platform. The importance of the careful comfort control together with the flight mechanics control is namely stressed for the blended wing body (BWB) aircrafts. They have a very large fuselage, where the mechanical properties (accelerations, angular accelerations) varies considerably for different seat places.The model have been improved by adding of dynamical models of the aircraft passenger seats identified by the measure-ments on the 6 DOF vibrating platform. The experiments, their results and the identification of the dynamical seat model are described. The model is further modified by adding of the comfort evaluation norms represented by dynamical filters. The structure and identification of the seat model is briefly described and discussed.

Název v anglickém jazyce

Dynamic Model of Aircraft Passenger Seats for Vibration Comfort Evaluation and Control

Popis výsledku anglicky

The paper deals with the development of the seat dynamical model for vibration comfort evaluation and control. The aircraft seats have been tested extensively by vibrations on the 6 DOF vibrating platform. The importance of the careful comfort control together with the flight mechanics control is namely stressed for the blended wing body (BWB) aircrafts. They have a very large fuselage, where the mechanical properties (accelerations, angular accelerations) varies considerably for different seat places.The model have been improved by adding of dynamical models of the aircraft passenger seats identified by the measure-ments on the 6 DOF vibrating platform. The experiments, their results and the identification of the dynamical seat model are described. The model is further modified by adding of the comfort evaluation norms represented by dynamical filters. The structure and identification of the seat model is briefly described and discussed.

Druh

D - Stať ve sborníku

CEP obor

JU - Aeronautika, aerodynamika, letadla

OECD FORD obor

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Projekt

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Návaznosti

R - Projekt Ramcoveho programu EK

Rok uplatnění

2011

Kód důvěrnosti údajů

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

Název statě ve sborníku

Vibration Problems ICOVP 2011

ISBN

978-94-007-2069-5

ISSN

0930-8989

e-ISSN

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Počet stran výsledku

7

Strana od-do

217-223

Název nakladatele

Springer Science+Business Media

Místo vydání

Berlin

Místo konání akce

Praha

Datum konání akce

5. 9. 2011

Typ akce podle státní příslušnosti

EUR - Evropská akce

Kód UT WoS článku

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