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Article

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Title

Assessment of vibration isolation generated by the inertial forces of an aircraft combustion engine on a test bench

Authors

[ 1 ] Instytut Transportu, Wydział Inżynierii Lądowej i Transportu, Politechnika Poznańska | [ 2 ] Instytut Silników Spalinowych i Napędów, Wydział Inżynierii Lądowej i Transportu, Politechnika Poznańska | [ P ] employee

Scientific discipline (Law 2.0)

[2.7] Civil engineering, geodesy and transport

Year of publication

2024

Published in

Diagnostyka

Journal year: 2024 | Journal volume: online first/in press

Article type

scientific article

Publication language

english

Keywords
EN
  • order analysis
  • vibration isolation
  • empirical research
  • aircraft engine
  • susceptibility method
Abstract

EN The scientific issues that are the subject of this article are related to the assessment of the vibration damping efficiency of an aircraft engine installed on a test stand for the type of vibration isolator used. For this purpose, appropriate empirical tests were carried out on an aircraft internal combustion piston engine of the Rotax 912 type, under conditions of variable engine speed, for selected mounting locations of vibration transducers on the engine and its frame. The effectiveness of vibration isolation of vibrations generated by inertia forces was assessed, based on the proposed mathematical equations and the determination of the values of discrete impulse and energy measures describing them for accelerations, velocities and vibration displacements in various directions. Thanks to this, it became possible to perform a diagnostic assessment of the generation and propagation of vibrations and their isolation from the perspective of operational vibration loads on the object and its supporting structure, as well as in the context of the research reliability of the signal for a given type of damping of forces and moments of inertia.

Pages (from - to)

1 - 13

DOI

10.29354/diag/188673

URL

http://www.diagnostyka.net.pl/Assessment-of-vibration-isolation-generated-by-the-inertial-forces-of-an-aircraft,188673,0,2.html

License type

CC BY (attribution alone)

Open Access Mode

open journal

Open Access Text Version

final author's version

Date of Open Access to the publication

at the time of publication

Full text of article

Download file

Access level to full text

public

Ministry points / journal

40

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