<abstract xmlns="http://www.w3.org/1999/xhtml">

<p>Rescue patrol hovercrafts must meet the basic condition – high reliability of use in extreme conditions. The introduction to the work shows damage to the propulsion system and the fan tunnel structure resulting from a fatigue fracture of the attachment wound to the propulsion unit hull. In this paper, the author describes some ways of improving the engine frame structure. In the first phase of the exploitation crack testing of the hovercraft frame, the probable causes of damage were determined. The necessary output data for analysis of the load course were obtained from the operating documentation. The approximate number of variable load cycles acting on the frame truss rod was determined. Using the comparative testing methods, the service life of the frame was estimated. Probable resonance frequencies of the vibrating bars in the truss were determined. Vibration tests of the power transmission assemblies were carried out, which allowed to determine the amplitudes and frequencies of free vibrations. Finally, a modification of the frame shifting the resonant frequency range was proposed. In conclusions, changes to the design and a schedule of inspections were proposed. The newly designed engine frame should have an extended service life.</p>
</abstract>

Rescue patrol hovercrafts must meet the basic condition – high reliability of use in extreme conditions. The introduction to the work shows damage to the propulsion system and the fan tunnel structure resulting from a fatigue fracture of the attachment wound to the propulsion unit hull. In this paper, the author describes some ways of improving the engine frame structure. In the first phase of the exploitation crack testing of the hovercraft frame, the probable causes of damage were determined. The necessary output data for analysis of the load course were obtained from the operating documentation. The approximate number of variable load cycles acting on the frame truss rod was determined. Using the comparative testing methods, the service life of the frame was estimated. Probable resonance frequencies of the vibrating bars in the truss were determined. Vibration tests of the power transmission assemblies were carried out, which allowed to determine the amplitudes and frequencies of free vibrations. Finally, a modification of the frame shifting the resonant frequency range was proposed. In conclusions, changes to the design and a schedule of inspections were proposed. The newly designed engine frame should have an extended service life.

Research on Hovercraft – Fatigue Cracks in the Engine Frame

krzysztof.szafran@ilot.lukasiewicz.gov.pl

Fatigue of Aircraft Structures

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

{"article-title":"Research on Hovercraft \u2013 Fatigue Cracks in the Engine Frame"}

Rescue patrol hovercrafts must meet the basic condition – high reliability of use in extreme conditions. The introduction to the work shows damage to the...

Research on Hovercraft – Fatigue Cracks in the Engine Frame

Data publikacji: 28 lip 2022

Zakres stron: 106 - 115

DOI: https://doi.org/10.2478/fas-2021-0010

Słowa kluczowe
rescue, hovercraft exploitation, fatigue degradation, mission safety

© 2021 Krzysztof Stanisław Szafran et al., published by Sciendo

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Research on Hovercraft – Fatigue Cracks in the Engine Frame

Data publikacji: 28 lip 2022

Zakres stron: 106 - 115

DOI: https://doi.org/10.2478/fas-2021-0010

Słowa kluczowerescue, hovercraft exploitation, fatigue degradation, mission safety

© 2021 Krzysztof Stanisław Szafran et al., published by Sciendo

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

Słowa kluczowe
rescue, hovercraft exploitation, fatigue degradation, mission safety