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Studies into hail ingestion of turbofan engines using a rotating fan and spinner assembly

Published online by Cambridge University Press:  04 July 2016

H. Pant  and
P. M. Render
H. Pant
Affiliation:
Department of Aeronautical and Automotive Engineering and Transport StudiesLoughborough UniversityLoughborough, UK
P. M. Render
Affiliation:
Department of Aeronautical and Automotive Engineering and Transport StudiesLoughborough UniversityLoughborough, UK
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Abstract

Simulated hailstones were made to impact on the rotating spinner and fan assembly of a Williams FJ44 engine. The mass distribution of ice behind the fan was determined by use of a suction tube technique. Suction was added to ensure that the tube did not affect the flow through the fan assembly. The strong air flow behind the fan meant that the ice caught by the tube melted and evaporated. This made it difficult to accurately determine the mass distribution of ice. As a result, the simulated hailstones were made from a water-salt solution so that the weight of salt residue could be measured after the water had evaporated, and hence the amount of ice caught was determined. A parametric study into the hail ingestion characteristics of the fan assembly was carried out. The parameters studied included the radial position of the impact point, the rotational speed of the fan and the position of the splitter between the core engine and bypass duct. The results showed that the impact position had a major effect on the overall ice distribution, which was determined by the combination of blade geometry at the impact point and the rotational speed. The splitter position was shown to have a significant effect on the amount of ice passing into the bypass duct.

Type
Research Article
Information
The Aeronautical Journal , Volume 102 , Issue 1011 , January 1998 , pp. 45 - 52
Copyright
Copyright © Royal Aeronautical Society 1998 

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Footnotes

†

Currently at Topmode Systems

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