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Heat transfer in an injector-scaled additively manufactured fuel passage

journal contribution
posted on 2023-11-07, 11:05 authored by Thomas WalkerThomas Walker, Clare Bonham

Knowledge of heat transfer in fuel wetted passages is important for informing injector design and life estimates due to the effects of temperature on fuel degradation. Future injectors will be manufactured using additive methods in an effort to reduce production costs and time, while also facilitating more agile design practices. Additive manufacturing (AM) is known to result in increased surface roughness compared to conventional manufacturing techniques, however limited data exist on how this roughness impacts heat transfer, particularly in liquid flows. This paper solves the inverse heat conduction problem for heat transfer coefficient in liquid flows through rough 90 deg channel bends typical of the pilot gallery in a lean direct-injection fuel spray nozzle. Heat transfer distributions across two rough surfaces are compared to an equivalent smooth surface. The two rough surfaces have different morphologies but have the same relative effective sand grain roughness which is matched to a prototype AM fuel injector. The sand grain roughness is predicted from a correlation that has been adapted for the high relative roughness scales characteristic of additively manufactured fuel passages. The effective sand grain roughness estimated from surface measurements of a prototype AM fuel gallery was ∼13% of the passage hydraulic diameter. For the two rough surfaces, the heat transfer enhancement is up to three times the smooth surface value for the straight section preceding the bend and up to four times around the bend. Heat transfer distributions across the two rough surfaces are similar, but the magnitudes differ by ∼17% depending on the surface morphology. This highlights the importance of the heat transfer effectiveness of surface features, which unlike the sand grain roughness is not matched for the two surfaces considered. Adjusting the data for differences in heat transfer effectiveness corrects the average heat transfer for the rough surfaces to within 7%.

Funding

EPSRC Centre for Doctoral Training in Gas Turbine Aerodynamics

Engineering and Physical Sciences Research Council

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Rolls-Royce

History

School

  • Aeronautical, Automotive, Chemical and Materials Engineering

Department

  • Aeronautical and Automotive Engineering

Published in

Journal of Turbomachinery

Volume

146

Issue

1

Publisher

ASME International

Version

  • AM (Accepted Manuscript)

Rights holder

© Rolls-Royce plc

Publisher statement

This paper was accepted for publication in the journal Journal of Turbomachinery and the definitive published version is available at https://doi.org/10.1115/1.4063569.

Acceptance date

2023-08-25

Publication date

2023-10-19

Copyright date

2023

ISSN

0889-504X

eISSN

1528-8900

Other identifier

Paper No: TURBO-23-1145

Language

  • en

Depositor

Tom Walker. Deposit date: 6 November 2023

Article number

011001

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