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Aeral injector for combustor of small unmanned aircraft – results of investigation
Publication date: 2006-11-01
Combustion Engines 2006,127(4), 44–53
KEYWORDS
ABSTRACT
The conception of the construction of the fuel spray injector for a turbo engine of a small unmanned aircraft is
proposed in this paper. The work out of the injector model made in rapid prototyping method is shortly presented.
Methods of the injector investigation were described. The results of the injector flow parameters and macrostructure
parameters investigation were presented and discussed. They were used to formulate the main conclusion connected
with the relation between the injector construction, the injector feeding parameters and spray parameters.
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