AIRCRAFT ENGINE COMPRISING AZIMUTH SETTING OF THE DIFFUSER WITH RESPECT TO THE COMBUSTION CHAMBER
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Apr 7, 2015
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Apr 9, 2014
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The fixed vanes of a diffuser are set to an azimuth angle setting (α) with respect to the injectors of a combustion chamber so that the paths leading from the trailing edges pass through the gaps between injectors and more preferably mid-way between same, so that these portions of the flow, which may contain condensed water, do not affect the initiation of the combustion.
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