Combustion and cooling performance in an aero-engine annular combustor
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Title: Combustion and cooling performance in an aero-engine annular combustor

Essay Details:

Subject: Technology
Author: John F
Date: January 6, 2015
Level:
Grade: A
Length: 16 / 4622

Essay text:

A counter-rotating vortex pair (CRVP) ensures the ignition and flame stability formed in the head zone of the combustor, and the strong injections from the first row of the in-line dilution holes retard flame diffusion downstream. The rotation leads to a non-symmetry of exit temperature distribution. The tubes are cooled by the full film from discrete tiny holes with the average diameter 1.5 mm. The flow structures in the downstream zones of several typical cooling holes are analyzed to study the contribution of dilution jets to film formation and cooling performance. Generally, the air film is very uniform and can protect tubes nearly whole surface very well...

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