NON-FLAME-OUT TEST FOR THE COMBUSTION CHAMBER OF A TURBINE ENGINE
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United States of America Patent
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Issued Date -
Aug 23, 2012
app pub date -
Oct 18, 2010
filing date -
Oct 19, 2009
priority date (Note) -
Abandoned
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Abstract
A method for ground control of proper operation of an aeronautical turbine engine for a plane. A test includes carrying out, on the operating turbine engine and from a predetermined speed, a quick reduction in fuel flow according to a programmed decrease to evaluate flame-out resistance of the combustion chamber of the turbine engine during a quick inflight deceleration maneuver of the speed thereof.
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