Method for guiding of a spark plug into a turbine engine combustion chamber
A turbine engine, combustion chamber technology, applied in the field of spark plugs, can solve problems such as wear and tear
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[0039] in such as figure 1 and 2 In the prior art shown, the annular combustor of a turbine engine such as an aircraft turboprop or turbojet is mounted on an outer shell 2 and comprises: a housing 3 forming a body of rotation, the housing 3 having a a downstream annular flange fixed to the casing 2; an inner casing 4, which also forms a body of revolution, the inner casing 4 having a downstream annular flange for mounting on the inner casing; and a combustion chamber end wall 5, on which A fairing 6 extending upstream is installed.
[0040] Injection lines 7 distributed around the axis of the turbine engine lead via injection heads 8 to the combustion chamber end wall 5 . A deflector plate 9 is provided around each spray head 8 .
[0041] The airflow delivered by the compressor of the turbine engine is directed through the cowl 6 into an airflow divided into a central channel for feeding into the combustion chamber 1 and two outer channels extending around the combustion ch...
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