Annular deflection wall for turbomachine combustion chamber injection system providing a wide fuel atomization zone
A deflection wall 100 for improving the air fuel mix in a turbo machine combustion chamber, having a downstream edge 102 formed by the repetition of a sinuous pattern 104. The pattern being an undulation or wave formed from a plurality of bosses 120, 122 with downstream ends 124, 126 which alternate...
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| Format: | Patent |
| Sprache: | eng |
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| Zusammenfassung: | A deflection wall 100 for improving the air fuel mix in a turbo machine combustion chamber, having a downstream edge 102 formed by the repetition of a sinuous pattern 104. The pattern being an undulation or wave formed from a plurality of bosses 120, 122 with downstream ends 124, 126 which alternately project radially inward or outward. The bosses or deflections are oriented with their longitudinal axis P2 at an angle relative to the longitudinal axis of the deflection wall itself P1. |
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