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Main mixer in an axial staged combustor for a gas turbine engine

Patent ·
OSTI ID:2293859
A main mixer including a swirler along an axis, the swirler including an outer swirler with a multiple of outer vanes, and a center swirler with a multiple of center vanes and a swirler hub along the axis, the swirler hub including a fuel manifold and an inner swirler with a multiple of inner vanes that support a centerbody, the multiple of inner vanes interconnect the fuel manifold and the centerbody.
Research Organization:
RTX Corporation, Farmington, CT (United States)
Sponsoring Organization:
USDOE; National Aeronautics and Space Administration (NASA)
Assignee:
RTX Corporation (Farmington, CT)
Patent Number(s):
11,815,268
Application Number:
17/370,154
OSTI ID:
2293859
Country of Publication:
United States
Language:
English

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