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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