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

Abstract

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.

Inventors:
; ;
Issue Date:
Research Org.:
RTX Corporation, Farmington, CT (United States)
Sponsoring Org.:
USDOE; National Aeronautics and Space Administration (NASA)
OSTI Identifier:
2293859
Patent Number(s):
11815268
Application Number:
17/370,154
Assignee:
RTX Corporation (Farmington, CT)
Patent Classifications (CPCs):
F - MECHANICAL ENGINEERING F23 - COMBUSTION APPARATUS F23R - GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
Y - NEW / CROSS SECTIONAL TECHNOLOGIES Y02 - TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE Y02T - CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
DOE Contract Number:  
NNC14CA30C
Resource Type:
Patent
Resource Relation:
Patent File Date: 07/08/2021
Country of Publication:
United States
Language:
English

Citation Formats

Dai, Zhongtao, Smith, Lance L., and Cohen, Jeffrey M. Main mixer in an axial staged combustor for a gas turbine engine. United States: N. p., 2023. Web.
Dai, Zhongtao, Smith, Lance L., & Cohen, Jeffrey M. Main mixer in an axial staged combustor for a gas turbine engine. United States.
Dai, Zhongtao, Smith, Lance L., and Cohen, Jeffrey M. Tue . "Main mixer in an axial staged combustor for a gas turbine engine". United States. https://www.osti.gov/servlets/purl/2293859.
@article{osti_2293859,
title = {Main mixer in an axial staged combustor for a gas turbine engine},
author = {Dai, Zhongtao and Smith, Lance L. and Cohen, Jeffrey M.},
abstractNote = {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.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2023},
month = {11}
}

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