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Advanced Low-Emissions Catalytic-Combustor Program, phase 1Six catalytic combustor concepts were defined, analyzed, and evaluated. Major design considerations included low emissions, performance, safety, durability, installations, operations and development. On the basis of these considerations the two most promising concepts were selected. Refined analysis and preliminary design work was conducted on these two concepts. The selected concepts were required to fit within the combustor chamber dimensions of the reference engine. This is achieved by using a dump diffuser discharging into a plenum chamber between the compressor discharge and the turbine inlet, with the combustors overlaying the prediffuser and the rear of the compressor. To enhance maintainability, the outer combustor case for each concept is designed to translate forward for accessibility to the catalytic reactor, liners and high pressure turbine area. The catalytic reactor is self-contained with air-cooled canning on a resilient mounting. Both selected concepts employed integrated engine-starting approaches to raise the catalytic reactor up to operating conditions. Advanced liner schemes are used to minimize required cooling air. The two selected concepts respectively employ fuel-rich initial thermal reaction followed by rapid quench and subsequent fuel-lean catalytic reaction of carbon monoxide, and, fuel-lean thermal reaction of some fuel in a continuously operating pilot combustor with fuel-lean catalytic reaction of remaining fuel in a radially-staged main combustor.
Document ID
19820014391
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sturgess, G. J.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1981
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:159656
ESL-TR-79-23
NASA-CR-159656
PWA-5589-19
Report Number: NAS 1.26:159656
Report Number: ESL-TR-79-23
Report Number: NASA-CR-159656
Report Number: PWA-5589-19
Accession Number
82N22265
Funding Number(s)
PROJECT: RTOP 505-03-22
CONTRACT_GRANT: NAS3-20821
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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