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Evaluation of the transient operation of advanced gas turbine combustorsA unique test capability has been defined and used at the United Technologies Research Center to evaluate the transient response of advanced gas turbine combustors. This UTC Transient Combustion Facility offers the opportunity to achieve pre-defined time variations of the air and fuel flow rates and air temperature delivered to a combustor model. This capability can be used for model scales ranging from multi-nozzle combustor sectors to smaller setups focusing on one component or process. A dedicated control computer aids in establishing time profiles for the input parameters and automatically executing the transient test. Among its applications, the facility has been used to study the occurrence of in-nozzle fuel vaporization during Bodie cycles and to assess the tolerance of a fuel-staged combustor to rapid fuel redistribution.
Document ID
19940024766
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
T J Rosfjord
(United Technologies Research Center East Hartford, Connecticut, United States)
J M Cohen
(United Technologies Research Center East Hartford, Connecticut, United States)
Date Acquired
August 16, 2013
Publication Date
September 1, 1993
Publication Information
Publication: AGARD, Fuels and Combustion Technology for Advanced Aircraft Engines
Publisher: North Atlantic Treaty Organization
ISBN: 92-835-0719-3
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AD-A275679
AGARD-CP-536
Meeting Information
Meeting: The Propulsion and Energetics Panel 81st Symposium
Location: Fiuggi
Country: IT
Start Date: May 10, 1993
End Date: May 14, 1993
Sponsors: North Atlantic Treaty Organization
Accession Number
94N29269
Funding Number(s)
CONTRACT_GRANT: N00140-87-C-9902
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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