Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Joseph R. Saus"'
Publikováno v:
Journal of Propulsion and Power. 29:991-1000
Lean combustion concepts for aircraft engines are more susceptible to combustion instabilities. Prior activity has demonstrated active control to suppress combustion instabilities with a conventional rich-front-end combustor. The current effort is de
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ca1437c4e75f2b46bd5d860e21ea4704
https://doi.org/10.2514/1.b34653
https://doi.org/10.2514/1.b34653
Publikováno v:
Volume 4: Ceramics; Concentrating Solar Power Plants; Controls, Diagnostics and Instrumentation; Education; Electric Power; Fans and Blowers.
Turbine engines are highly complex mechanical systems that are becoming increasingly dependent on control technologies to achieve system performance and safety metrics. However, the contribution of controls to these measurable system objectives is di
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9527f84395d9f154da639a7fd93c4a04
https://doi.org/10.1115/gt2013-95118
https://doi.org/10.1115/gt2013-95118
Publikováno v:
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
Lean combustion concepts for aircraft engine combustors are prone to combustion instabilities. Mitigation of instabilities is an enabling technology for these low-emissions combustors. NASA Glenn Research Center s prior activity has demonstrated acti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::32c1a3552aae510cdf5d17c0cd704833
https://doi.org/10.2514/6.2012-783
https://doi.org/10.2514/6.2012-783
Publikováno v:
36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Lean-burning combustors are susceptible to combustion instabilities. Additionally, due to non-uniformities in the fuel-air mixing and in the combustion process, there typically exist hot areas in the combustor exit plane. These hot areas limit the op
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::828f60a84c31266062308a6297bbc172
https://doi.org/10.2514/6.2000-3500
https://doi.org/10.2514/6.2000-3500
Publikováno v:
Guidance, Navigation, and Control Conference.
This paper develops a novel sensor validation approach for the F100 turbofan engine by using an autoassociative neural network. The proposed approach utilizes dimensionality reduction to develop the neural network for sensor failure detection and dat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3bf413886af0cea6963a2061bef1f41c
https://doi.org/10.2514/6.1996-3926
https://doi.org/10.2514/6.1996-3926