Zobrazeno 1 - 10
of 71
pro vyhledávání: '"Ten-Huei Guo"'
Publikováno v:
Volume 6: Ceramics; Controls, Diagnostics and Instrumentation; Education; Manufacturing Materials and Metallurgy.
The efficiency of aircraft gas turbine engines is sensitive to the distance between the tips of its turbine blades and its shroud, which serves as its containment structure. Maintaining tighter clearance between these components has been shown to inc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a33cca98de8952c9a21356090c99ea7a
https://doi.org/10.1115/gt2017-63472
https://doi.org/10.1115/gt2017-63472
Publikováno v:
International Journal of Smart Engineering System Design. Jan2003, Vol. 5 Issue 1, p21-32. 12p.
Publikováno v:
52nd AIAA/SAE/ASEE Joint Propulsion Conference.
Gas turbine compressor and turbine blade tip clearance (i.e., the radial distance between the blade tip of an axial compressor or turbine and the containment structure) is a major contributing factor to gas path sealing, and can significantly affect
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::289b51fcc2bfc096a67becc2b12d55e3
https://doi.org/10.2514/6.2016-5047
https://doi.org/10.2514/6.2016-5047
Autor:
Jeffryes W. Chapman, Ten-Huei Guo
Publikováno v:
AIAA Atmospheric Flight Mechanics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::21b8392385a83fa53d70f2bc1df0e623
https://doi.org/10.2514/6.2016-1043
https://doi.org/10.2514/6.2016-1043
Autor:
C.L.P. Chen, Ten-Huei Guo
Publikováno v:
IEEE Transactions on Systems, Man and Cybernetics, Part C (Applications and Reviews). 37:1005-1015
Aircraft engine controllers are designed and operated to provide desired performance and stability margins. This paper addresses the relationship between acceleration action and engine component life usage. Based upon this relationship, an intelligen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a502cfa32b980b358a9f86457ad6d9ed
https://doi.org/10.1109/tsmcc.2007.902823
https://doi.org/10.1109/tsmcc.2007.902823
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
The National Aeronautics and Space Administration (NASA) has developed independent airframe and engine models that have been integrated into a single real-time aircraft simulation for piloted evaluation of propulsion control algorithms. In order to h
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::802f09478819ed2758abc55f781fca42
https://doi.org/10.2514/6.2015-1476
https://doi.org/10.2514/6.2015-1476
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
The engine control system for civil transport aircraft imposes operational limits on the propulsion system to ensure compliance with safety standards. However, during certain emergency situations, aircraft survivability may benefit from engine perfor
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f715025fcba43faf33bd1e47c6063012
https://doi.org/10.2514/6.2014-3637
https://doi.org/10.2514/6.2014-3637
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
A simulation toolbox has been developed for the creation of both steady-state and dynamic thermodynamic software models. This paper describes the Toolbox for the Modeling and Analysis of Thermodynamic Systems (T-MATS), which combines generic thermody
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f8592e08abbe08453cfcab711e4b86e3
https://doi.org/10.2514/6.2014-3929
https://doi.org/10.2514/6.2014-3929
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
A modular thermodynamic simulation package called the Toolbox for the Modeling and Analysis of Thermodynamic Systems (T-MATS) has been developed for the creation of dynamic simulations. The T-MATS software is designed as a plug-in for Simulink (Math
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::773486fb3cfaaf0d7103e1384a8cd1a3
https://doi.org/10.2514/6.2014-3931
https://doi.org/10.2514/6.2014-3931
Autor:
Ten-Huei Guo, Thomas M. Lavelle
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::df7097befc19dc6635476a4351f81eba
https://doi.org/10.2514/6.2014-3932
https://doi.org/10.2514/6.2014-3932