Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Kenneth Semega"'
Publikováno v:
AIAA Propulsion and Energy 2019 Forum.
Autor:
Richard J. Black, Alexander Von Moll, Vahid Sotoudeh, Behzad Moslehi, Alireza Behbahani, William Price, Michael Osterman, Kenneth Semega, Diganta Das
Publikováno v:
2018 AIAA Information Systems-AIAA Infotech @ Aerospace.
Autor:
William Price, Ming Han, Alexander Von Moll, Behzad Moslehi, Kenneth Semega, Alireza Behbahani, Richard J. Black
Publikováno v:
2018 AIAA Information Systems-AIAA Infotech @ Aerospace.
Publikováno v:
SAE Technical Paper Series.
Publikováno v:
Volume 3: Controls, Diagnostics and Instrumentation; Education; Electric Power; Microturbines and Small Turbomachinery; Solar Brayton and Rankine Cycle.
In this study, the authors conducted a model-based, engine system analysis of Electro-Mechanical Actuators (EMAs). This effort employed an existing, NASA developed, aircraft engine model. A critical engine actuator within the model was replaced by a
Autor:
Kenneth Semega, Alireza Behbahani
Publikováno v:
SAE Technical Paper Series.
Sensing Challenges for Controls and PHM in the Hostile Operating Conditions of Modern Turbine Engine
Autor:
Alireza Behbahani, Kenneth Semega
Publikováno v:
44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Advanced gas turbine engines have evolved over the last several decades to dominate aviation's propulsion, commercial and the military market. Continuing engine performance and reliability advances will require sensor components that operate reliably
Publikováno v:
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
Maintaining continuous performance in the event of failures from aircraft propulsion engines is critical for mission readiness, mission completion, and maintenance cost. In this paper, a Model-Based Control (MBC) approach was developed and demonstrat
Autor:
Kenneth Semega
Publikováno v:
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit.
This paper reviews turbine engine subsy stem technology, consisting of the major components that provide control, fuel, and variable geometry. Curr ent state of the art componen ts play a major role in enabling engine performance and efficiency. Futu
Publikováno v:
Volume 2: Aircraft Engine; Ceramics; Coal, Biomass and Alternative Fuels; Controls, Diagnostics and Instrumentation; Environmental and Regulatory Affairs.
Passive optical probes and high-resolution emission spectroscopy are used to provide a general-purpose real-time temperature and chemical species sensing capability. Probes can be inserted in the combustor, at the turbine inlet, in the augmenter, or