diff options
Diffstat (limited to 'references.bib')
| -rw-r--r-- | references.bib | 88 |
1 files changed, 88 insertions, 0 deletions
diff --git a/references.bib b/references.bib new file mode 100644 index 0000000..19c9c85 --- /dev/null +++ b/references.bib @@ -0,0 +1,88 @@ +@phdthesis {MelvinThesis, + TYPE = {Master's Thesis}, + MONTH = {May}, + AUTHOR = {Melvin, Joshua}, + TITLE = {INTEGRATION AND EVALUATION OF A 180-KW TURBOPROP ENGINE WITH A TURBOELECTRIC GROUND TEST RIG}, + SCHOOL = {OKLAHOMA STATE UNIVERSITY}, + YEAR = {2021}, + } +@article {CessnaASME, + AUTHOR = {Johnsen, Joshua and Melvin, Joshua and Drake, Joshua and Jdiobe, Muwanika and Rouser, Kurt}, + TITLE = {Experimental Evaluation of an Electric PowerTrain Designed for a 180-kW Turboelectric Aircraft Ground Test Rig}, + JOURNAL = {Journal of Engineering for Gas Turbines and Power}, + FJOURNAL = {ASME Journal of Engineering for Gas Turbines and Power}, + VOLUME = {146}, + YEAR = {2024}, + NUMBER = {}, + PAGES = {}, + ISSN = {}, + MRCLASS = {}, + MRNUMBER = {}, +MRREVIEWER = {}, + DOI = {}, + URL = {}, +} +@Article{TurboelectricAS, +AUTHOR = {Burgess, Johnathan and Runnels, Timothy and Johnsen, Joshua and Drake, Joshua and Rouser, Kurt}, +TITLE = {Experimental Comparison of Direct and Active Throttle Control of a 7 kW Turboelectric Power System for Unmanned Aircraft}, +JOURNAL = {Applied Sciences}, +VOLUME = {11}, +YEAR = {2021}, +NUMBER = {22}, +ARTICLE-NUMBER = {10608}, +URL = {https://www.mdpi.com/2076-3417/11/22/10608}, +ISSN = {2076-3417}, +ABSTRACT = {This article compares direct turbine throttle control and active turbine throttle control for a turboelectric system; the featured turboprop is rated for 7 kW of shaft output power. The powerplant is intended for applications in unmanned aerial systems and requires a control system to produce different amounts of power for varying mission legs. The most straightforward control scheme explored is direct turbine control, which is characterized by the pilot controlling the throttle of the turbine engine. In contrast, active control is characterized by the turbine reacting to the power demanded by the electric motors or battery recharge cycle. The transient response to electric loads of a small-scale turboelectric system is essential in identifying and characterizing such a system’s safe operational parameters. This paper directly compares the turbogenerator’s transient behavior to varying electric loads and categorizes its dynamic response. A proportional, integral, and derivative (PID) control algorithm was utilized as an active throttle controller through a microcontroller with battery power augmentation for the turboelectric system. This controller manages the turbine’s throttle reactions in response to any electric load when applied or altered. By comparing the system’s response with and without the controller, the authors provide a method to safely minimize the response time of the active throttle controller for use in the real-world environment of unmanned aircraft.}, +DOI = {10.3390/app112210608} +} +@inbook{doi:10.2514/6.2018-4984, +author = {Cheryl L. Bowman and Ty V. Marien and James L. Felder}, +title = {Turbo- and Hybrid-Electrified Aircraft Propulsion for Commercial Transport}, +booktitle = {2018 AIAA/IEEE Electric Aircraft Technologies Symposium}, +chapter = {}, +pages = {}, +doi = {10.2514/6.2018-4984}, +year = {2018}, +URL = {https://arc.aiaa.org/doi/abs/10.2514/6.2018-4984}, +eprint = {https://arc.aiaa.org/doi/pdf/10.2514/6.2018-4984} +} +@article{hybrid_trends, +author = {Rendón, Manuel and Sánchez, Carlos and Gallo Muñoz, Josselyn and Anzai, Alexandre}, +year = {2021}, +month = {06}, +pages = {}, +title = {Aircraft Hybrid-Electric Propulsion: Development Trends, Challenges and Opportunities (https://rdcu.be/cmG4u)}, +journal = {Sba Controle \& Automação Sociedade Brasileira de Automatica}, +doi = {10.1007/s40313-021-00740-x} +} +@inproceedings{nasa_prop_overview, + author = {Jansen, Ralph}, + year = {2017}, + URL = {https://ntrs.nasa.gov/api/citations/20180000593/downloads/20180000593.pdf}, + organization = {NASA Glenn Research Center}, + title = {Overview of NASA Electrified Aircraft Propulsion Activities}, +} +@manual{tp100technical, + year = {2015}, + month = {April}, + title = {Basic Technical Information Turboprop Engine TP100}, + publisher = {PBS Aerospace}, + number = {PP-63}, + version = {2}, + issue = {Second}, + author = {PBS Aerospace}, + institution = {PBS Aerospace} +} +@inproceedings{nasa_turbojet, + author = {NASA}, + year = {2017}, + URL = {https://www.grc.nasa.gov/WWW/K-12/airplane/turbth.html}, + organization = {NASA Glenn Research Center}, + title = {Turbojet Engine}, +} +@book{EoPGTR2, + title = {Elements of Propulsion: Gas Turbines and Rockets 2nd Edition}, + year = {2016}, + author = {Mattingly, Jack and von Obain, Hans}, + publisher = {AIAA}, +} |