Title :
270-VDC/hybrid 115-VAC electric power generating system technology demonstrator
Author :
Niggeman, R.E. ; Peecher, S. ; Rozman, G.
Author_Institution :
Sundstrand Aerosp., Rockford, IL, USA
Abstract :
Sundstrand is actively investigating the technologies required by 270-VDC, hybrid 115-VAC systems to meet power quality and stability requirements when supplying largely negative impedance loads. The design of the technology demonstrator system has focused on assembling a highly flexible test system that is capable of providing the data and experience necessary to successfully design and build a high-efficiency, high-reliability, fault-tolerant, low-weight, low-cost hybrid aircraft electrical system for future applications. Data taken to date indicate that voltage regulation requirements of Aerospace Standard AS1831 or MIL-STD-MS704E can be met with state-of-the-art technology. It is demonstrated that with improper source/load impedance matching, system instability can occur. Measurements of source and load impedance compare reasonably well in both magnitude and phase with analytical predictions
Keywords :
aircraft; impedance matching; power supplies to apparatus; voltage regulators; 115 V; 270 V; AC; Aerospace Standard AS1831; DC; MIL-STD-MS704E; assembling; demonstrator; electric power generating system; fault tolerant power generation; flexible test system; hybrid aircraft electrical system; negative impedance loads; power quality; source/load impedance matching; stability; voltage regulation; Aerospace testing; Aircraft; Assembly systems; Fault tolerant systems; Hybrid power systems; Impedance; Power generation; Power quality; Stability; System testing;
Conference_Titel :
Aerospace and Electronics Conference, 1991. NAECON 1991., Proceedings of the IEEE 1991 National
Conference_Location :
Dayton, OH
Print_ISBN :
0-7803-0085-8
DOI :
10.1109/NAECON.1991.165788