On using PEMFC for Electrical Power Generation on More Electric Aircraft
The electrical power systems of aircrafts have made
serious progress in recent years because the aircrafts depend more
and more on the electricity. There is a trend in the aircraft industry to
replace hydraulic and pneumatic systems with electrical systems,
achieving more comfort and monitoring features and enlarging the
energetic efficiency. Thus, was born the concept More Electric
Aircraft. In this paper is analyzed the integration of a fuel cell into
the existing electrical generation and distribution systems of an
aircraft. The dynamic characteristics of fuel cell systems necessitate
an adaptation of the electrical power system. The architecture studied
in this paper consists of a 50kW fuel cell, a dc to dc converter and
several loads. The dc to dc converter is used to step down the fuel
cell voltage from about 625Vdc to 28Vdc.
[1] Huiyu Zhu. New Multi-Pulse Diode Rectifier Average Models for AC
and DC Power Systems Studies. Thesis of dissertation, 2005
Blacksburg, Virginia;
[2] Emandi, A., Ehsani M. "Aircraft Power Systems: Technology, State of
the Art and Future Trends". IEEE AES Systems Magazine, January
2000;
[3] Pratt J. W., Klebanoff L. E., Munoz-Ramos K., Akhil A. A., Curgus D.
B., Schenkman B. L. "Proton Exchange Membrane Fuel Cells for
Electrical Power Generation On-Board Commercial Airplanes". Sandia
Report, 2011;
[4] Corcau, J., Dinca L. "Problems which imposed More-Electric-Aircraft
developmend". ICATE 2010-10th International Conference on Applied
and Theoretical Electricity, Copernicus data bases, pp. 361-365,
Craiova, 2010;
[5] J. Brombach, A Lucken, D Schulz. "Extended power delivery with fuel
cell systems". Electrical systems for aircraft, railway and ship
propulsion, IEEE Conference, Bologna - Italy, October 19-21, (2010);
[6] M. Santin, A. Traverso, A. Massardo. "Technological aspects of gas
turbine and fuel cell hybrid systems for aircraft: a review". The
Aeronautical Journal, august (2008), vol. 112;
[7] A. L├╝cken, J. Brombach, D. Schulz. "Design and protection of a high
voltage dc on-board grid with integrated fuel cell system on more
electric aircraft". Electrical systems for aircraft, railway and ship
propulsion, IEEE Conference, Bologna - Italy, October 19-21, (2010);
[8] M. A. Maldonado, N. M. Shah, K. J. Cleek, P. S. Walia, G. J. Korba,
"Power management and distribution system for a more-electric aircraft
(MADMEL) - program status," Proc. of 32nd Intersociety Energy
Conversion Engineering Conference, vol. 1, pp. 274- 279, July/Aug.
1997;
[9] Ranjit Jayabalan, "Monitoring and fault diagnosis of multiconverter
power electronic systems", The Unversity of Texas at Arlington,
december 2006;
[10] Florian Misoc, "A comparative study of DC-DC converters- efects on
the output characteristics of direct ethanol fuel cells and NiCd
batteries", Kansas State University 2007;
[11] Moir, "The all-electric aircraft - major challenges", IEE Colloquium on
All Electric Aircraft, digest no. 1998/260, pp. 2/1 - 2/6, June 1998;
[12] Lungu, M. "Aircrafts- control and command using hierarchical dynamic
inversion". Published in Rev. WSEAS TRANSACTIONS on SYSTEMS
and CONTROL, Issue 10, Volume 5, October 2010, pag. 792 - 801.
ISSN: 1991-8763.
[1] Huiyu Zhu. New Multi-Pulse Diode Rectifier Average Models for AC
and DC Power Systems Studies. Thesis of dissertation, 2005
Blacksburg, Virginia;
[2] Emandi, A., Ehsani M. "Aircraft Power Systems: Technology, State of
the Art and Future Trends". IEEE AES Systems Magazine, January
2000;
[3] Pratt J. W., Klebanoff L. E., Munoz-Ramos K., Akhil A. A., Curgus D.
B., Schenkman B. L. "Proton Exchange Membrane Fuel Cells for
Electrical Power Generation On-Board Commercial Airplanes". Sandia
Report, 2011;
[4] Corcau, J., Dinca L. "Problems which imposed More-Electric-Aircraft
developmend". ICATE 2010-10th International Conference on Applied
and Theoretical Electricity, Copernicus data bases, pp. 361-365,
Craiova, 2010;
[5] J. Brombach, A Lucken, D Schulz. "Extended power delivery with fuel
cell systems". Electrical systems for aircraft, railway and ship
propulsion, IEEE Conference, Bologna - Italy, October 19-21, (2010);
[6] M. Santin, A. Traverso, A. Massardo. "Technological aspects of gas
turbine and fuel cell hybrid systems for aircraft: a review". The
Aeronautical Journal, august (2008), vol. 112;
[7] A. L├╝cken, J. Brombach, D. Schulz. "Design and protection of a high
voltage dc on-board grid with integrated fuel cell system on more
electric aircraft". Electrical systems for aircraft, railway and ship
propulsion, IEEE Conference, Bologna - Italy, October 19-21, (2010);
[8] M. A. Maldonado, N. M. Shah, K. J. Cleek, P. S. Walia, G. J. Korba,
"Power management and distribution system for a more-electric aircraft
(MADMEL) - program status," Proc. of 32nd Intersociety Energy
Conversion Engineering Conference, vol. 1, pp. 274- 279, July/Aug.
1997;
[9] Ranjit Jayabalan, "Monitoring and fault diagnosis of multiconverter
power electronic systems", The Unversity of Texas at Arlington,
december 2006;
[10] Florian Misoc, "A comparative study of DC-DC converters- efects on
the output characteristics of direct ethanol fuel cells and NiCd
batteries", Kansas State University 2007;
[11] Moir, "The all-electric aircraft - major challenges", IEE Colloquium on
All Electric Aircraft, digest no. 1998/260, pp. 2/1 - 2/6, June 1998;
[12] Lungu, M. "Aircrafts- control and command using hierarchical dynamic
inversion". Published in Rev. WSEAS TRANSACTIONS on SYSTEMS
and CONTROL, Issue 10, Volume 5, October 2010, pag. 792 - 801.
ISSN: 1991-8763.
@article{"International Journal of Electrical, Electronic and Communication Sciences:65005", author = "Jenica Ileana Corcau and Liviu Dinca", title = "On using PEMFC for Electrical Power Generation on More Electric Aircraft", abstract = "The electrical power systems of aircrafts have made
serious progress in recent years because the aircrafts depend more
and more on the electricity. There is a trend in the aircraft industry to
replace hydraulic and pneumatic systems with electrical systems,
achieving more comfort and monitoring features and enlarging the
energetic efficiency. Thus, was born the concept More Electric
Aircraft. In this paper is analyzed the integration of a fuel cell into
the existing electrical generation and distribution systems of an
aircraft. The dynamic characteristics of fuel cell systems necessitate
an adaptation of the electrical power system. The architecture studied
in this paper consists of a 50kW fuel cell, a dc to dc converter and
several loads. The dc to dc converter is used to step down the fuel
cell voltage from about 625Vdc to 28Vdc.", keywords = "Electrical power system, More Electric Aircraft, Fuel
Cell, dc to dc converter", volume = "6", number = "2", pages = "255-4", }