Uçaklarda Kullanım Amaçlı Interleaved Süper Lift Luo Dönüştürücü Tasarımı

Öz

Bu çalışmanın temel amacı, havacılık sistemleri için mevcut topolojilere kıyasla daha düşük kayıplar elde etmek için 28V batarya ile çalışan 1,2kW interleaved super lift Luo dönüştürücü tasarlamaktır. Uygulanan devrenin basit yapısı nedeniyle kayıplarda azalma amaçlanmaktadır. F-22 gibi askeri uçaklar ve Boeing 787 gibi sivil uçaklar batarya sistemleri için 270V DC kullanmaktadırlar. Bu nedenle, 270V DC standardının uygun olduğu yeni hava araçları eski gerilim standartlarıyla çalışmayabilir. 28'den 270 volta yükseltme hem eski hem de yeni sistemler için iyi bir çözüm olarak düşünülmektedir. Bu nedenle, eski havacılık teknolojisini yeni sistemlere uyarlamak için 28 voltu 270 volta yükselten bir interleaved süper lift Luo dönüştürücü tasarımı önerilmiştir. Silisyum karbür MOSFET tabanlı interleaved süper lift Luo dönüştürücünün çift döngü PI kontrolör tasarımı gerçekleştirilmiştir. Bu makale, alanındaki gelişmelere uyum sağlamak amacıyla uçaklarda kullanım için interleaved süper lift Luo dönüştürücü tasarımının prensiplerini göstermektedir ve konsept simülasyonlar kullanılarak doğrulanmıştır.

Anahtar Kelimeler

• Uçak,DA-DA güç dönüşümü,Darbe genişlik modülasyonu

An Interleaved Super Lift Luo Converter Design for Aircraft Applications

Öz

The main purpose of this study is to adapt a 28V battery powered super Lift Luo converter topology to the aircraft systems by adding the interleaving feature. It is aimed to have better efficiency compared to conventional designs. F-22 military aircraft and civil aircraft such as Boeing 787 use 270V DC for battery systems. New standards for the avionics using 270V DC may not apply to older avionics. Therefore, conversion from 28V to 270V can be an advantageous application for both new and old systems. As a result, an interleaved super lift Luo converter has been designed to increase the voltage from 28V to 270V with a quite high conversion ratio so existing old systems stay up-to-date due to developments. Analysis of this new interleaved super lift Luo converter was carried out with a double loop PI controller. The topology uses silicon carbide MOSFETs as high-frequency switches. This paper shows the design philosophy of the converter and proves the system with simulations.

Anahtar Kelimeler

• Aircraft,DC-DC power converters,Pulse width modulation

Kaynakça

1. Rosero J. A., Ortega J. A., Aldabas E. and Romeral L. (2007). Moving towards a more electric aircraft. IEEE Aerospace and Electronic Systems Magazine, 22, 3-9.
2. Moir I., Seabridge A. (2011). Aircraft systems: mechanical, electrical, and avionics subsystems integration 3rd ed. John Wiley & Sons Inc.
3. Military Standards. (1975). Aircraft Electric Power Characteristics, MIL-STD-704B http://everyspec.com/MIL-STD/MIL-STD-0700-0799/download.php?spec=MIL-STD-704B.021342.PDF
4. Madonna V., Giangrande P. and Galea M. (2018). Electrical Power Generation in Aircraft: Review, Challenges, and Opportunities. IEEE Transactions on Transportation Electrification, 4, 646-659.
5. Quigley R. E. J. (1993). More Electric Aircraft. IEEE Proceedings Eighth Annual Applied Power Electronics Conference and Exposition. 7- 11 March, San Diego, CA, USA, 906-911.
6. Weimer J. A. (1993). Electrical power technology for the more electric aircraft. AIAA/IEEE Digital Avionics Systems Conference. 25-28 October, Fort Worth, TX, USA, 445-450.
7. Kreutzer O., Billmann M., Maerz M. and Lange A. (2016). Non-isolating DC/DC Converter for a Fuel Cell Powered Aircraft. IEEE International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles & International Transportation Electrification Conference. 2-4 November. Toulouse, 1-6.
8. Clements R. and Jones R. W. (2018). DC-DC convertor design for the 270 volts DC ‘More Electric Aircraft’. IEEE Conference on Industrial Electronics and Applications, 31 May - 2 June, Wuhan, 1847-1852.

9. Rubino L., Guida B., Liccardo F., Marino P. and Cavallo A. (2010). Buck-boost DC/DC converter for aeronautical applications. IEEE International Symposium on Industrial Electronics. 4-7 July. Bari, 2690-2695.
10. De D., Castellazzi A., Lopez-Arevalo S. and Lamantia A. (2014). SiC MOSFET based avionic power supply. 7th IET International Conference on Power Electronics, Machines and Drives. 8-10 April, Manchester, 1-6.
11. Duarte R. R., Ferreira G. F., Dalla Costa M. A. and Alonso J. M. (2017). Performance investigation of silicon and gallium nitride transistors in an integrated double buck-boost LED driver. IEEE Industry Applications Society Annual Meeting, Cincinnati, 1-5 October, OH, 1-5.
12. Chen H., Hao Z., Shao C., Pu C. and Lu B. (2018). Research on 270V/28V aviation bidirectional DC/DC converter. CSAA/IET International Conference on Aircraft Utility Systems, 19-22 June, Guiyang, 1-7.
13. Military Standards. (2016). Aircraft Electric Power Characteristics, MIL-STD-704F w/CHANGE 1 http://everyspec.com/MIL-STD/MIL-STD-0700-0799/download.php?spec=MIL-STD-704F_CHG-1.055461.pdf
14. Shan Z., Liu S. and Luo F. (2012). Investigation of a Super-Lift Luo-Converter used in solar panel system. China International Conference on Electricity Distribution, 10-14 September, Shanghai, 1-4.
15. Luo, F. L. & Y. Hong (2016). Advanced DC/DC Converters 2nd ed. CRC Press, Florida.
16. González A., López-Erauskin R., and Gyselinck J. Analysis, modeling, control and operation of an interleaved three-port boost converter for DMPPT systems including PV and storage at module level. Heliyon, 5.
17. Florides M. (2010). Interleaved Switching of DC/DC Converters. MEng Thesis, University of Newcastle Upon Tyne, Newcastle. https://www.researchgate.net/publication/308886975_Interleaved_Switching_of_DCDC_Converters
18. Wang X., Loh P. C. and Blaabjerg F. (2017). Stability Analysis and Controller Synthesis for Single-Loop Voltage-Controlled VSIs. IEEE Transactions on Power Electronics, 32, 7394-7404.
19. Wang X., Li Y. W., Blaabjerg F. and Loh P. C. (2015). Virtual-Impedance-Based Control for Voltage-Source and Current-Source Converters. IEEE Transactions on Power Electronics, 30, 7019-7037.
20. Wang X., Blaabjerg F., Chen Z. and Wu W. (2013). Resonance analysis in parallel voltage-controlled Distributed Generation inverters. Twenty-Eighth Annual IEEE Applied Power Electronics Conference and Exposition. 17-21 March, Long Beach, CA, 2977-2983.
21. Wang X., Blaabjerg F., Loh P.C. (2015). High-performance feedback-type active damping of LCL-filtered voltage source converters. Energy Conversion Congress and Exposition. 20-24 September 2015, 2629-2636.