Design Algorithm of an Aircraft Power Generation System

被引：5

作者：

Ismagilov, Flur Rashitovich ^{[1
]}

Kiselev, Mikhail Anatolyevich ^{[2
]}

Vavilov, Viacheslav Evgenievich ^{[1
]}

Gusakov, Denis Valerievich ^{[1
]}

机构：

[1] Ufa State Aviat Tech Univ, Ufa, Russia

[2] State Res Inst Aviat Syst, Moscow 125319, Russia

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2019年 / 55卷 / 06期

关键词：

Aircraft; Optimization; Windings; Aerospace electronics; Power generation; Standards; Rectifiers; Design algorithm; permanent magnet (PM) machines; power generation; pulse transformers;

D O I：

10.1109/TAES.2019.2894893

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The paper deals with the design and testing of a power generation system for the future and existing aircrafts. A new design algorithm of the power generation components is presented. The proposed design algorithm was tested on a prototype: a full-size starter-generator and transformer-rectifier unit prototype was created with a transformer magnetic core made up of an amorphous magnetic material. Its stand tests were carried out both for each element and for the entire system. The proposed algorithm can be used to create power supply systems for aircraft with different voltage levels, including 270 Vdc and 200 Vac. The developed power generation system turned out to be 25-40% better than serial solutions by mass and efficiency.

引用

页码：2899 / 2910

页数：12

共 50 条

[1] Design of trajectory generation algorithm to enhance position control performance of gimbal system on aircraft
Choi D.-G.
Park J.-Y.
Ahn J.-H.
Choi, Dae-Gyu (daegyu.choi@hanwha.com), 1909, Korean Institute of Electrical Engineers (69): : 1909 - 1915
[2] Design and tests of a new promising ac electric-power generation system for aircraft
Anuchin L.C.
Beliakov Y.O.
Gabidov A.A.
Kozachenko V.F.
Kulmanov V.I.
Ostrirov V.N.
Russian Electrical Engineering, 2015, 86 (01) : 39 - 45
[3] Design and Verification of Aircraft Electrical Power System
Sagirkaya, Huseyin
2023 IEEE INTERNATIONAL CONFERENCE ON ELECTRICAL SYSTEMS FOR AIRCRAFT, RAILWAY, SHIP PROPULSION AND ROAD VEHICLES & INTERNATIONAL TRANSPORTATION ELECTRIFICATION CONFERENCE, ESARS-ITEC, 2023,
[4] Erratum to: “Design and tests of a new promising AC electric-power generation system for aircraft”
A. S. Anuchin
Yu. O. Belyakov
A. A. Gabidov
V. F. Kozachenko
V. I. Kulmanov
V. N. Ostrirov
Russian Electrical Engineering, 2015, 86 (3) : 161 - 161
[5] An algorithm design of sequential component in the aircraft electrical system
Zhao, Wenzhi
IMECS 2007: International Multiconference of Engineers and Computer Scientists, Vols I and II, 2007, : 2413 - 2416
[6] Review of intelligent design of electrified aircraft power system
Wang L.
Dai Z.
Yang S.
Mao L.
Yan Y.
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2019, 40 (02):
[7] Design of an electric generator for an aircraft with a hybrid power system
Varyukhin, Anton N.
Ismagilov, Flyur R.
Vavilov, Viacheslav Ye.
Ayguzina, Valentina V.
Gordin, Mikhail V.
2019 26TH INTERNATIONAL WORKSHOP ON ELECTRIC DRIVES: IMPROVEMENT IN EFFICIENCY OF ELECTRIC DRIVES (IWED) PROCEEDINGS, 2019,
[8] Hybrid power generation system for aircraft electrical emergency network
Roboam, X.
Langlois, O.
Piquet, H.
Morin, B.
Turpin, C.
IET ELECTRICAL SYSTEMS IN TRANSPORTATION, 2011, 1 (04) : 148 - 155
[9] Dynamic Programming Algorithm for Management of Aircraft Power Supply System
Liu, Yazhu
Yang, Shanshui
Wang, Li
Wei, Qinhua
2018 IEEE INTERNATIONAL CONFERENCE ON ELECTRICAL SYSTEMS FOR AIRCRAFT, RAILWAY, SHIP PROPULSION AND ROAD VEHICLES & INTERNATIONAL TRANSPORTATION ELECTRIFICATION CONFERENCE (ESARS-ITEC), 2018,
[10] Design of an automatic transmission system having an arbitrary power flow using the automatic power flow generation algorithm
Seo, J
Yi, SJ
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART D-JOURNAL OF AUTOMOBILE ENGINEERING, 2005, 219 (D9) : 1085 - 1097

← 1 2 3 4 5 →