New electric starter system based on on-board power network with hydrogen energy storage☆

被引:0
作者
Zharkov, M. A. [1 ]
Sarakhanova, R. Yu [1 ]
Kharitonov, S. A. [1 ]
机构
[1] Novosibirsk State Tech Univ NSTU, Prospekt K Marksa 20 Bldg 4,Room 316, Novosibirsk 630073, Russia
关键词
Hydrogen; Hydrogen storage; Starting system; Three-stage synchronous generator; Dc/ac converter; Control system; Electromagnetic torque of a synchronous; generator; Angular characteristic;
D O I
10.1016/j.ijhydene.2024.08.325
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
Current trends in industries related to autonomous, mobile objects, such as aircraft manufacturing, are aimed at increasing the share of electrification or completely replacing all units in favor of electric ones. Replacing components and assemblies with fully electric ones corresponds to the concept of a fully electric aircraft, which is based on new power sources and sources of electric propulsion, such as lithium-ion batteries, hydrogen batteries, and sources based on renewable energy. At the same time, the requirements for energy efficiency and weight and size parameters of components and assemblies are increasing. These needs can be met through the multi-purpose use of equipment, as well as through new systems that combine a number of functions. The article discusses the use of an aircraft three-stage synchronous generator as a starting device for a gas turbine engine. The problems associated with the use of a three-stage generator are analyzed and a method for solving them is proposed. The article presents a method for creating a starting torque using the reactive component of the electromagnetic torque for a synchronous salient pole generator. The analysis was carried out from the point of view of the formation of electromagnetic torque in an aircraft generator using a voltage inverter. A generalized expression for the torque is obtained, regulated and controlled by the electrical parameters of the frequency converter.
引用
收藏
页码:385 / 393
页数:9
相关论文
共 68 条
[1]  
Balagurov VA, 1990, Design of special AC electrical machines, P272
[2]   Investigation on the Selection of Electric Power System Architecture for Future More Electric Aircraft [J].
Chen, Jiawei ;
Wang, Chengjun ;
Chen, Jie .
IEEE TRANSACTIONS ON TRANSPORTATION ELECTRIFICATION, 2018, 4 (02) :563-576
[3]   On Power Quality of Variable-Speed Constant-Frequency Aircraft Electric Power Systems [J].
Eid, Ahmad ;
El-Kishky, Hassan ;
Abdel-Salam, Mazen ;
El-Mohandes, Mohamed T. .
IEEE TRANSACTIONS ON POWER DELIVERY, 2010, 25 (01) :55-65
[4]  
Firago BI, 2004, Theory of electric drive, P527
[5]  
Gusev A.L., RF Patent, Patent No. 2082911
[6]  
Gusev A.L., 2004, P 30 ISTC JAP WORKSH, P226
[7]  
Gusev A. L., 2002, Hydrogen materials science and chemistry of metal hydrides, DOI [10.1007/978-94-010-0558-65, DOI 10.1007/978-94-010-0558-65.978-1-4020-0731-6]
[8]  
Gusev A.L., Patent of Russian Federation, Patent No. 2027942
[9]  
Gusev A.L., 1994, Patent of Russian Federation, Patent No. [N2022204, 2022204]
[10]  
Gusev A.L., RF Patent, Patent No. [N2082910, 2082910]