Zobrazeno 1 - 10
of 1 480
pro vyhledávání: '"More Electric Aircraft"'
Autor:
QING Xinlin
Publikováno v:
Hangkong gongcheng jinzhan, Vol 15, Iss 3, Pp 27-44 (2024)
The aircraft power supply system is the power source of all electrical equipment on board，thus its safety and reliability are pretty important. Against the backdrop of environmental protection and high-efficiency development needs，research and ap
Externí odkaz:
https://doaj.org/article/b0ea6ac3ab684a0d916ca42ca29f7ba7
Autor:
Karvekar, Aditi Sushil, Joshi, Prasad
Publikováno v:
World Journal of Engineering, 2023, Vol. 21, Issue 3, pp. 510-521.
Externí odkaz:
http://www.emeraldinsight.com/doi/10.1108/WJE-12-2022-0478
Publikováno v:
IEEE Access, Vol 12, Pp 164325-164336 (2024)
More Electric Aircraft (MEA) and All Electric Aircraft (AEA) require advanced autonomous electric Energy Management Systems (EMS) onboard the aircraft. The aircraft electric network can be considered as an islanded microgrid, and as such some approac
Externí odkaz:
https://doaj.org/article/b99a7891f70a4c94a2fac16033dcc922
Publikováno v:
IEEE Access, Vol 12, Pp 112053-112061 (2024)
There is a growing need for electrical power due to increased challenging electrical characteristics of newly developed avionics and mission system equipment in aircrafts. Therefore, with the development of More Electric Aircraft (MEA) and All Electr
Externí odkaz:
https://doaj.org/article/710b8950c1424d208ecec9471e62fe94
Publikováno v:
IEEE Access, Vol 12, Pp 100908-100920 (2024)
The number of power converters that act as constant power loads (CPLs) has increased continuously with the penetration of power electronic technology in more electric aircraft (MEA). The negative impedance of CPLs can drastically degrade overall stab
Externí odkaz:
https://doaj.org/article/8662913ffb5547bb98e5bc8924b088e3
Autor:
Jierui Zhou, Mohamadreza Arab Baferani, Tohid Shahsavarian, Patrick McGinnis, Steven Walker, Dehao Qin, Zheyu Zhang, Dong Dong, Di Zhang, Chuanyang Li, Yang Cao
Publikováno v:
IEEE Access, Vol 12, Pp 77347-77355 (2024)
PCB layouts with different polygon shapes and insulation distances were prepared and their surface flashover voltage subjected to different ramping rates were measured at different temperatures and different low gas pressures for emulated high-altitu
Externí odkaz:
https://doaj.org/article/9d9e9a912ed74be287a569d39755060b
Publikováno v:
IEEE Access, Vol 12, Pp 76579-76588 (2024)
An important reflection of the overall efficiency, reliability, and passenger safety of a more electric aircraft (MEA) is the output performance of its electrical power system (EPS) controller. This output performance encompasses the rise time, setti
Externí odkaz:
https://doaj.org/article/555c8210c6d24e4caf933833c437c654
Publikováno v:
Energies, Vol 17, Iss 15, p 3799 (2024)
The crucial issue of supervising and managing electrical energy in the context of aircraft electrification, known as More-Electric Aircraft (MEA), is addressed in this paper. In the pursuit of developing energy-efficient solutions with reduced enviro
Externí odkaz:
https://doaj.org/article/17f8def901a44172a293db494218c6df
Publikováno v:
Aerospace, Vol 11, Iss 7, p 585 (2024)
Electrification of aircraft is a very challenging task as the demand for energy and power is high. While the storage and generation of electrical energy are widely studied due to the limited specific energy and specific power of batteries and fuel ce
Externí odkaz:
https://doaj.org/article/50d97f617773438d9571a50c75ef9863
Publikováno v:
Aerospace, Vol 11, Iss 6, p 468 (2024)
In the last decades, electromechanical actuators started to be introduced in transport aircraft for primary and secondary flight control surfaces. Some innovative architectures have been proposed in the literature to use these actuators for high-lift
Externí odkaz:
https://doaj.org/article/25867ed9097246999200b49f4dc652fb