DocumentCode
3357055
Title
Progress in electrically-propelled aircraft
Author
Colyer, R.E.
Author_Institution
Cranfield Univ., Swindon
fYear
2007
fDate
10-12 Sept. 2007
Firstpage
357
Lastpage
362
Abstract
In recent years, the performance of electrical drives and power sources has increased to an extent that they have now become viable as propulsion systems for aircraft. Whilst they are unlikely to be applicable to commercial airliners in the foreseeable future, a number of smaller aircraft are under development or have already been produced. The paper examines the advantages (and disadvantages) of the use of electric propulsion and compares an electric drive using currently available components with one employing a conventional internal combustion engine. It then considers a number of examples of aircraft using electrical propulsion and discusses their particular features. It is concluded that on weight and cost most electrical propulsion systems still cannot compete with conventional systems but other factors may override this disadvantage and further expected improvements in electrical system components should see them increasingly employed in the future.
Keywords
aerospace propulsion; electric drives; electric propulsion; electrical drives; electrically-propelled aircraft; internal combustion engine; propulsion systems; Aircraft propulsion; Batteries; Costs; Europe; Fuel cells; Fuel storage; Hydrogen; Internal combustion engines; NASA; Unmanned aerial vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
Electrical Machines and Power Electronics, 2007. ACEMP '07. International Aegean Conference on
Conference_Location
Bodrum
Print_ISBN
978-1-4244-0890-0
Electronic_ISBN
978-1-4244-0891-7
Type
conf
DOI
10.1109/ACEMP.2007.4510529
Filename
4510529
Link To Document