DocumentCode :
518400
Title :
Notice of Retraction
Automatic thrust augmentation
Author :
Balaji, S. ; Dinesh, M. ; Raj, N Dileep
Author_Institution :
Aeronaut. Eng. Dept., Rajalakshmi Eng. Coll., Chennai, India
Volume :
5
fYear :
2010
fDate :
16-18 April 2010
Abstract :
Notice of Retraction

After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.

We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.

The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.

The automatic thrust augmentation is the method of powering a high speed aircraft with the objective of minimizing the fuel consumption and making use of the atmospheric air in collecting the propellant. The automatic thrust augmentation is a system that can be used in assisting the main engine in order to provide thrust during critical situations which includes crossing the sonic region, during air combat, taking off from an aircraft carrier and so on. This method of thrust augmentation includes making use of the atmospheric air in collecting the propellant (oxidizer) and mixing it with the aircraft´s fuel for the combustion to take place. Also, these processes occur automatically without pilots´ effort which also increases accuracy and relieves pilot´s stress. Since we are collecting the propellant from atmosphere, we can minimise fuel consumption significantly, and further research in this can lead to many other developments in aerospace field. We have given a conceptual idea on extracting the propellant from atmosphere and on providing automatic thrust augmentation.
Keywords :
aerospace engines; aerospace propulsion; aerospace field; aircraft carrier; automatic thrust augmentation; engine; high speed aircraft; Aircraft propulsion; Atmosphere; Combustion; Cryogenics; Engines; Fuels; Level control; Magnetic liquids; Oxygen; Refrigeration; minimising fuel consumption; propellant extraction from atmosphere; thrust augmentation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computer Engineering and Technology (ICCET), 2010 2nd International Conference on
Conference_Location :
Chengdu
Print_ISBN :
978-1-4244-6347-3
Type :
conf
DOI :
10.1109/ICCET.2010.5486136
Filename :
5486136
Link To Document :
بازگشت