Call For Paper Volume:6 Issue:11 Nov'2019 |

A model cascade thrust reverser designed by changing outlet vane angle and declining cascade towards engine centre line.

Publication Date : 28/06/2017


DOI : 10.21884/IJMTER.2017.4193.GILOE

Author(s) :

Patel Bhavik Narsinhbhai , Dalwala Parth , Patel Darshan , Modh Mihirkumar.


Volume/Issue :
Volume 4
,
Issue 6
(06 - 2017)



Abstract :

A thrust reverser uses for fan jet type aircraft gas turbine engine. A nacelle assembly for the turbofan engine includes a translatable sleeve and blocker in such way that the air flow in the bypass duct is directed out the cascade assembly. The paper is aimed to increase the performance of conventional cascade assembly with two alternative designs and achieved by calculating Thrust Reverser of the prototype which is designed on Solidworks and parts are 3-D printed.


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A model cascade thrust reverser designed by changing outlet vane angle and declining cascade towards engine centre line.

June 24, 2017