DEVELOPMENT OF TURBOCHARGER CONTROL SYSTEM FOR WANKEL ENGINE
| Author(s) | : | Mr. Sundar Ganesh, C S, Mr. ThevagiriRajan, H |
| Institution | : | Assistant Professor, Dept of RAE, PSG College of Technology, Coimbatore, Tamil Nadu, India |
| Published In | : | Vol. 2, Issue 4 — April 2015 |
| Page No. | : | 512-517 |
| Domain | : | Engineering |
| Type | : | Research Paper |
| ISSN (Online) | : | 2348-4470 |
| ISSN (Print) | : | 2348-6406 |
The paper deals with the aspect of Development of Turbocharger Control Unit for Unmanned Aerial Vehiclewhich is running with Wankel Engine. The main aim of the work is to compensate the intake Pressure drop at high altitude asthis engine is operated there. This is done by controlling the boost pressure of turbo charger, Waste gate is used to controlthe amount of exhaust gases directed to the turbine wheel of the turbocharger. A closed loop turbocharger control system tocontrol waste gate in response to the pressure at inlet manifold is developed and tested in engine. The best suited InletManifold pressure is found using real time engine testing and from that the set point is found for every engine speed. Usingthat as a set point intake pressure, pressure is controlled using MC9S12B128 microcontroller. This Controlling of waste gatewill allow the engine not to lose its efficiency even at high altitude.
Mr. Sundar Ganesh, C S, Mr. ThevagiriRajan, H, “DEVELOPMENT OF TURBOCHARGER CONTROL SYSTEM FOR WANKEL ENGINE”, International Journal of Advance Engineering and Research Development (IJAERD), Vol. 2, Issue 4, pp. 512-517, April 2015.
