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M-COMBUSTION CHAMBER AND COLD STARTING OF CI ENGIINES


Posted by: seminar surveyer
Created at: Friday 08th of October 2010 03:27:26 AM
Last Edited Or Replied at :Friday 08th of October 2010 03:27:26 AM
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sed by most engine manufacturers because of simplicity and low operating cost in spite of their short comings in accuracy.
-These programs can readily utilized for the prediction of cylinder firing pressure for the stress analysis of main engine parts, investigation of engine ..................[:=> Show Contents <=:]



High Efficiency Miller Cycle Gas Engine full report


Posted by: project report tiger
Created at: Tuesday 16th of February 2010 09:43:19 AM
Last Edited Or Replied at :Tuesday 12th of October 2010 02:44:54 AM
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A turbocharger with low efficiency causes the exhaust pressure to rise and thereby the pump loss to increase, no matter how high the engine cylinder cycle efficiency is. The thermal efficiency consequently does not improve. In other words, a high efficiency supercharging system is indispensable to a Miller cycle engine.
We, therefore, developed a turbocharger optimized for Miller cycle. This was done optimizing the turbine and compressor component elements to obtain higher efficiency. A new type 3-dimensional blade with inner and exit flow loss reduced was adopted for the turbine while the n..................[:=> Show Contents <=:]



chemical rocket engine full report


Posted by: project report tiger
Created at: Tuesday 16th of February 2010 09:22:03 AM
Last Edited Or Replied at :Tuesday 16th of February 2010 09:22:03 AM
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FIGURE 3.9. DIAGRAM OF A HALL THRUSTER
Electromagnets around the outside cylinder and inside core create a magnetic field pointing radically inward. The interplay of this magnetic field and the electric field between the anode propellant injectors and the electron cloud created outside of the thruster causes a current (called the Hall current) to be induced to flow azimuthally around the open annulus in the thruster. The magnetic field pushes on the current and accelerates it, and the gas it's traveling through, out of the thruster to create thrust.
Typical thrusters in U..................[:=> Show Contents <=:]



NO-MOVING-PART HYBRID-SYNTHETIC JET ACTUATOR full report


Posted by: project report tiger
Created at: Sunday 14th of February 2010 08:07:42 PM
Last Edited Or Replied at :Sunday 14th of February 2010 08:07:42 PM
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w phase than is sucked in during the following inflow suction phase of the cycle. The actuator drives not a single nozzle but two nozzles operating in opposing phases“suction in nozzle A is simultaneous with outflow from the other nozzle B. Availability of two phase-shifted exit flows is an advantage for some applications.
Fig. 2. Schematic representation of the fluidic oscillator: a jet-deflection diverter type fluidic bistable
amplifier is provided with feedback loop connecting the two control terminals X1 and X2. Black triangles:
nozzles, white triangles: diffusers.
The oscillati..................[:=> Show Contents <=:]



smartcombustor


Posted by: vinayaka
Created at: Monday 08th of February 2010 11:01:00 PM
Last Edited Or Replied at :Wednesday 10th of February 2010 12:04:38 AM
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sir, will you please give me information on smartcombu..................[:=> Show Contents <=:]



ppt on rocket engine and their propelants


Posted by: l.chandrikarani
Created at: Saturday 02nd of January 2010 11:23:42 AM
Last Edited Or Replied at :Thursday 16th of February 2012 07:41:10 AM
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send this ppt about rocket engine&thei..................[:=> Show Contents <=:]



Lean Burn Spark Ignition Engine


Posted by: computer science crazy
Created at: Tuesday 07th of April 2009 10:56:31 AM
Last Edited Or Replied at :Thursday 22nd of August 2013 12:23:44 AM
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unt of atmospheric pollution caused by it has been a major concern in automobile industry. Thus the need to conserve this non renewable petrol and yet meet the needs of booming automobile industry led to the birth of a new advanced engine -Lean Burn Spark Ignition Engine. The ratio of air to fuel in a spark ignition engine is on average 14.7:1. With the diminishing oil reserves and tightened legislations, fuel consumption and exhaust emission of spark ignition engines is to be reduced. The efficiency of lean burn engines is high due to the usage of higher air fuel ratio. Lean burn engine can r..................[:=> Show Contents <=:]



FADEC - Full Authority Digital Engine Control


Posted by: computer science crazy
Created at: Saturday 20th of September 2008 12:15:06 PM
Last Edited Or Replied at :Saturday 20th of September 2008 12:15:06 PM
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th a highly modified Pratt & Whitney TF-30 left engine. The experiments led to Pratt & Whitney F100 and Pratt & Whitney PW2000 being the first military and civil engines respectively fitted with FADEC and later the Pratt & Whitney PW4000 as the first commercial 'Dual FADEC' engine.

The aircraft's thrust lever sends electrical signals (pilot's command, may also be the autothrottle) to the FADEC. The FADEC digitally calculates and precisely controls the fuel flow rate to the engines giving precise thrust. In addition to the fuel metering function, the FADEC performs numerous other control and..................[:=> Show Contents <=:]



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