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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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b]Introduction

-The thermodynamic cycle analysis and the performance prediction of diesel engines using the engine cycle simulation programs has become an established part of the diesel engine research and development.
-Particularly ,the engine simulation programs based on the single-zone combustion model are widely used 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..................[:=> 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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cted the inlet valve close timing that provides the effective compression ratio of 11.
2.3. Improvement in combustion performance
In the case of a Miller cycle gas engine the combustion chamber volume at compression top dead center (TDC) is reduced because of the high expansion ratio. This causes the combustion efficiency to get reduced, nullifying the effect of high expansion ratio, and inversely reducing the efficiency. The major problem in this development program was tonsure combustion efficiency equivalent to or higher than that of a conventional gas engine at a smaller volumetric spac..................[:=> 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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, creating thrust, before it can dissipate into the vacuum of space.
Pulsed inductive thrusters are big, beautiful, sexy looking thrusters up to a meter in diameter. They operate in a pulsed mode at up to 1,000 pulses per second with specific impulses between 2,000 and 5,000 sec and thrusts of fractions of a pound to tens of pounds. Efficiencies can be as high as 50 percent.
Although the inductive coupling between the engine and plasma should imply that there is no erosion as there is in the MPD thruster, at high pulse rates the large surface area of the engine will be exposed to the thermal..................[:=> 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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re gain between its input control terminals X and the output terminals Y. The output flow is provided from the supplied steady flow, brought into the supply nozzle through the supply terminal S. In the present case, the fluidic amplifier valve is of the diverter type. The supplied flow is not turned down by the control action, but diverted into one of the two output terminals, Y1 and Y2. Each of them is connected to one of the two exit nozzles, A and B. The time-mean flow rate in each nozzle is positive: more flow issues in the outflow phase than is sucked in during the following inflow suctio..................[:=> 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 ..................[:=> 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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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 reach unburned hydrocarbon and carbon monoxide emission targets. The design features of lean burn engines can be improved with increased ..................[:=> 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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trol, thrust reversers control, engine health monitoring, oil debr..................[:=> Show Contents <=:]



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