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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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a heat addition process and the in-cylinder conditions are spatially uniform. as the heat release model, the well known wiebe’s combustion function and the white house-way’s heat release model were studied and successfully employed to the combustion simulation
- A comparison has been made between the predicted results of the cylinder pressure and rate of heat release and the measured data , and showed that the predictions agreed well with the measured data.

Introduction

-The thermodynamic cycle analysis and the performance prediction of diesel engines using..................[:=> 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 thermal efficiency of 42.2% (at a generating efficiency of 40%). We set up a target in our development program using simulation, etc. in order to raise the conventional engine thermal efficiency from 37% to 42.2%. The development program proceeded putting the target to getting the thermal efficiency improved by 3% or over by improving the theoretical cycle efficiency through the set expansion ratio/compression ratio, and the remaining 2.0% by improving the degree of constant volume of combustion and combustion efficiency and by reducing the heat loss and pumping loss
2.2 Setting of expans..................[:=> 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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l, only 0.001 millimeters across, capillary action both draws the liquid propellant into it and prevents it from exhausting into space; therefore a valve is not required.
FEEPs typically have specific impulses from 6,000 to 12,000 seconds and use melted indium as a propellant.
4. PROBLEMS WITH USING ELECTRIC PROPULSION FOR PRIMARY PROPULSION MISSIONS
First, multi-megawatt space power systems continue to be too heavy to make EP for primary propulsion attractive. Second, even with a multi-megawatt power supply the thrust provided by the highest thrust engines is only measured in tens of poun..................[:=> 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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) in terms of the flow transfer characteristic”the dependence of the relative output flow µY1 (Eq. (2) in the terminal Y1 on the relative control flow rate in the terminal X1):
(4)
which is first increasing and then decreasing, maintaining constant supply mass flow rate (and hence constant Reynolds number Re). The two exit nozzles issue into the same
space so that the pressure difference _PY between the amplifier outputs is constant and
equal to zero. In the state A, with at the beginning zero control flow and the supplied air
flow directed into the output terminal Y1 the c..................[:=> 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 informati..................[:=> 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&their ..................[:=> 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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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 compression ratio, mixture swirl, mixture preparation, and improved ignition. As en..................[:=> 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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addition to the fuel metering function, the FADEC performs numerous other control and monitoring functions such as Variable Stator Vanes (VSV's) and Variable Bleed Valves (VBV's) control, cabin bleeds and power off-takes control, control of starting and re-starting, turbine blade and vane cooling and blade tip clearance control, thrust reversers control, engine health monitoring, oil debris monitoring and vibration monitoring. The inputs come from various aircraft and engine sensors. Apart from the key parameters that are monitored for a safe thrust control (shaft rotational speeds, pressures..................[:=> Show Contents <=:]



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