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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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he 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 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 manu..................[:=> 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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newly developed elementary technologies to a six-cylinder engine in order to execute the development program for commercialization
3.1 Application of air-fuel ratio electronic-control system
In order to control the air-fuel ratio to an optimum range, it is necessary to control the flow rate of fuel gas and air. In the case of the newly developed Miller cycle gas engine, the air-fuel ratio electronic-control system was applied. The system calculates the required fuel gas feed rate on the basis of the temperature and pressure in the inlet manifold and the engine speed, and controls the gas fe..................[:=> 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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ration chamber and is longer; the TAL has conducting material lining the walls and is shorter.
3.3.3. Pulsed Inductive Thrusters
Imagine an electromagnet sitting on its end on a table. Now place a metal ring on top of it. Pulse current through the coil and a second current will be induced to flow through the ring. This induced current will flow around the ring in the direction opposite to the coil. We now have another case of a current (flowing in the ring) moving perpendicular to a magnetic field (created by the coil and directed along the coil's axis) so the Lorenz law tells us there will..................[:=> 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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a recognisable
growth roughly proportional to l1/4.
Fig. 17. Velocity of the signal propagation wa (approximately evaluated) in the feedback loop is near to the
speed of sound. In the high Reynolds number regime wa is constant”here seen to be practically
independent of the loop length l.
3.4. Constant propagation velocity regime
In this regime, the propagation velocity wa evaluated by the approximate Eq. (7) is
a constant not only independent of the flow rate through the valve (Fig. 17 and Fig. 18)
but also of the other varied parameter, the feedback loop length l (Fig. 17). The..................[:=> 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 i..................[:=> 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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ines 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 engine operates at leaner fuel levels, nitrogen emissions increase. Therefore, for lean burn engines to replace traditional fuel mixture engines, nitrogen oxide emission must be reduced. This can be done by catalyst or exhaust recirculation in the engine. However research continues to make lean burn engi..................[:=> 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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960s. Later in the 1970s NASA and Pratt and Whitney experimented with the first experimental FADEC, first flown on an F-111 fitted with 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 flo..................[:=> Show Contents <=:]



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