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Steam Jet vaccum ejector


Posted by: seminar class
Created at: Saturday 12th of March 2011 05:23:25 AM
Last Edited Or Replied at :Tuesday 05th of April 2011 06:35:58 AM
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rs, pistons or other moving parts, it is a relatively low-cost component is easy to operate and requires relatively little maintenance.
In a steam-jet ejector, the suction chamber is connected to the vessel or pipeline that is to be evacuated under vacuum. The gas that is to be induced into the suction chamber can be any fluid that is compatible with the steam and the components materials of construction.
The steam nozzle discharges a high-velocity jet across the suction chamber. This steam jet creates a vacuum which extracts air or gas from the adjoining vessel. As these gases are entrained..................[:=> Show Contents <=:]



Vortex refrigeration


Posted by: summer project pal
Created at: Sunday 09th of January 2011 07:07:54 PM
Last Edited Or Replied at :Sunday 09th of January 2011 07:07:54 PM
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y (as r − 2 ) as the center line is approached.
The tangential velocity is given by:
(2.1)
where Γ is the circulation and r is the radial distance from the center of the vortex.
In non-technical terms the circular streamlines toward the center can sweep out a given angle faster than the outer streamlines. The speed along the circular path of flow is held constant or decreases as you move out from the center. At the same time the inner streamlines have a shorter distance to travel to complete a ring. If you were running a race on a circular track would you rather be on..................[:=> Show Contents <=:]



TURBOFAN ENGINES


Posted by: summer project pal
Created at: Saturday 08th of January 2011 12:40:23 PM
Last Edited Or Replied at :Tuesday 26th of April 2011 05:58:55 AM
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gine to improve the aircraft takeoff, climb and (for military aircraft) combat performance. Afterburning consists of the introduction and burning of raw fuel between the engine turbine and the jet pipe propelling nozzle, utilizing the unburned oxygen in the exhaust gas to support combustion. The increase in the temperature of the exhaust gas increases the velocity of the jet leaving the propelling nozzle and therefore increases the engine thrust. This increased thrust could be obtained by the use of a larger engine, but this would increase the weigh and overall fuel consumption. In other words..................[:=> Show Contents <=:]



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