Showing posts with label Flame stabilizing and general airflow pattern.. Show all posts
Showing posts with label Flame stabilizing and general airflow pattern.. Show all posts

Saturday, December 31, 2011

Apportioning the airflow - COMBUSTION PROCESS

COMBUSTION PROCESS
4. Air from the engine compressor enters the combustion chamber at a velocity up to 500 feet per second, but because at this velocity the air speed is far too high for combustion, the first thing that the chamber must do is to diffuse it, i.e. decelerate it and raise its static pressure. Since the speed of burning kerosine at normal mixture ratios is only a few feet  per second, any fuel lit even in the diffused airstream, which now has a velocity of about 80 feet persecond, would be blown away. A region of low axialvelocity has therefore to be created in the chamber,so that the flame will remain alight throughout therange of engine operating conditions.
Fig. 4-2 Apportioning the airflow.
5. In normal operation, the overall air/fuel ratio of a combustion chamber can vary between 45:1 and 130:1, However, kerosine will only burn efficiently at, or close to, a ratio of 15:1, so the fuel must be burned with only part of the air entering the chamber, in what is called a primary combustion zone. This is achieved by means of a flame tube (combustion liner) that ha various devices for metering the airflow distribution along the chamber.