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METHODS AND APPARATUS FOR STABILISHING AND AUGMETER SYSTEMS OF AIRCRAFT JET ENGINES
METHODS AND APPARATUS FOR STABILISHING AND AUGMETER SYSTEMS OF AIRCRAFT JET ENGINES
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机译:飞机喷气发动机稳定和增稳系统的方法和装置
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摘要
A turbine is stabilized in high speed, high altitude flight conditions by reducing the maximum augmenter fuel/air ratio in response to certain pressure and temperature conditions. Temperatures and pressures indicative of those at the combustor are sensed and the augmenter fuel schedule is accordingly modified to a level which provides reduced fuel/air ratios and stable burning conditions.
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