Aviation Dictionary
کمپرسور ترکیبی ،کمپرسوری که متشکل از دور ردیف پره یکی از نوع گریز از مرکز و دیگری خطی باشد
A type of gas turbine engine compressor which has both an axial-flow and a centrifugal stage. Inlet air first passes through the low-pressure axial-flow compressor and then flows into the high-pressure centrifugal compressor. The centrifugal compressor builds up the pressure of the air high enough for efficient operation in the combustors.