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compressor stall
Fonte1
ASSOCIAÇÃO BRASILEIRA DE NORMAS TÉCNICAS. NBR 15971-4: aeronáutica – vocabulário – parte 4: propulsão aeronáutica. Rio de Janeiro, 2011. 44 p.
Nota adicional1
Reingestion stall: gas-turbine compressor stall induced by reingestion of hot gas during reverse-thrust mode.
Nota adicional2
Hung stall: after compressor stall, engine fails to recover immediately.
Contexto
In-flight ice affects jet engines differently than reciprocating engines. For the most part, the problems involve damage to rotating components or disruption of the airflow through the engine and accompanying engine stalls or stagnations. Structural ice which forms ahead of or in the inlets can be shed in slabs which, if they enter the engine, can cause damage to the engine and loss of thrust. In addition, if the slabs disrupt the airflow across the compressor face, compressor stall, which results in engine flameouts or stagnation, can also occur.
Subárea1
Engine
Português
estol do compressor