AIRCRAFT ENGINE HAVING AT LEAST ONE REVERSE THRUST SYSTEM ACTUATOR ARRANGED IN A GAS EXHAUST CONE
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United States of America Patent
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Issued Date -
Nov 29, 2018
app pub date -
May 21, 2018
filing date -
May 21, 2018
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Abstract
To reduce the size of an aircraft engine, an assembly is disclosed including a nacelle section, a gas exhaust cone positioned radially towards the inside in relation to the nacelle section and forming therewith an annular gas exhaust channel, and a reverse thrust system including moveable gas diversion elements for the gas flowing in the annular channel, at least one actuator and a transmission device linking the at least one actuator to the moveable gas diversion elements. Furthermore, the actuator is located inside the gas exhaust cone.
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