Thrust reverser for use in downstream end of nacelle of turbojet engine of airplane, has secondary door arranged to swivel with respect to main doors on which secondary door is assembled between retracted position and blocking position
摘要
<p>The reverser (10) has an annular fixed structure (12) to form an external wall of an ejection channel (18). A secondary door (30) of the structure is arranged to swivel with main doors (22) on which the secondary door is assembled between a retracted position corresponding to a closed position of the main doors in which the secondary door is retracted inside the main door and a blocking position corresponding to a deployed position of the main doors in which the secondary door is deployed between downstream ends of the main doors.</p>
