| 摘要 |
A bypass turbo jet thrust reverse includes obstacles formed of lower flaps 7 and upper flaps 8 of substantially equivalent size articulated to one another and deployed radially downstream of the nacelle 4 of the turbo jet. In the retracted position, the flaps 7 and 8 are withdrawn into the thickness of the primary cowling 2, the flap 8 of which forms again the internal wall of the bypass stream. <IMAGE>
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