| 摘要 |
<p>A turbojet engine nacelle comprising a thrust reversing device with doors, comprising inner walls on the sides of the opening. A turbojet engine nacelle comprising a thrust reversing device comprising doors (4) that swing to brake the direct gas flow, guiding it through counter-thrust openings (8), the inside of each door comprising, at the front, a cavity receiving a spoiler turned towards the front when this door is open, the fixed structure (2) upstream from each door (4) supporting a deflection edge (16) that partially covers the cavity, characterised in that the fixed structure (2) supports, on each side, counter-thrust openings (8), a flank (18) disposed in the continuation of the deflection edge (16) and extending behind the cavity, which is incorporated into a leaf of the door (4).</p> |
