| 摘要 |
A tilting door (107) of a thrust reverser for the secondary flow of a double-flow jet engine comprises an outer panel (9), the outer surface of which is connected to the outer profile of the nacelle (4) and fixed rear part (3) of the reverser and an inner panel (111), the inner surface (111a) of which coincides, in direct thrust, with the theoretical surface delimiting the line of the secondary flow. Between the said inner panel (111) and outer panel (9) is formed a passage (20) having an orifice (21, 22) at each end on the inside of the door and, in the thrust reversal mode, forming a mini-nozzle via which passes part (15b) of the reversed flow (15a) of which it ensures the best possible deflection. …<IMAGE>… |
