| 摘要 |
FIELD: transport.SUBSTANCE: invention relates to aircraft engineering, namely, to aircraft engine nacelle nose-over device. Said configuration if composed on one top semi-cowl 2 and one bottom semi-cowl 3 arranged in symmetry about said first semi-coal, both semi-cowl being locked in closed position by locks 8a, 8b. One of said semi-cowl, top 2 and bottom 3, can turn separately at distal edge 7d of pylon 7 so that, when open, access is allowed into both engine 4 and pylon central section 7b.EFFECT: easier access to in-pylon hardware.15 cl, 3 dwg |
