FIELD: transport.
SUBSTANCE: extending part 30 comprises downstream connection end 64 with hole made up of multiple angular sectors 76a, 76b to make annular groove 66 open radially outward to house nacelle covers.
EFFECT: simplified servicing.
11 cl, 10 dwg
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| DRIVE EQUIPPED WITH “NO BACK” SYSTEM WITH LOCKING ZONE | 2018 |
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| IMPROVED AIR-TIGHT SEALING DEVICE, MADE WITH THE POSSIBILITY OF INTRODUCTION BETWEEN THE ELEMENT OF THE HULL OF A DOUBLE-FLOW TURBINE ENGINE OF THE AIRCRAFT AND THE ELEMENT OF THE NACELLE | 2019 |
|
RU2798402C2 |
| NACELLE FOR BYPASS TURBOJET ENGINE | 2007 |
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RU2453477C2 |
