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Thrust reverser for a turbojet engine nacelle comprising an end-of-travel stop on the primary guide rail
The present disclosure relates to a thrust reverser for a turbojet engine nacelle, including cowls that move backwards to open the thrust reverser. Each cowl includes a primary axial guide rail that receives most of the loads of the cowl, and secondary rails guiding an outer portion of each cowl. The thrust reverser includes a rear end stop for each cowl is arranged on the primary axial guide rails.
Thrust reverser for a turbojet engine nacelle comprising an end-of-travel stop on the primary guide rail
The present disclosure relates to a thrust reverser for a turbojet engine nacelle, including cowls that move backwards to open the thrust reverser. Each cowl includes a primary axial guide rail that receives most of the loads of the cowl, and secondary rails guiding an outer portion of each cowl. The thrust reverser includes a rear end stop for each cowl is arranged on the primary axial guide rails.
Thrust reverser for a turbojet engine nacelle comprising an end-of-travel stop on the primary guide rail
LONCLE ALEXIS (author)
2017-12-05
Patent
Electronic Resource
English
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