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Grid for thrust reverser system of ducted-fan turbine engine i.e. jet engine, of aircraft, has two modules for respectively holding two opposite vanes at two ends of two supports, where grid is telescopic and extensible
Grid for thrust reverser system of ducted-fan turbine engine i.e. jet engine, of aircraft, has two modules for respectively holding two opposite vanes at two ends of two supports, where grid is telescopic and extensible
The grid (108) has two modules (30) respectively holding two opposite vanes at two ends of two supports, where the grid is telescopic and extensible. The modules are moved and slidingly assembled with respect to each other. A rail is cooperated with the support. An independent claim is also included for a thrust reverser system for a turbomachine of an aircraft, including a grid.
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