3 Patents
- US121349832024Process for Using an Air Input of a Turboreactor Nacelle Comprising an Air Input Lip Which Comprises a Portion Which Can Be Moved to Promote a Thrust Inversion Phase
SAFRAN AIRCRAFT ENGINES
0 cites - US117396882023Turbojet Comprising a Nacelle with an Air Intake for Promoting a Reverse Thrust Phase
Safran Aircraft Engines
0 cites - US116497652023Method for Operating an Air Intake of a Turbojet Engine Nacelle During a Thrust Phase and During a Reverse Thrust Phase
SAFRAN AIRCRAFT ENGINES
0 cites