A propulsion system is provided for an aircraft. This aircraft propulsion system includes an engine housing, an open propulsor rotor, an engine core and a thrust diversion system. The open propulsor rotor is outside of the engine housing. The engine core is within the engine housing and motively coupled to the open propulsor rotor. The thrust diversion system is configured with the engine housing. The thrust diversion system includes a door configured to move radially from a stowed position to a deployed position.

A thrust reverser (30) for an aircraft propulsion unit, the reverser comprising a stationary structure (31) and a movable structure (29) comprising at least one movable reverser cover (33) delimiting the secondary flow path (21B), the movable structure being translatable with respect to the stationary structure between an advanced direct-thrust position and a retracted thrust-reversal position in which the movable structure (29) and the stationary structure (31) axially define therebetween, on the secondary flow path, a radial extraction opening (56) for at least one portion (20B) of the secondary flow. The thrust reverser also comprises at least one deployable deflecting membrane (32, 32) which is designed to deflect the at least one portion (20B) of the secondary flow forwards. Moreover, in the deployed configuration, the membrane (32, 32) extends radially outwards beyond the movable reverser cover (33).

A thrust reverser (30) for an aircraft propulsion unit, the reverser comprising a stationary structure (31) and a movable structure (29) comprising at least one movable reverser cover (33) delimiting the secondary flow path (21B), the movable structure being translatable with respect to the stationary structure between an advanced direct-thrust position and a retracted thrust-reversal position in which the movable structure (29) and the stationary structure (31) axially define therebetween, on the secondary flow path, a radial extraction opening (56) for at least one portion (20B) of the secondary flow. The thrust reverser also comprises at least one deployable deflecting membrane (32, 32) which is designed to deflect the at least one portion (20B) of the secondary flow forwards. Moreover, in the deployed configuration, the membrane (32, 32) extends radially outwards beyond the movable reverser cover (33).

A thrust reverser (30) for an aircraft propulsion unit, the reverser comprising a stationary structure (31) and a movable structure (29) comprising at least one movable reverser cover (33) delimiting the secondary flow path (21B), the movable structure being translatable with respect to the stationary structure between an advanced direct-thrust position and a retracted thrust-reversal position in which the movable structure (29) and the stationary structure (31) axially define therebetween, on the secondary flow path, a radial extraction opening (56) for at least one portion (20B) of the secondary flow. The thrust reverser also comprises at least one deployable deflecting membrane (32, 32) which is designed to deflect the at least one portion (20B) of the secondary flow forwards. Moreover, in the deployed configuration, the membrane (32, 32) extends radially outwards beyond the movable reverser cover (33).

A thrust reverser (30) for an aircraft propulsion unit, the reverser comprising a stationary structure (31) and a movable structure (29) comprising at least one movable reverser cover (33) delimiting the secondary flow path (21B), the movable structure being translatable with respect to the stationary structure between an advanced direct-thrust position and a retracted thrust-reversal position in which the movable structure (29) and the stationary structure (31) axially define therebetween, on the secondary flow path, a radial extraction opening (56) for at least one portion (20B) of the secondary flow. The thrust reverser also comprises at least one deployable deflecting membrane (32, 32) which is designed to deflect the at least one portion (20B) of the secondary flow forwards. Moreover, in the deployed configuration, the membrane (32, 32) extends radially outwards beyond the movable reverser cover (33).