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An aircraft nacelle includes a cowling, an engine housed in an internal volume of the cowling, and at least one thrust reverser, an air passage duct being formed between an internal wall of the cowling and an external wall of the engine. The cowling includes a fixed cowling part and a moving cowling

An aircraft nacelle includes a cowling, an engine housed in an internal volume of the cowling, and at least one thrust reverser, an air passage duct being formed between an internal wall of the cowling and an external wall of the engine. The cowling includes a fixed cowling part and a moving cowling part that is translationally movable between a plurality of positions, at least one of the positions varying an air flow through the duct. The moving cowling part includes the at least one thrust reverser so that translational movement of the moving cowling part also allows the moving cowling part to switch from a position in which the at least one thrust reverser is retracted into a reverse-thrust position in which a bypass flow is deflected to generate a reverse thrust.

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1. An aircraft nacelle comprising: a cowling, an engine housed in an internal volume of the cowling, andat least one thrust reverser, an air passage duct being formed between an internal wall of the cowling and an external wall of the engine,the cowling comprises a fixed cowling part and a moving co

1. An aircraft nacelle comprising: a cowling, an engine housed in an internal volume of the cowling, andat least one thrust reverser, an air passage duct being formed between an internal wall of the cowling and an external wall of the engine,the cowling comprises a fixed cowling part and a moving cowling part that is translationally movable between a plurality of positions, at least one of the positions varying an air flow through the air passage duct, the moving cowling part comprising the at least one thrust reverser so that translational movement of the moving cowling part also allows the moving cowling part to switch from a position in which the at least one thrust reverser is retracted into a reverse-thrust position in which a bypass flow is deflected to generate a reverse thrust, the at least one thrust reverser comprising a pivoting door, the pivoting door comprises at least two extreme stable positions, a retracted position in which the pivoting door is incorporated into the cowling, and a reverse-thrust position in which a surface of the pivoting door that forms a part of an outer surface of the cowling in the retracted position is positioned partially inside and outside the nacelle to divert the bypass flow and to generate reverse thrust, the moving cowling part then being in a fully displaced position, whereinwhen the moving cowling part is in the at least one position that varies the air flow through the air passage duct, the at least one thrust reverser which comprises the pivoting door has a stable intermediate position in which a portion of the pivoting door that is positioned downstream in relation to a direction of travel of the bypass flow through the nacelle is positioned outside of the nacelle. 2. The nacelle according to claim 1, wherein, with the at least one thrust reverser comprising the pivoting door, an internal surface of the pivoting door has at least one curved portion to deflect the bypass flow in the reverse-thrust direction when the moving cowling part is in the reverse-thrust position. 3. The nacelle according to claim 1 or 2, wherein, with the at least one thrust reverser comprises a connecting member pivotally connecting the pivoting door to the external wall of the engine. 4. The nacelle according to claim 1, wherein the nacelle comprises an actuator allowing the moving cowling part to be moved in terms of translation between the plurality of positions. 5. The nacelle according to claim 1, wherein the nacelle comprises guide elements guiding the translational movement of the moving cowling part. 6. The nacelle according to claim 1, wherein the thrust reversers are formed in the moving cowling part, being positioned around a circumference of the nacelle. 7. The nacelle according to claim 6, wherein, with the thrust reversers being distributed non-continuously around the circumference, the nacelle comprises two groups of four of the pivoting doors, the pivoting doors being diametrically opposed in pairs. 8. An aircraft equipped with at least one nacelle according to claim 1. 9. The nacelle according to claim 1, wherein in the stable intermediate position a first path to direct at least part of the bypass flow outside of the nacelle is formed between a leading end of the pivoting door and the fixed cowling part, anda second path to direct at least part of the bypass flow outside of the nacelle is formed between a trailing end of the pivoting door and the moving cowling part.