Patent ID: 11878809
Assignee: AIRBUS OPERATIONS S.L.
Field: Transport (Mechanical engineering)
Classification: CPC B  F | IPC B  F

Claim 2:
3. The aircraft propulsion assembly as claimed in claim 1, wherein the first engine comprises a first gas ejection nozzle and the second engine comprises a second gas ejection nozzle, and
wherein the first gas ejection nozzle and the second gas ejection nozzle each have an outlet section, defined by an outer wall of the corresponding one of the first and second gas ejection nozzles, of which a portion is straight,
the propulsion assembly being configured such that the straight portion of the outlet section of the first gas ejection nozzle and the straight portion of the outlet section of the second gas ejection nozzle are facing one another on either side of a median plane of symmetry of the propulsion assembly, in contact with one another, or form a wall common to said first and second gas ejection nozzles at said median plane of symmetry of the propulsion assembly.