| 摘要 |
An aircraft turbo engine having non-ducted propellers provided with a gas generator and a receiver comprising a propulsion assembly carrying at least one propeller, comprising a first housing (27), a second housing (40) and a third housing (29), the third housing (29) being provided between the first and second housings (27, 40) and surrounding at least a portion of the gas generator, a reinforcing casing (50) having a first attachment area (52) mounted on the first housing (27), a second attachment area (60) mounted on the second housing (40), and a wall (70) provided between the first and second attachment areas (52, 60) and surrounding the third housing (29), in which the reinforcing casing (50) further comprises at least one section of pipe (71) incorporated into said wall (70). |
