Aircraft nacelle including a rear frame inclined to the rear

An aircraft nacelle that comprises:

• a lip;
• an inside wall that delimits an inside pipe;
• a surface of the lip that is in contact with aerodynamic streams extends inside the nacelle by the inside wall that delimits the inside pipe;
• a junction zone that connects the inside pipe to a pipe of a power plant outside of the nacelle by an outside wall;
• a front frame that connects the inside wall and the outside wall, delimiting an annular pipe with the lip;
• a rear frame that connects the outside wall and the inside wall at the junction zone between the inside pipe and the pipe of the power plant;
• at least one opening to link zones that are located on either side of the rear frame, each opening comprising at least one door that is articulated relative to an edge of the opening, whereby said door is able to occupy a first state in which the door blocks the opening and another state in which the door clears the opening, and the zones are isolated by the rear frame except during maintenance;
• a point A corresponding to an intersection between the rear frame and the inside wall;
• and
• a point B corresponding to an intersection between the rear frame and the outside wall, wherein point A and point B line a plane that contains longitudinal axis of the nacelle, wherein the point B is offset toward the rear of the nacelle relative to the point A over more than 50% of a periphery of the rear frame.