Anterior part of the nacelle of an aircraft propulsion assembly whose air intake lip is linked to the outer panel by nesting
An anterior part of an aircraft propulsion assembly nacelle, having an air intake lip disposed at a front end and an outer panel, of which an outer face extends an outer part of the air intake lip. A front edge of the outer panel and a rear edge of the air intake lip are shaped so as to overlap radially and to nest so as to ensure a continuous surface between the outer surface of the outer part of the air intake lip and the outer face of the outer panel. Moreover, the front edge of the outer panel is connected to the rear edge of the air intake lip with no added rigid element. This permits a rigid connection while avoiding creating local irregularities on the outer surface of the nacelle, which irregularities might disrupt the flow of air around the nacelle, giving rise to additional drag.
1. An anterior part of a nacelle of an aircraft propulsion assembly, said anterior part having a front end allowing air to enter and a rear end configured to be connected to a remainder of the nacelle, said anterior part comprising:
an air intake lip disposed at said front end,
an outer panel, an outer face of which extends an outer part of the air intake lip, a front edge of the outer panel being connected to a rear edge of the air intake lip,
wherein the front edge of the outer panel and the rear edge of the air intake lip are shaped so as to overlap radially and nest so as to ensure a continuous surface between an outer surface of the outer part of the air intake lip and the outer face of the outer panel, and
wherein the front edge of the outer panel is connected to the rear edge of the air intake lip with no added rigid element fully penetrating said front edge of the outer panel and the rear edge of the air intake lip,
wherein one of the outer panel and the air intake lip rear has an opening in which the other of the outer panel edge and the air intake lip resides.
2. The nacelle anterior part according to claim 1 , in which the rear edge of the air intake lip has a thinned section that reduces in thickness progressively to an end of the thinned section.
3. The nacelle anterior part according to claim 1 , in which the front edge of the outer panel is connected to the rear edge of the air intake lip using a glue.
4. The nacelle anterior part according to claim 1 , in which the front edge of the outer panel is connected to the rear edge of the air intake lip by welding or soldering.
5. The nacelle anterior part according to claim 1 , in which
the outer panel is formed of a composite material and in which the front edge of said outer panel is formed directly on the rear edge of the air intake lip, or
the air intake lip is formed of a composite material and in which the rear edge of said air intake lip is formed directly on the front edge of the outer panel.
6. The nacelle anterior part according to claim 1 , in which either the rear edge of the air intake lip or the front edge of the outer panel comprises radially projecting parts that are captively held in the other of the front edge of the outer panel and the rear edge of the air intake lip.
7. The nacelle anterior part according to claim 1 , in which the front edge of the outer panel radially surrounds the rear edge of the air intake lip.
8. The nacelle anterior part according to claim 1 , in which the rear edge of the air intake lip radially surrounds the front edge of the outer panel.
9. The nacelle anterior part according to claim 1 , comprising a surface coating formed straddling the outer face of the outer panel and the outer part of the air intake lip.
10. The nacelle anterior part according to claim 1 , wherein the lip and outer panel being made of metal and a contacting surface between the lip and outer panel is roughened.
11. A nacelle of an aircraft propulsion unit, comprising an anterior part according to claim 1 .
12. An anterior part of a nacelle of an aircraft propulsion assembly, said anterior part having a front end allowing air to enter and a rear end configured to be connected to a remainder of the nacelle, said anterior part comprising:
an air intake lip disposed at said front end,
an outer panel, an outer face of which extends an outer part of the air intake lip, a front edge of the outer panel being connected to a rear edge of the air intake lip,
wherein the front edge of the outer panel and the rear edge of the air intake lip are shaped so as to overlap radially and nest so as to ensure a continuous surface between an outer surface of the outer part of the air intake lip and the outer face of the outer panel, and
wherein the front edge of the outer panel is connected to the rear edge of the air intake lip with no added rigid element fully penetrating said front edge of the outer panel and the rear edge of the air intake lip,
wherein either the rear edge of the air intake lip or the front edge of the outer panel comprises radial openings that are filled with the other of the front edge of the outer panel and the rear edge of the air intake lip.
13. The nacelle anterior part according to claim 12 , in which that one of the front edge of the outer panel and the rear edge of the air intake lip that fills the radial openings is formed of a composite material, and comprises plies of composite materials that fill said radial openings and are distinct from the other plies constituting said outer panel or said air intake lip.