Method for manufacturing a structural and/or acoustic panel for a nacelle of an aircraft propulsion unit, and corresponding device

Patent metadata

Field	Value
Publication number	US-12109639-B2
Application number	US-202016870391-A
Country	US
Kind code	B2
Filing date	May 8, 2020
Priority date	Nov 8, 2017
Publication date	Oct 8, 2024
Grant date	Oct 8, 2024

Abstract

A method and a device for manufacturing a structural and/or acoustic panel for a nacelle of an aircraft propulsion assembly involves heating, by producing electromagnetic radiation, at least one skin of the structural and/or acoustic panel in such a way as to assemble this skin with a cellular structure of the structural and/or acoustic panel, by diffusion brazing or welding. This heating device can also be used to shape the skin to the cellular structure prior to assembly.

First claim

What is claimed is:

1. A method for manufacturing a structural and/or acoustic panel for a nacelle of an aircraft propulsion unit, the structural and/or acoustic panel comprising two metallic skins and a metallic cellular structure, the method comprising an arrangement of one of the two metallic skins, called a working skin, such that the working skin delimits a first volume and a second volume of an enclosure, and an arrangement of the metallic cellular structure within the second volume of the enclosure, wherein the method further comprises:
placing the working skin, which is not deformed at all, by pinching between pinch areas of the enclosure;
applying a gas pressure in the first volume of the enclosure so as to press and hold the working skin against the metallic cellular structure;
deforming the working skin in the enclosure by heating the working skin with electromagnetic radiation when the first volume of the enclosure is pressurized by a gas such that the working skin is deformed into a shape conforming to a shape of the metallic cellular structure, the heating by the electromagnetic radiation during the deforming being carried out by selectively heating the working skin from ends up to a center of the working skin so as to uniformize deformation of the working skin; and
heating the working skin by infrared electromagnetic radiation by a first heating device placed in the first volume of the enclosure so as to assemble the working skin to the metallic cellular structure by at least one of brazing and diffusion-welding.

2. The method according to claim 1 , further comprising a vacuuming of at least one of the first volume and the second volume of the enclosure using a pump.

3. The method according to claim 1 , further comprising providing infrared electromagnetic radiation by a second heating device to a tooling on which the other of the two metallic skins is disposed.

4. The method according to claim 3 , further comprising placing the second heating device in the second volume of the enclosure.

Assignees

• Safran Nacelles

Inventors

• Bienvenu Philippe
• Soula Aurélie
• Perrotin Thomas

Classifications

• B64D29/00 Primary

  Power-plant nacelles, fairings or cowlings · CPC title

• B64D27/16

  of jet type · CPC title

• B23K20/24

  Preliminary treatment · CPC title

• B23K20/021

  Isostatic pressure welding · CPC title

• B23K2101/006

  Vehicles · CPC title