Acoustic panels that include multi-layer facesheets

Patent metadata

Field	Value
Publication number	US-10720135-B2
Application number	US-201715434378-A
Country	US
Kind code	B2
Filing date	Feb 16, 2017
Priority date	Jul 18, 2016
Publication date	Jul 21, 2020
Grant date	Jul 21, 2020

Abstract

Systems and methods are provided for fabricating acoustic panels. One embodiment is a method comprising acquiring a core of acoustic cells, and fabricating a facesheet covering the core by: dispensing a base layer of material atop the acoustic cells while leaving openings into each of the acoustic cells, covering the openings by applying a liner of porous material atop the base layer, dispensing a cap layer of material atop liner while leaving gaps in the cap layer over the acoustic cells, and fusing the cap layer to the liner by directly radiating laser energy onto locations where the cap layer has been dispensed.

First claim

The invention claimed is:

1. A method comprising:
acquiring a core of acoustic cells; and
fabricating a facesheet covering the core by:
dispensing a base layer of material atop the acoustic cells while leaving openings into each of the acoustic cells;
covering the openings by applying a liner of porous material atop the base layer;
dispensing a cap layer of material atop the liner, wherein the cap layer is shaped in a repeating pattern that exhibits gaps over the acoustic cells, each gap being aligned with an opening defined in the base layer; and
fusing the cap layer to the liner by directly radiating laser energy solely onto the repeating pattern of the cap layer.

2. The method of claim 1 wherein:
fusing the cap layer to the liner further comprises fusing the liner to the base layer.

3. The method of claim 2 wherein:
the core of acoustic cells is thermoplastic; and
the method further comprises fusing the base layer to the core of acoustic cells by directly radiating laser energy onto locations where the base layer has been dispensed.

4. The method of claim 1 wherein:
fusing the cap layer comprises directly radiating laser energy only onto locations at which the cap layer overlaps the liner.

5. The method of claim 4 wherein:
fusing the cap layer causes the liner to become non-porous at locations where laser energy is directly applied.

6. The method of claim 1 wherein:
dispensing the cap layer forms the gaps such that a width of each gap parallel to expected airflow is less than a height of each gap perpendicular to expected airflow.

7. The method of claim 1 further comprising:
printing the base layer via three dimensional (3D) printing techniques.

8. The method of claim 1 further comprising:
printing the liner via three dimensional (3D) printing techniques.

9. The method of claim 1 wherein:
material for the base layer and the cap layer comprises Carbon Fiber Reinforced Polymer (CFRP) thermoplastic; and
material for the liner comprises thermoplastic.

Assignees

• Boeing Co

Inventors

• Herrera Eric

Classifications

• B29D24/005

  the structure having joined ribs, e.g. honeycomb · CPC title

• B29C70/382

  Automated fiber placement [AFP] · CPC title

• B64D33/02 Primary

  of combustion air intakes · CPC title

• G10K11/168 Primary

  Plural layers of different materials, e.g. sandwiches · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title