IP Library › Granted Patent US 11,034,460
Granted Patent B2
US 11,034,460 · App. 15/836,034 · Granted Jun 15, 2021

Additively manufactured septa for acoustic panels

Inventors: Zachary B. Renwick (Saint Louis, MO); Brandon L. Bertolucci (Seattle, WA); Eric Herrera (Mukilteo, WA); Michael William Hayes (Belleville, IL); John C. Waldrop, III (St. Peters, MO); Matthew Scott Thompson (Madison, AL)
Assignee: The Boeing Company
B64D33/02B29C64/106B29D99/0089B33Y10/00B33Y30/00B33Y80/00G10K11/168G10K11/172B29K2701/12B29L2007/002B32B2260/023B32B2307/10B32B2605/18B64D2033/0206B64D2033/0286
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Quick Facts
Patent No.
US 11,034,460
App. No.
15/836,034
Granted
Jun 15, 2021
Kind
B2
Abstract

Systems and methods are provided for septa for acoustic cells. One embodiment is a method that includes fabricating a septum of a cell of an acoustic panel, by heating a material into a molten material, depositing the molten material to form a lower chamber of the septum that extends vertically upwards and includes an entry, iteratively depositing layers of the molten material, each layer comprising a filament at the entry that includes overhangs with respect to vertically adjacent layers, and forming openings at locations of the overhangs.

Claims (49)

1. A method comprising:

fabricating a septum of a cell of an acoustic panel, by:

heating a material into a molten material;

depositing the molten material to form a lower chamber of the septum that extends vertically upwards and includes an entry;

subsequently iteratively depositing layers of the molten material atop the entry, each layer comprising a filament that includes overhangs with respect to vertically adjacent layers; and

forming openings at locations of the overhangs.

2. The method of claim 1 wherein:

iteratively depositing the layers comprises, for each layer, depositing a filament that extends beyond filaments of adjacent layers to form the overhangs.

3. The method of claim 1 wherein:

iteratively depositing the layers is performed such that each of the filaments is deposited as a multi-pointed star shape having vertices comprising recesses and protrusions, wherein recesses in each of the layers align with protrusions of vertically adjacent layers to form the openings.

4. The method of claim 3 further comprising:

drooping each protrusion downward after it is deposited.

5. The method of claim 1 wherein:

iteratively depositing the layers results in at least fifty layers, and

each layer forms at least ten openings with vertically adjacent layers.

6. The method of claim 1 wherein:

fabricating the septum is performed via fused filament fabrication.

7. The method of claim 1 wherein:

forming a seam at each layer, wherein seams of vertically adjacent layers are deposited atop each other.

8. The method of claim 1 wherein:

the openings have diameters between one ten thousandth of an inch and one thousandth of an inch in diameter.

9. The method of claim 1 further comprising:

depositing molten material to form a solid cap of material atop the layers.

10. The method of claim 1 further comprising:

depositing molten material to form a solid wall of material that surrounds the layers and forms an upper chamber of an acoustic cell.

11. The method of claim 1 wherein:

the molten material comprises thermoplastic.

12. A portion of an aircraft assembled according to the method of claim 1 .

13. A non-transitory computer readable medium embodying programmed instructions which, when executed by a processor, are operable for performing a method comprising:

fabricating a septum of a cell of an acoustic panel, by:

heating a material into a molten material;

depositing the molten material to form a lower chamber of the septum that extends vertically upwards and includes an entry;

subsequently iteratively depositing layers of the molten material atop the entry, each layer comprising a filament that includes overhangs with respect to vertically adjacent layers; and

forming openings at locations of the overhangs.

14. The medium of claim 13 wherein:

iteratively depositing the layers comprises, for each layer depositing a filament that extends beyond filaments of adjacent layers to form the overhangs.

15. The medium of claim 13 wherein:

iteratively depositing the layers is performed such that each of the filaments is deposited as a multi-pointed star shape having vertices comprising recesses and protrusions, wherein recesses in each of the layers align with protrusions of vertically adjacent layers to form the openings.

16. The medium of claim 15 wherein the method further comprises:

drooping each protrusion downward after it is deposited.

17. The medium of claim 13 wherein:

iteratively depositing the layers results in at least fifty layers, and

each layer forms at least ten openings with vertically adjacent layers.

18. The medium of claim 13 wherein:

fabricating the septum is performed via fused filament fabrication.

19. The medium of claim 13 wherein the method further comprises:

forming a seam at each layer, wherein seams of vertically adjacent layers are deposited atop each other.

20. The medium of claim 13 wherein:

the molten material comprises thermoplastic.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 8, 2017
From: HERRERA, ERIC; BERTOLUCCI, BRANDON L; RENWICK, ZACHARY B; HAYES, MICHAEL WILLIAM; WALDROP, JOHN C; THOMPSON, MATTHEW SCOTT
To: THE BOEING COMPANY
Reel/Frame 044340/0190 →
Continuity (1)
Related Publication 20190176998A1 · Jun 13, 2019