IP Library Granted Patent US 11,766,828
Granted Patent B2
US 11,766,828 · App. 16/929,195 · Granted Sep 26, 2023

Method of manufacturing folded structure with additive features

Inventor: Randall Ray West (Wichita, KS)
Assignee: SPIRIT AEROSYSTEMS, INC.
B29C64/188B21D39/028F02C7/20F16B5/00B21D5/16B33Y10/00F05D2230/232F05D2230/31
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Quick Facts
Patent No.
US 11,766,828
App. No.
16/929,195
Granted
Sep 26, 2023
Kind
B2
Abstract

A method of manufacturing a multi-sided or otherwise relatively three-dimensional formed structure for, e.g., an aerospace vehicle. A relatively planar base structure is constructed using a first construction technique. Features (e.g., ribs) are incorporated into the base structure using a second construction technique (e.g., additive or subtractive manufacturing) to create an intermediate structure. The intermediate structure is folded along fold-lines or otherwise physically formed to create the formed structure, such that some of the features are located within an internal space defined by the formed structure. Joints between the sides of the formed structure are welded, fastened, or otherwise secured. Separately constructed additional elements (e.g., bulkheads) may be incorporated into the structure. A closeout element may be added to the formed structure to further define and close the internal space. Throughout the process, the structures, features, and elements may be refined to desired tolerances.

Claims (11)

1. A method of manufacturing a multi-sided formed engine pylon structure which is a component of an aerospace vehicle, the method comprising:

constructing a base structure using a first construction technique;

creating one or more fold lines of reduced cross-sectional thickness in the base structure;

incorporating one or more additional features into the base structure using an additive manufacturing technique to create an intermediate structure, wherein the one or more additional features include one or more stiffening ribs configured to physically stiffen the multi-sided formed engine pylon structure;

refining to a tolerance an area of the intermediate structure which will be located within an internal space defined by the multi-sided formed engine pylon structure;

folding the intermediate structure along the one or more fold lines of reduced cross-sectional thickness to create the multi-sided formed engine pylon structure having two or more sides, wherein at least one of the one or more additional features is located within the internal space defined by the multi-sided formed engine pylon structure;

welding along the one or more fold lines between the two or more sides of the multi-sided formed engine pylon structure; and

incorporating a closeout element into the multi-sided formed engine pylon structure, wherein the closeout element further defines and closes the internal space.

2. The method of claim 1 , wherein the base structure is constructed from wrought plate metal and comprises one or more thicker areas associated with one or more attachment points of the multi-sided formed engine pylon structure.

3. The method of claim 1 , further including incorporating one or more separately constructed additional elements into the intermediate structure prior to forming or into the multi-sided formed engine pylon structure after forming.

4. The method of claim 3 , wherein the one or more separately constructed additional elements include a bulkhead extending across the internal space.

Assignments (12)
RELEASE OF SECURITY INTEREST Recorded Dec 11, 2025
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073932/0669 →
RELEASE OF SECURITY INTEREST Recorded Dec 10, 2025
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073900/0356 →
RELEASE OF SECURITY INTEREST Recorded Dec 9, 2025
From: MORGAN STANLEY SENIOR FUNDING, INC., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073916/0346 →
SECURITY AGREEMENT Recorded Jul 8, 2024
From: SPIRIT AEROSYSTEMS, INC.
To: MORGAN STANLEY SENIOR FUNDING, INC.
Reel/Frame 068217/0456 →
RELEASE OF SECURITY INTEREST Recorded Dec 4, 2023
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
To: SPIRIT AEROSYSTEMS, INC.; SPIRIT AEROSYSTEMS HOLDINGS, INC.; SPIRIT AEROSYSTEMS NORTH CAROLINA, INC.
Reel/Frame 065757/0074 →
SECURITY AGREEMENT (SECOND LIEN NOTES) Recorded Nov 21, 2023
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
Reel/Frame 065659/0585 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Nov 23, 2022
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 061993/0847 →
RELEASE OF SECURITY INTEREST Recorded Nov 23, 2022
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 061995/0281 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 053993/0569 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A.
Reel/Frame 053983/0350 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 053978/0149 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 4, 2020
From: WEST, RANDALL RAY
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 053398/0593 →
Continuity (1)
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