IP Library › Granted Patent US 12,030,274
Granted Patent B2
US 12,030,274 · App. 17/782,772 · Granted Jul 9, 2024

Article with 2D and 3D fiber structure

Inventors: Russell A. Ellis (Saratoga, CA); Jeffrey D. Haynes (Stuart, FL)
Assignee: AEROJET ROCKETDYNE, INC.
B32B1/08B32B5/10B32B5/12B32B9/007B32B2250/20B32B2262/105B32B2262/106B32B2262/12B32B2305/08B32B2305/18B32B2313/04B32B2315/02B32B2605/08
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Quick Facts
Patent No.
US 12,030,274
App. No.
17/782,772
Granted
Jul 9, 2024
Kind
B2
Abstract

An article includes a completed fabric structure that has multiple plies of fiber reinforced fabric. A first portion of the fabric structure has a three-directional fiber reinforced configuration and, exclusive of the first portion, a second portion of the fabric structure having a two-directional fiber reinforced configuration. In the three-directional fiber reinforced configuration there are multiple plies that are bound together via a matrix and a plurality of fibers normal through the multiple plies. In the two-directional fiber reinforced configuration the multiple plies are bound to one another via the matrix and not fibers normal through the multiple plies.

Claims (21)

1. An article comprising:

a completed fabric structure having multiple plies of fiber reinforced fabric;

a first portion of the fabric structure having a three-directional fiber reinforced configuration through which the multiple plies each having in-plane fibers, wherein the multiple plies are bound together via a matrix and are bound together by a plurality of fibers normal to the in-plane fibers and that extend through the multiple plies, wherein the first portion is an attachment portion for relatively high load-bearing, and in the three-directional fiber reinforced configuration the multiple plies and the fibers normal through the multiple plies together define a total fiber volume, and 10% to 25% of the total fiber volume are the fibers normal through the multiple plies; and

exclusive of the first portion, a second portion of the fabric structure having a two-directional fiber reinforced configuration through which the multiple plies are bound to one another via the matrix and not fibers normal through the multiple plies, wherein the second portion is a non-attachment portion that is relatively low load-bearing.

2. The article as recited in claim 1 , wherein the matrix is a carbon matrix.

3. The article as recited in claim 1 , wherein the completed fabric structure is axisymmetric.

4. The article as recited in claim 3 , wherein the completed fabric structure is conical.

5. The article as recited in claim 4 , wherein the attachment portion is an annular end portion of the completed fabric structure.

6. The article as recited in claim 1 , wherein the multiple plies are continuous through the first portion and the second portion.

7. The article as recited in claim 1 , wherein the multiple plies are silicon carbide fibers.

8. A vehicle comprising:

an engine; and

a nozzle attached to the engine, the nozzle having an axisymmetric body formed of a fiber-reinforced composite, the axisymmetric body including,

at least one attachment portion that is relatively highly load-bearing, and

adjacent to the at least one attachment portion, a non-attachment portion that is relatively low load-bearing,

the fiber-reinforced composite having a three-directional fiber reinforced configuration in the at least one attachment portion and a two-directional fiber reinforced configuration in the non-attachment portion, the three-directional fiber reinforced configuration including multiple plies each having in-plane fibers, wherein the multiple plies are bound together via a matrix and are bound together by a plurality of fibers normal to the in-plane fibers and that extend through the multiple plies, in the three-directional fiber reinforced configuration the in-plane fibers and the fibers normal through the in-plane fibers together define a total fiber volume, and 10% to 25% of the total fiber volume are the fibers normal through the in-plane fibers, and in the two-directional fiber reinforced configuration the multiple plies are bound to one another via the matrix and not fibers normal through the multiple plies.

9. The vehicle as recited in claim 8 , wherein the fiber-reinforced composite is continuous through the at least one attachment portion and the non-attachment portion, and the fiber-reinforced composite is selected from the group consisting of a carbon matrix/carbon fiber composite and a carbon matrix/silicon carbide fiber composite.

10. The vehicle as recited in claim 9 , wherein the non-attachment portion surrounds the attachment portion.

11. The article as recited in claim 1 , wherein the in-plane fibers lie an X-Y plane, and the plurality of fibers normal to the in-plane fibers are in a Z-direction that is orthogonal to the X-Y plane.

12. The article as recited in claim 1 , wherein the plurality of fibers normal to the in-plane fibers extend through two or more of the multiple plies.

13. The article as recited in claim 1 , wherein the plurality of fibers normal to the in-plane fibers extend through all of the multiple plies.

Assignments (3)
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 064423/0966 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Sep 28, 2022
From: AEROJET ROCKETDYNE, INC.
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 061561/0451 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 6, 2022
From: ELLIS, RUSSELL A.; HAYNES, JEFFREY D.
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 060109/0217 →
Continuity (1)
Related Publication 20230010439A1 · Jan 12, 2023