IP Library Granted Patent US 10,427,330
Granted Patent B2
US 10,427,330 · App. 15/403,278 · Granted Oct 1, 2019

Hybrid lay-up mold

Inventors: Parme G. Anthony (Williams, AZ); Michael Fox (Brea, CA); Zachary Skelton (Laguna Hills, CA); Daniel Brennan (Fullerton, CA); Randel Dean Moruzzi, Jr. (Calimesa, CA)
Assignee: Ascent Aerospace, LLC
B29C33/3842B29C33/3807B29C66/712B29C66/729B29C66/7212B29C66/74283B29C70/342B29C70/44B29C70/542B29C70/86B23K2103/02B29C2033/385B29K2307/04B29K2705/12B29L2031/757
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Quick Facts
Patent No.
US 10,427,330
App. No.
15/403,278
Granted
Oct 1, 2019
Kind
B2
Abstract

A hybrid mold includes (a) an Invar® eggcrate structure, (b) an Invar® interim working surface and (c) a CF composite material overlay. The eggcrate and interim working surface are welded or otherwise connected together to form a unitary base mold. The CF overlay is bonded to the interim working surface. The CF overlay is easily reconfigurable and can be replaced without destroying the integrity of the base mold.

Claims (12)

1. A hybrid lay-up mold, comprising:

an iron-nickel eggcrate structure;

an iron-nickel alloy interim working surface secured to the eggcrate structure, the eggcrate structure and interim working surface cooperating to define a base mold;

a carbon fiber composite material overlay bonded to the interim structure; and

wherein the lay-up mold is free of any mechanical attachments, the eggcrate structure being fabricated from welded together header boards, and the interim working surface being welded and atop the eggcrate structure.

2. The lay-up mold of claim 1 wherein the iron-nickel alloy is selected from the group consisting of (a) an iron-nickel alloy having a 36% nickel content and (b) an iron-nickel alloy having a 41% nickel content.

3. The lay-up mold of claim 1 wherein the eggcrate structure and the interim working surface comprise the same iron-nickel alloy.

4. The lay-up mold of claim 1 wherein the interim working surface comprises a plurality of abutting thin sheets of the iron-nickel alloy, each abutment between the sheets defining a fully welded seam.

5. The lay-up mold of claim 1 wherein the carbon fiber material for the CF composite material overly overlay is selected from the group consisting of woven CF fabrics, chopped CF mats, CF unidirectional mats, CF unidirectional tapes, stitched CF multi-layer mats, and CF random orientation fabrics.

6. The lay-up mold of claim 5 wherein the CF composite material is selected from the group consisting of, pre-impregnated fabric systems, CF resin infused fabrics, sheet molding compounds, press molded composite materials, match or bladder molded composites, and wet laminated materials.

7. The lay-up mold of claim 6 wherein the CF composite material is an epoxy, benzoxazine, or BMI impregnated multi-layered woven cloth or chopped fiber mat.

8. The lay-up mold of claim 6 wherein the CF composite material is a pre-impregnated fabric, the impregnants being selected from the group consisting of phenolic resin, polyaryletherketone (PAEK), polyetheretherketone (PEEK), polyetherketone (PEK), BMI resins, PMR, epoxy resins, benzoxazine resins, cyanate esters, polyimides, acrylic resins, as well as mixtures thereof.

Assignments (1)
SECURITY AGREEMENT Recorded Oct 29, 2019
From: ASCENT AEROSPACE, LLC
To: ALLY BANK, AS AGENT
Reel/Frame 050865/0554 →
Continuity (2)
Provisional Application 62277264 · Jan 11, 2016
Related Publication 20170225362A1 · Aug 10, 2017