US2014119904A1PendingUtilityA1
In-situ pressure enhanced processing of composite articles
Est. expiryNov 1, 2032(~6.3 yrs left)· nominal 20-yr term from priority
F04D 29/023B29K 2995/0037B29C 70/446B29C 45/02Y10T156/10F04D 29/526F05D 2300/20F01D 5/005F05D 2300/43B29L 2031/7504B29K 2063/00F02C 7/04F05D 2300/603B29K 2313/00Y02T50/60F05D 2300/702B29C 70/36B29C 70/347B29K 2307/04
48
PatentIndex Score
0
Cited by
0
References
0
Claims
Abstract
A method for making a composite article comprises securing a layup over a form. The layup including a plurality of dry intermediate reinforcement plies wrapped around an inner reinforcement ply. Resin is infused into the layup under vacuum. The resin-infused layup is consolidated under pressure and cured.
Claims
exact text as granted — not AI-modified1 . A method for making a composite article, the method comprising:
securing a layup over a form, the layup including a plurality of dry intermediate reinforcement plies wrapped around an inner reinforcement ply; infusing resin into the layup under vacuum; consolidating the resin-infused layup under pressure; and curing the consolidated layup.
2 . The method of claim 1 , wherein the plurality of dry intermediate reinforcement plies are wrapped in tension.
3 . The method of claim 1 , wherein each of the plurality of dry intermediate reinforcement plies includes a fabric composition selected from one or more of: carbon, fiberglass, silicon carbide, aramid, and glass.
4 . The method of claim 1 , wherein a fabric composition of the inner reinforcement ply is the same as a fabric composition of at least one of the dry intermediate reinforcement plies.
5 . The method of claim 1 , wherein the securing step includes adhesively bonding the inner reinforcement ply to the form.
6 . The method of claim 1 , wherein the inner reinforcement ply comprises a pre-impregnated fabric.
7 . The method of claim 1 , wherein the infusing step is performed with a longitudinal axis of the layup and the form arranged in a substantially vertical orientation.
8 . The method of claim 1 , wherein at least one of the consolidation step and the curing step is performed with a longitudinal axis of the layup and the form arranged in a substantially horizontal orientation.
9 . The method of claim 1 , wherein the consolidation step is performed at an applied pressure measuring between about 100 psig (about 690 kPa) and about 150 psig (about 1030 kPa).
10 . The method of claim 1 , wherein the resin comprises a thermoset polymer resin.
11 . The method of claim 1 , wherein the infusing step is performed at a first infusion temperature, and the consolidation step is performed at a first consolidation temperature, the first consolidation temperature greater than the first infusion temperature.
12 . The method of claim 1 , wherein the composite article is a finished fan containment case having a fiber volume of at least about 60%.
13 . A method for making a composite article, the method comprising:
securing an inner reinforcement ply over a form to define an inner surface of the article; wrapping a plurality of dry intermediate reinforcement plies under tension over the inner reinforcement ply; vacuum infusing resin into the reinforcement plies to form a resin-infused layup; consolidating the resin-infused layup under pressure; and curing the consolidated layup.
14 . The method of claim 13 , wherein the inner reinforcement ply is adhesively bonded to the tool.
15 . The method of claim 13 , wherein a fabric composition of the inner reinforcement ply is the same as a fabric composition of at least one of the plurality of dry intermediate reinforcement plies.
16 . The method of claim 13 , wherein the plurality of dry reinforcement plies includes a fabric composition selected from one of: carbon, fiberglass, silicon carbide, aramid, and glass.
17 . The method of claim 13 , wherein the resin comprises a thermoset polymer selected from the group consisting of: an epoxy resin, a bismaleimide resin, and a polyimide resin.
18 . The method of claim 13 , wherein at least one of the consolidation step and the curing step is performed with a longitudinal axis of the resin-infused layup in a horizontal orientation.
19 . The method of claim 13 , wherein the consolidation step is performed at an applied pressure measuring between about 100 psig (about 690 kPa) and about 150 psig (about 1030 kPa).
20 . A composite fan containment case made according to the method of claim 13 .Join the waitlist — get patent alerts
Track US2014119904A1 — get alerts on status changes and closely related new filings.
We store only your email — no account needed. See our privacy policy.