Apparatus for manufacturing constant velocity joint boot and method of manufacturing the same
US-2015360405-A1 · Dec 17, 2015 · US
US9669570B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9669570-B2 |
| Application number | US-201214116068-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 2, 2012 |
| Priority date | May 6, 2011 |
| Publication date | Jun 6, 2017 |
| Grant date | Jun 6, 2017 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A method of injection molding a part made of composite material is provided. The method includes placing a preform in a mold; injecting a resin into the mold so as to impregnate the preform; unmolding the part after curing the resin; and subjecting the resin and the preform to pressure inside the mold while the resin is curing.
Opening claim text (preview).
The invention claimed is: 1. A method of injection molding a blade comprising a composite material, the method comprising: placing a blade fiber preform in a mold, the blade fiber preform being formed by weaving yarns and including a root portion having a first planar sloping face, a second planar sloping face, and a bottom planar face between the first and second sloping faces in a cross-sectional view, and an airfoil portion having a leading edge and a trailing edge; injecting a resin into the mold so as to impregnate the blade fiber preform; unmolding the blade after curing the resin; and subjecting the resin and the blade fiber preform to pressure inside the mold while the resin is curing, wherein the blade is free of pores, wherein the mold includes a resin injection hole facing the bottom planar face of the root portion and a vent hole facing a tip of the airfoil portion, a first gas injection hole facing the leading edge of the airfoil portion, and a second gas injection hole facing the trailing edge of the airfoil portion, and wherein the pressure is applied to the blade fiber preform by injecting a fluid under pressure into the mold via the first gas injection hole and the second injection hole. 2. The method according to claim 1 , wherein the pressure is applied to the blade fiber preform in the mold before a degree of curing of the resin exceeds a value of from 20% to 30%. 3. The method according to claim 1 , wherein the pressure applied to the blade fiber preform in the mold is higher than a vapor pressure of a gas generated during curing of the resin. 4. The method according to claim 1 , wherein the pressure applied to the blade fiber preform is greater than or equal to 2 bars, relative to atmospheric pressure. 5. The method according to claim 1 , wherein the resin is an epoxy resin, a bismaleimide resin, a polyimide resin, or any resin comprising volatile impurities, solvents, or both. 6. The method according claim 1 , wherein the mold is evacuated in order to inject the resin. 7. The method according to claim 1 , further comprising a plurality of successive stages of injecting resin into the mold and of pressurizing the resin and the mold. 8. The method according to claim 1 , wherein the fluid injected under pressure is a gas such as air or nitrogen, or a liquid that is not miscible with the resin. 9. The method according to claim 1 , wherein the mold includes recesses corresponding to the first and second sloping faces of the root portion. 10. The method according to claim 1 , wherein the pressure is further applied to the blade fiber preform by injecting the fluid under pressure into the mold via the resin injection hole and the vent hole.
Preventing defects on the moulded article, e.g. weld lines, shrinkage marks (preventing defects on the preformed parts or layers B29C45/14836) · CPC title
and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM] {, e.g. by vacuum} · CPC title
Rigid movable compressing mould parts acting independently from opening or closing action of the main mould · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.