Systems and methods for manufacturing large contoured parts from thermoplastic laminate sheets
US-12172396-B2 · Dec 24, 2024 · US
US9415549B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9415549-B2 |
| Application number | US-201214352159-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 17, 2012 |
| Priority date | Oct 26, 2011 |
| Publication date | Aug 16, 2016 |
| Grant date | Aug 16, 2016 |
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An impregnation mandrel for production of a gas turbine casing made from composite material, including: a mandrel having a central wall and two side plates; compaction bars, each including (i) a wedge configured to bear against a fibrous reinforcing part covering angles formed between the central wall and the side plates of the mandrel, and (ii) an attachment flange configured to be attached to the corresponding side plate of the mandrel; a flexible casing forming a vacuum bag and configured to be applied at least against the fibrous reinforcing part covering the central wall of the mandrel; and a mechanism for injecting resin into a space defined between the vacuum bag and the mandrel at one of longitudinal ends of the fibrous reinforcement and for extracting the resin at the opposite end.
Opening claim text (preview).
The invention claimed is: 1. An impregnation mandrel for making a gas turbine casing made of composite material, comprising: an impregnation mandrel on which a fibrous reinforcement is configured to be held, formed by superposed layers of a fibrous texture, the mandrel comprising a central annular wall with a profile that corresponds to that of the casing to be manufactured and two lateral flanges with profiles that correspond to those of external flanges of the casing to be manufactured; compaction bars each comprising a corner configured to be supported against a part of the fibrous reinforcement covering angles formed between the central wall and the flanges of the mandrel, and a coupling flange configured to be fixed on the corresponding flange of the mandrel; a supple envelope forming a vacuum liner configured to be applied at least on that part of the fibrous reinforcement covering the central wall of the mandrel; and means for injecting resin into a space delimited between the vacuum liner and the mandrel at a longitudinal end of the fibrous reinforcement and for extracting the resin at an opposite end. 2. The mandrel according to claim 1 , further comprising at least one resin injection orifice terminating inside the delimited space between the vacuum liner and the mandrel at a longitudinal end of the fibrous reinforcement, and at least one resin extraction orifice placed at the longitudinal end of the fibrous reinforcement opposite to where the resin injection orifice terminates. 3. The mandrel according to claim 2 , wherein the resin injection orifice is formed in a first of the flanges of the mandrel and the resin extraction orifice is formed in a second flange. 4. The mandrel according to in claim 3 , wherein the resin injection orifice terminates at a corner of an injection compaction bar, whereas the resin extraction orifice terminates downstream of opposite extraction compaction bars. 5. The mandrel according to in claim 4 , wherein the coupling flanges of the extraction compaction bars comprise grooves for passage of the resin. 6. The mandrel according to claim 1 , wherein the vacuum liner is configured to be also applied to the compaction bars and be fixed tightly by its free ends to the flanges of the mandrel. 7. The mandrel according to claim 1 , wherein the coupling flanges of the compaction bars are configured to be fixed tightly on the flanges of the mandrel. 8. The mandrel according to claim 1 , wherein for each flange of the mandrel, there are four compaction bars that are put end to end angularly to cover a total circumference of the mandrel. 9. A winding machine of a fibrous texture on an impregnation mandrel, comprising: a take-up mandrel on which a fibrous texture is configured to be stored, produced by three-dimensional weaving, the take-up mandrel having a substantially horizontal axis of rotation; an impregnation mandrel according to claim 1 , the impregnation mandrel having a substantially horizontal axis of rotation parallel to the axis of rotation of the take-up mandrel; electric motors for driving the mandrels in rotation about their respective axis of rotation; and a control unit of the electric motors for driving the mandrels in rotation.
using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding · CPC title
and impregnating by vacuum or injection · CPC title
Air intakes for gas-turbine plants or jet-propulsion plants · CPC title
Moulds for making articles of definite length, i.e. discrete articles · CPC title
Composites; e.g. fibre-reinforced · CPC title
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