Impregnation mandrel with vacuum liner for making a gas turbine casing made of composite material

US9415549B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9415549-B2
Application numberUS-201214352159-A
CountryUS
Kind codeB2
Filing dateOct 17, 2012
Priority dateOct 26, 2011
Publication dateAug 16, 2016
Grant dateAug 16, 2016

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

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.

First claim

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.

Assignees

Inventors

Classifications

  • B29C70/44Primary

    using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding · CPC title

  • B29C70/443Primary

    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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Frequently asked questions

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What does patent US9415549B2 cover?
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…
Who is the assignee on this patent?
Snecma
What technology area does this patent fall under?
Primary CPC classification B29C70/44. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Aug 16 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).