Compacting and injection mold for a fiber preform for fabricating a turbine engine guide vane made of composite material

Patent metadata

Field	Value
Publication number	US-9868235-B2
Application number	US-201214115771-A
Country	US
Kind code	B2
Filing date	May 3, 2012
Priority date	May 10, 2011
Publication date	Jan 16, 2018
Grant date	Jan 16, 2018

Abstract

A compacting and injection mold for a fiber preform is for use in fabricating a turbine engine guide vane out of composite material. The mold includes a shell forming a trough that is to receive the fiber preform and that is closed in leaktight manner by bottom and top covers, compacting blocks arranged inside the trough each having a surface pressing normally against a surface of the fiber preform that is to be compacted, and closure blocks arranged inside the trough. Each closure block has a surface pressing normally against a surface of a compacting block and does not have a surface in contact with the fiber preform.

First claim

The invention claimed is:

1. A compacting and injection mold for a fiber preform for use in fabricating a turbine engine part out of composite material, the mold comprising:
a shell forming a trough that is to receive the fiber preform and that is closed in a leaktight manner by substantially plane bottom and top covers, the top cover being assembled on side walls of the trough in order to close the mold in the leaktight manner;
compacting blocks arranged inside the trough each having a surface pressing normally against a surface of the fiber preform that is to be compacted; and
closure blocks arranged inside the trough, each closure block having a surface pressing normally against a surface of a compacting block and not having a surface in contact with the fiber preform.

2. The mold according to claim 1 , wherein the compacting blocks and the closure blocks present a coefficient of thermal expansion that is greater than that of the trough and of the covers.

3. The mold according to claim 1 , wherein inside surfaces of the side walls of the trough slope perceptibly relative to a plane normal to the bottom and top covers.

4. The mold according to claim 1 , wherein the fiber preform is for fabricating a turbine engine vane including an airfoil having a pressure side and a suction side, a top platform at a radially outer end of the airfoil, and a bottom platform at a radially inner end of the airfoil, the bottom platform including an upstream flange at an upstream end thereof and a downstream flange at a downstream end thereof, and
wherein the compacting blocks include
a first compacting block having a surface for pressing normally against a surface of the fiber preform constituting the pressure side of the airfoil of the vane,
a second compacting block having a surface for pressing normally against a surface of the fiber preform constituting the suction side of the airfoil of the vane,
a third compacting block having a surface for pressing normally against a surface of the fiber preform constituting the top platform of the vane,
a fourth compacting block having a surface for pressing normally against a surface of the fiber preform constituting the bottom platform of the vane, and
fifth and sixth compacting blocks having surfaces for pressing normally against respective surfaces of the fiber preform constituting upstream and downstream flanges of bottom platform of the vane.

5. The mold according to claim 4 , wherein at least one of the compacting blocks is made up of at least two distinct portions in order to facilitate unmolding thereof.

6. The mold according to claim 4 , wherein the closure blocks include
a first closure block having a first surface for pressing normally against a surface of the third compacting block, and a second surface, remote from the first surface, for pressing against the surface of the fiber preform constituting the top platform of the vane,
a second closure block having a first surface for pressing normally against a surface of the fourth compacting block, and a second surface, remote from the first surface, for pressing against the surface of the fiber preform constituting the bottom platform of the vane,
a third closure block having a first surface for pressing normally against a surface of the fifth compacting block, and a second surface, remote from the first surface, for pressing against the surface of the fiber preform constituting the upstream flange of the bottom platform of the vane, and
a fourth closure block having a first surface for pressing normally against a surface of the sixth compacting blocks, and a second surface, remote from the first surface, for pressing against the surface of the fiber preform constituting the downstream flange of the bottom platform of the vane.

Assignees

• Plante Romain
• Lacroix Lise
• Patrigeon Olivier
• Cauchois Jean-Pierre
• Burek Pascal
• Snecma

Inventors

• Plante Romain
• Lacroix Lise
• Patrigeon Olivier
• Cauchois Jean-Pierre
• Burek Pascal

Classifications

• B29C45/0005 Primary

  using fibre reinforcements · CPC title

• B29C70/48 Primary

  and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM] {, e.g. by vacuum} · CPC title

• B29D99/0025

  Producing blades or the like, e.g. blades for turbines, propellers, or wings · CPC title

• B29C70/461 Primary

  Rigid movable compressing mould parts acting independently from opening or closing action of the main mould · CPC title