Composite blade made by additive manufacturing

Patent metadata

Field	Value
Publication number	US-9903211-B2
Application number	US-201414471979-A
Country	US
Kind code	B2
Filing date	Aug 28, 2014
Priority date	Aug 28, 2013
Publication date	Feb 27, 2018
Grant date	Feb 27, 2018

Abstract

The present application relates to a blade of a rectifier of a low pressure compressor of an axial turbomachine. The blade can also be a rotor and/or turbine blade. The blade includes a composite material with a matrix and a reinforcement comprising a mesh with rods. The rods of the reinforcement are connected to each other and are distributed throughout the volume between the pressure side surface and the suction side surface of the blade. The mesh forms a three-dimensional structure extending over the majority of the thickness of the blade between the pressure side surface and the suction side surface and/or the majority of the length of the blade between the leading edge and the trailing edge. The present application also relates to an iterative method for manufacturing a blade composite where the reinforcement is formed by additive layer manufacturing based on titanium powder and then placed in an injection mold.

First claim

I claim:

1. A blade for a turbomachine, comprising:
a leading edge;
a trailing edge;
a pressure side surface; and
a suction side surface;
wherein both surfaces extend from the leading edge to the trailing edge;
wherein the blade is formed from a composite material having a matrix and a reinforcement having a mesh; and
wherein the mesh forms a three-dimensional structure which extends over the majority of the thickness of the blade between the pressure side surface and the suction side surface and/or the majority of the length of the blade between the leading edge and the trailing edge;
wherein the three-dimensional structure is made of rods each including two ends, the rods being joined to each other by their ends.

2. The blade according to claim 1 , wherein the mesh comprises:
an envelope which defines a space occupying the majority of the thickness of the blade between the pressure side surface and the suction side surface and/or the majority of the length of the blade between the leading edge and the trailing edge, the space of the envelope occupies the majority of the volume between the pressure side surface and the suction side surface.

3. The blade according to claim 1 , wherein the three-dimensional structure of the reinforcement comprises:
rods interconnected to each other with material continuity by connecting nodes;
wherein the number of rods connected to the connecting nodes varies.

4. The blade according to claim 3 , wherein the rods define with each other polyhedrons that occupy the majority of the volume between the pressure side surface and the suction side surface.

5. The blade according to claim 3 , wherein the rods define with each other polyhedrons that occupy at least 75% of the volume between the pressure side surface and the suction side surface.

6. The blade according to claim 3 , wherein the rods define with each other polyhedrons that occupy at least 95% of the volume between the pressure side surface and the suction side surface.

7. The blade according to claim 1 , wherein the structure comprises:
at least one set of rods connected together, each set forming a junction, the junction extending over the majority of the thickness of the blade and/or the majority of the length of the blade and/or the majority of the height of the blade.

8. The blade according to claim 7 , wherein the rods forming a junction are inclined with respect to the main direction of said junction by one of the following:
less than 60°;
less than 45°; and
less than 30°.

9. The blade according to claim 3 , wherein the majority of the rods connected to a common rod are inclined relative to the common shaft by one of the following:
more than 10°;
more than 25°; and
more than 60°.

10. The blade according to claim 3 , wherein at least one rod is generally flat and/or at least one rod is generally spherical.

11. The blade according to claim 3 , wherein the rods have variable lengths and/or variable widths.

12. The blade according to claim 1 , wherein the specific volume density of the mesh is between one of the following ranges:
1% and 80%;
5% and 50%; and
10% and 20%.

13. The blade according to claim 1 , wherein the volume density of the mesh between the pressure side surface and the suction side surface varies along the height of the blade and/or from the leading edge to the trailing edge, the blade comprising:
fastening means;
wherein the volume density of the mesh increases in the direction of the fastening means.

14. The blade according to claim 1 , wherein the reinforcement is integral and made by a method of additive layer manufacturing.

15. The blade according to claim 1 , wherein the matrix and the reinforcement are made of different materials, the matrix comprising:
a thermoplastic resin; and
the reinforcement comprising:
metal.

16. The blade according to claim 15 , wherein the metal is titanium.

17. A turbomachine blade comprising:
a leading edge,
a trailing edge,
an outer pressure side surface and an outer suction side surface, both surfaces extending from the leading edge to the trailing edge,
a composite material with a matrix and an integral and one piece reinforcement,
wherein the integral and one piece reinforcement forms an integral network of interconnected cavities filled with the matrix, the integral network of interconnected cavities filled with the matrix extends from the leading edge to the trailing edge and communicates from the outer pressure side surface to the outer suction side surface.

18. The turbomachine blade of claim 17 , wherein the reinforcement comprises a three-dimensional mesh with rods, said rods forming the network of interconnected cavities which is filled by the matrix.

19. A turbomachine blade comprising:
a leading edge,
a trailing edge,
a pressure side surface and a suction side surface, both surfaces extending from the leading edge to the trailing edge,
a composite material including a matrix and a reinforcement with a three-dimensional mesh formed of rods,
said rods delimiting a network of interconnected polyhedral cavities,
said polyhedral cavities being selected from the group consisting of tetrahedral cavities and hexahedral cavities,
said network of interconnected polyhedral cavities being filled by the matrix so as to form a solid body.

20. The turbomachine blade of claim 19 , wherein the solid body extends from at least one of the following group comprising:
the leading edge;
the trailing edge;
the pressure side surface; and
the suction side surface.

Assignees

• Techspace Aero Sa
• Safran Aero Boosters Sa

Inventors

• Perez Rafael

Classifications

• B29C70/70

  Completely encapsulating inserts {(B29C70/86 takes precedence)} · CPC title

• F05D2300/6033

  Ceramic matrix composites [CMC] · CPC title

• F01D5/282 Primary

  Selecting composite materials, e.g. blades with reinforcing filaments · CPC title

• B33Y80/00

  Products made by additive manufacturing · CPC title

• B29K2305/00

  Use of metals, their alloys or their compounds, as reinforcement · CPC title