Method and a thermoplastic blade

Patent metadata

Field	Value
Publication number	US-10654225-B2
Application number	US-201715603628-A
Country	US
Kind code	B2
Filing date	May 24, 2017
Priority date	May 25, 2016
Publication date	May 19, 2020
Grant date	May 19, 2020

Abstract

A method of fabricating a blade. The blade comprises subassemblies made of thermoplastic composite materials, each subassembly comprising an internal arrangement and at least one external arrangement, each internal arrangement comprising a stack of intermediate layers comprising reinforcing fibers impregnated with a semicrystalline thermoplastic matrix, each external arrangement comprising at least one surface layer comprising reinforcing fibers impregnated with an alloy of a semicrystalline thermoplastic polymer and of an amorphous thermoplastic polymer. An assembly film comprising an amorphous thermoplastic material and a ferromagnetic member is interposed between two surface layers of two distinct subassemblies that are to be assembled together by a method of local heating by induction.

First claim

What is claimed is:

1. A fabrication method for fabricating a blade, the method comprising the following steps:
fabricating subassemblies out of thermoplastic composite materials;
placing the subassemblies in an assembly mold;
locally arranging a plurality of assembly films, each assembly film being interposed between two distinct subassemblies that are to be assembled together; and
assembling the subassemblies together in the assembly mold by exerting pressure on the subassemblies and by locally heating each assembly film by electromagnetic induction in application of a cycle for applying heat and pressure;
wherein each subassembly comprises an internal arrangement and at least one external arrangement joined to the internal arrangement, the external arrangement of one subassembly being for adhesively bonding to an external arrangement of another subassembly, each internal arrangement comprising a stack of plies referred to as “intermediate” layers, each intermediate layer comprising reinforcing fibers impregnated with a semicrystalline thermoplastic matrix, each external arrangement comprising at least one ply referred to as a “surface” layer, each surface layer comprising reinforcing fibers impregnated with an alloy of a semicrystalline thermoplastic polymer and an amorphous thermoplastic polymer, each assembly film comprising an amorphous thermoplastic material and a ferromagnetic member.

2. The fabrication method according to claim 1 , wherein each reinforcing fiber is selected from a list consisting of: a glass fiber; a carbon fiber; a basalt fiber, and an aramid fiber.

3. The fabrication method according to claim 1 , wherein each subassembly is selected from a list consisting of: a spar; a stiffener; an outer skin; and a trailing edge strip.

4. The fabrication method according to claim 1 , wherein the blade comprises at least one spar, at least one trailing edge strip, a plurality of stiffeners, and a plurality of outer skins, outer skins being joined to one another spanwise in order to form a suction side wall, outer skins being joined to one another spanwise in order to form a pressure side wall, the or each trailing edge strip, the or each spar, and each stiffener extending between the suction side wall and the pressure side wall, at least one stiffener being located at the junction between two outer skins in the pressure side wall and two outer skins in the suction side wall.

5. The fabrication method according to claim 1 , wherein the semicrystalline thermoplastic matrix is poly ether ether ketone.

6. The fabrication method according to claim 1 , wherein the semicrystalline thermoplastic polymer is poly ether ether ketone, and the amorphous thermoplastic polymer is poly ether imide.

7. The fabrication method according to claim 1 , wherein the alloy of a semicrystalline thermoplastic polymer and of an amorphous thermoplastic polymer comprises 70% poly ether ether ketone and 30% poly ether imide.

8. The fabrication method according to claim 1 , wherein the amorphous thermoplastic material comprises at least poly ether imide.

9. The fabrication method according to claim 1 , wherein the ferromagnetic member comprises particles of ferrite or a metal element.

10. The fabrication method according to claim 1 , wherein the amorphous thermoplastic material includes benzophenone and/or propriophenone.

11. The fabrication method according to claim 1 , wherein the step of fabricating subassemblies comprises the following stages for fabricating a subassembly:
arranging the plies in a fabrication mold; and
heating the plies in the fabrication mold in application of a heating cycle that reaches a maximum temperature referred to as “hot” temperature.

12. The fabrication method according to claim 11 , wherein the plies of a subassembly comprise sized fibers.

13. The fabrication method according to claim 11 , wherein, prior to the stage of arranging the plies in a fabrication mold, the step of fabricating subassemblies comprises the following stages:
depositing plies one by one in a positioning mold, each ply deposited in the positioning mold being locally welded to the previously deposited ply; and
transferring the plies from the positioning mold to the fabrication mold.

14. The fabrication method according to claim 11 , wherein the cycle of applying heat and pressure comprises a stage of raising the temperature of the assembly films to a maximum temperature referred to as the “assembly” temperature, a stage of maintaining the assembly temperature, followed by a stage of reducing the temperature of the assembly films, the assembly temperature being lower than the hot temperature.

15. The fabrication method according to claim 14 , wherein the assembly temperature lies in the range 150° C. to 210° C., the hot temperature lying in the range 350° C. to 450° C.

16. The fabrication method according to claim 1 , wherein each surface layer (includes a tracer yarn enabling a surface layer to be distinguished visually from an intermediate layer.

17. The fabrication method according to claim 12 , further comprising prior to the stage of arranging the plies in a fabrication mold, the step of fabricating subassemblies comprises the following fabrication stages:
applying a power of thermoplastic polymer on at least one de-sized reinforcing fiber; and
bonding the thermoplastic polymer onto the de-sized reinforcing fiber by heating to form the sized fibers.

18. The fabrication method according to claim 1 , wherein the reinforcing fiber comprises synthetic fiber.

19. The fabrication method according to claim 1 , wherein the subassemblies comprise blade components.

20. A fabrication method for fabricating a blade, the method comprising:
providing subassemblies made of thermoplastic composite materials;
placing the subassemblies in an assembly mold;
locally arranging a plurality of assembly films, each assembly film being interposed between two distinct subassemblies that are to be assembled together; and
assembling the subassemblies together in the assembly mold by exerting pressure on the subassemblies and by heating each assembly film by electromagnetic induction in application of a cycle for applying heat and pressure;
wherein each subassembly comprises an internal arrangement and at least one external arrangement joined to the internal arrangement, the external arrangement of one subassembly being for adhesively bonding to an external arrangement of another subassembly, each internal arrangement comprising a stack of plies referred to as “intermediate” layers, each intermediate layer comprising reinforcing fibers impregnated with a semicrystalline thermoplastic matrix, each external arrangement comprising at least one ply referred to as a “surface” layer, each surface layer comprising reinforcing fibers impregnated with an alloy of a semicrystalline thermoplastic polymer and an amorphous thermoplastic polymer, each assembly film comprising an amorphous thermoplastic material and a ferromagnetic member.

Assignees

• Airbus Helicopters

Inventors

• Boschet Patrick

Classifications

• B29C35/0272 Primary

  using lost heating elements, i.e. heating means incorporated and remaining in the formed article (for preforms with internal stresses B29C61/0625; joining using lost heating elements B29C65/34; making electrically conductive articles B29C70/882) · CPC title

• F05B2280/4007

  Thermoplastics · CPC title

• B29C2035/0811

  using induction · CPC title

• B29C70/54

  Component parts, details or accessories; Auxiliary operations {, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing} · CPC title

• B29C70/34 Primary

  and shaping or impregnating by compression {, i.e. combined with compressing after the lay-up operation} · CPC title