Methods for producing a structural component

Patent metadata

Field	Value
Publication number	US-12565014-B2
Application number	US-201917222413-A
Country	US
Kind code	B2
Filing date	Oct 2, 2019
Priority date	Oct 4, 2018
Publication date	Mar 3, 2026
Grant date	Mar 3, 2026

Abstract

Methods of manufacturing a structural component each include providing a preformed layered structure including a plurality of layers each having reinforcing fibers embedded in a thermoplastic matrix material, heating the layered structure in a cavity formed between a contour surface and an abutment member to a first temperature, which is greater than a melting point of the thermoplastic matrix material, and cooling the layer structure in the cavity to a solidification temperature which is, e.g., less than the melting point of the thermoplastic matrix material, while applying a compression pressure. According to a method, the compression pressure is generated by using a magnet device to generate a magnetic field directed transversely to the contour surface, which pulls or compresses the abutment member and the contour surface relative to each other. According to a further method, inductive heating of the cavity occurs.

First claim

The invention claimed is:

1 . A method of manufacturing a structural component comprising:
providing a layered structure preformed according to a shape of the structural component to be manufactured, comprising a plurality of layers each having reinforcing fibers embedded in a thermoplastic matrix material; heating the layered structure in a cavity formed between a contour surface and an abutment member to a first temperature greater than a melting point of the thermoplastic matrix material; and cooling the layered structure in the cavity to a solidification temperature lower than the melting point of the thermoplastic matrix material while applying a compression pressure; wherein the compression pressure is generated by producing a first magnetic field directed transversely to the contour surface by a first magnet device, wherein the first magnetic field is coupled into a magnetizable material associated with the abutment member or wherein the first magnetic field is coupled into a magnetizable material associated with the contour surface or wherein the first magnetic field interacts with a second magnetic field generated by a second magnet device associated with the other of the abutment member or the contour surface in such a way that the layered structure is subjected to the compression pressure by the contour surface and the abutment member, wherein the first magnetic field is spatially concentrated but distributed over the contour surface or the abutment member in a planar manner and generates the compression pressure, wherein the contour surface is provided by an inner surface of a first mold plate, wherein the abutment member is formed by a second mold plate, wherein each of the first mold plate and the second mold plate is formed as a flatly-extending plate-shaped component having a constant thickness.

2 . The method of claim 1 , wherein the first magnet device is disposed on the abutment member or on the contour surface and wherein the first magnetic field generated by the first magnet device extends through the layered structure.

3 . The method according to claim 1 , wherein the heating of the layered structure is carried out by inductive heating or by infrared radiation.

4 . The method according to claim 1 , wherein the cavity is evacuated by a vacuum device.

5 . The method according to claim 4 , wherein the abutment member is formed by a vacuum film.

6 . The method of claim 1 , wherein a seal is disposed between the first mold plate and the contour surface which hermetically seals the cavity.

7 . The method according to claim 1 , wherein at least one stiffening profile comprising a thermoplastic material is placed on a layer of the layered structure located opposite to the contour surface, wherein the stiffening profile is pressed against the layered structure in the cavity by the abutment member.

8 . The method according to claim 1 , wherein the contour surface is provided by a first surface of a mold half.

9 . The method of claim 1 , wherein the first mold plate is supported by a first mold half.

10 . The method according to claim 1 , wherein the individual layers of the layered structure each have at least one semi-finished product comprising:
a plurality of prepreg tapes extending along each other, each comprising unidirectionally arranged reinforcing fibers embedded in thermoplastic matrix material; and a plurality of connecting strands comprising a thermoplastic plastics material, said connecting strands and said prepreg tapes joined to form a textile sheet structure in which each of said connecting strands crosses a plurality of said prepreg tapes, and wherein the connecting strands and the prepreg tapes in a first end region of the sheet structure and in a second end region of the sheet structure located opposite thereto are each connected to one another in a materially joined manner along a respective connecting line.

11 . The method according to claim 10 , wherein the connecting strands each comprise a first end portion and a second end portion located opposite thereto, the first and second end portions each projecting beyond the connecting lines, and wherein a respective layer of the layered structure is formed by thermoplastically joining at least the first end portions of the connecting strands of a first semi-finished product to prepreg tapes of a respective further semi-finished product, and wherein the second end portions of the connecting strands of the further semi-finished product are thermoplastically joined to prepreg tapes of the first semi-finished product.

12 . The method according to claim 1 , wherein the layers of the layered structure are formed by semi-finished products which comprise:
a plurality of prepreg tapes, each comprising unidirectionally arranged reinforcing fibers embedded in a thermoplastic matrix material, wherein the prepreg tapes are arranged to form a multiaxial fabric comprising a plurality of superimposed layers of prepreg tapes, wherein the prepreg tapes within a layer run parallel to one another, and wherein the layers are joined relative to one another at individual points.

13 . The method according to claim 1 , wherein the providing of the layered structure occurs by depositing prepreg tapes by a depositing head, and wherein the individual prepreg tapes are fixed relative to one another during deposition.

14 . The method according to claim 1 , wherein the layered structure is formed such that the reinforcing fibers extend along one direction within a respective layer and in different directions in different layers.

15 . The method according to claim 1 , wherein the contour surface has a curved geometry.

16 . The method according to claim 1 , wherein the first and second mold plates are dome-shaped.

Assignees

• Premium Aerotec Gmbh

Inventors

• Kuntz Julian
• Kaden Markus
• Schneider Marvin

Classifications

• B29L2031/3076

  Aircrafts (blades, propellers B29L2031/08) · CPC title

• B29K2101/12

  Thermoplastic materials · CPC title

• B29C2035/0822

  using IR radiation · CPC title

• B29C2035/0811

  using induction · CPC title

• B29C70/342

  using isostatic pressure · CPC title