Device and method for producing preforms

Patent metadata

Field	Value
Publication number	US-12420498-B2
Application number	US-202017639128-A
Country	US
Kind code	B2
Filing date	Jun 3, 2020
Priority date	Aug 30, 2019
Publication date	Sep 23, 2025
Grant date	Sep 23, 2025

Abstract

A device for producing preforms for aircraft structural components, wherein the device has a supply unit, which is designed to supply a layered structure having at least one material ply of a thermally activatable, flexible fiber composite material, together with a protective film arranged in each case on at least one outer side of the layered structure, wherein the device has at least one shaping unit, which is arranged downstream of the supply unit in a conveying direction and is designed to shape the layered structure supplied, wherein in that the layered structure, together with the respective protective film, can be fed to the shaping unit or to one of the shaping units with a cross-sectional profile with which the protective film or at least one of the protective films extends along a straight line.

First claim

The invention claimed is:

1. A device for producing preforms for aircraft structural components,
wherein the device has a supply unit, which is designed to supply a layered structure having at least one material ply of a thermally activatable, flexible fiber composite material, together with a protective film arranged in each case on at least one outer side of the layered structure,
wherein the device has at least one shaping unit, which is arranged downstream of the supply unit in a conveying direction and is designed to shape the layered structure supplied,
wherein the layered structure, together with the respective protective film, can be fed to the shaping unit or to one of the shaping units with a cross-sectional profile with which the protective film or at least one of the protective films extends along a straight line, and wherein the layered structure, together with the respective protective film, is transversely shaped by the shaping unit into a predetermined non-planar cross-sectional profile; and
wherein the device comprises a pull-off unit designed to pull off the protective film or protective films, which pull-off unit is arranged in conveying direction downstream of at least one of the shaping units.

2. The device as claimed in claim 1 , wherein the layered structure, together with the respective protective film, can be fed to the respective shaping unit along a plane which extends in the conveying direction.

3. The device as claimed in claim 1 , wherein the device has a feed unit, which is designed to transport the layered structure, together with the respective protective film, from the supply unit to the respective shaping unit with a cross-sectional profile with which the protective film or at least one of the protective films extends along a straight line.

4. The device as claimed in claim 1 , wherein the device has a heating unit, which is arranged upstream of the respective shaping unit in the conveying direction and is designed to heat the layered structure, together with the respective protective film, as it is passed through the heating unit.

5. The device as claimed in claim 1 , wherein the supply unit is designed to supply the layered structure as a multi-ply layered structure having at least two or more material plies of a thermally activatable, flexible fiber composite material, together with a protective film arranged in each case on at least one outer side of the layered structure.

6. The device as claimed in claim 1 , wherein the device has a separating unit, which is arranged downstream of the respective shaping unit in the conveying direction and is designed to sever the shaped layered structure transversely to the conveying direction and thereby to form preforms of a predetermined length.

7. The device as claimed in claim 1 , wherein the device has a post-curing unit, which is arranged downstream of the respective shaping unit in the conveying direction and is designed to heat the shaped and severed layered structure.

8. The device as claimed in claim 1 , wherein the device has a pull-off unit, which is designed to pull off from the layered structure the protective film or protective films which has/have extended along the respective straight line until the respective shaping unit has been reached.

9. The device as claimed in claim 1 , wherein the layered structure, together with the respective protective film, can be fed to the respective shaping unit along a plane which extends in the conveying direction, in such a way that the protective film or protective films, which extends/extend along the straight line until the respective shaping unit is reached, extends/extend along the plane.

10. The device as claimed in claim 1 , wherein the device has a heating unit, which is arranged upstream of the respective shaping unit in the conveying direction and is designed to heat the layered structure, together with the respective protective film, as it is passed through the heating unit to a temperature in a range from 100 to 160° C.

11. The device as claimed in claim 1 , wherein the device has a post-curing unit, which is arranged downstream of the respective shaping unit in the conveying direction and is designed to heat the shaped and severed layered structure, to a temperature in a range from 160 to 220° C.

12. The device as claimed in claim 3 , wherein the feed unit is designed to transport the layered structure, together with the respective protective film, along a plane from the supply unit to the respective shaping unit.

13. The device as claimed in claim 3 , wherein the feed unit is designed to transport the layered structure, together with the respective protective film, along a plane from the supply unit to the respective shaping unit, in such a way that the protective film or protective films, which extends/extend along the straight line until the respective shaping unit is reached, extends/extend along the plane.

14. The device as claimed in claim 5 , wherein the material plies are in direct contact with one another.

15. The device as claimed in claim 8 , wherein the pull-off unit is designed to pull off the protective film or protective films which has/have extended along the respective straight line until the respective shaping unit has been reached in a section of the device which lies between the respective shaping unit or one of the shaping units and the separating unit in the conveying direction and/or which lies between the respective shaping unit or one of the shaping units and the post-curing unit in the conveying direction and/or which lies between the separating unit and the post-curing unit in the conveying direction or which is arranged downstream of the post-curing unit in the conveying direction.

Assignees

• Broetje Automation Gmbh

Inventors

• Berg Erik

Classifications

• B29L2031/3076

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

• B29C70/545

  Perforating, cutting or machining during or after moulding · CPC title

• B29B11/16

  comprising fillers or reinforcement {(non-woven fabrics per se D04H1/00, D04H3/00)} · CPC title

• B29C70/50 Primary

  for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] · CPC title