IP Library Granted Patent US 11,426,953
Granted Patent B2
US 11,426,953 · App. 16/033,300 · Granted Aug 30, 2022

Fiber composite laying device and fiber composite laying method for producing a fiber composite scrim for forming a fiber composite component

Inventors: Katharina Schlegel (Taufkirchen, DE); Alois Friedberger (Taufkirchen, DE); David Lopez-Bravo (Getafe, ES)
Assignees: Airbus Defence and Space GmbH; Airbus Operations, S.L.
B29C70/384B29C70/34B29C70/388B29C70/504B29C2037/903B29K2105/0872
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Quick Facts
Patent No.
US 11,426,953
App. No.
16/033,300
Granted
Aug 30, 2022
Kind
B2
Abstract

A fiber composite laying device for producing a fiber composite scrim for forming a fiber composite component has a laying head which is designed or configured to continuously supply a reinforcement fiber band, a compaction roller which is designed or configured to receive the supplied reinforcement fiber band, lay the band on a laying surface and press the band onto the laying surface at an average compaction pressure, and pressure sensors which are arranged on the compaction roller and are designed or configured to detect a local compaction pressure on the laid reinforcement fiber band.

Claims (37)

1. A fiber composite laying device for producing a fiber composite scrim for forming a fiber composite component, the fiber composite laying device comprising:

a laying head to continuously supply a reinforcement fiber band;

a compaction roller to receive the supplied reinforcement fiber band, lay the reinforcement fiber band on a laying surface, and press the reinforcement fiber band onto the laying surface at an average compaction pressure, such that a laid reinforcement fiber band is produced;

a radiation source configured to irradiate the laid reinforcement fiber band, at least in regions;

a radiation sensor configured to detect reflection radiation reflected by the laid reinforcement fiber band;

an evaluation unit configured to evaluate the detected reflection radiation to determine any occurrences of laying errors of the laid reinforcement fiber band; and

a plurality of pressure sensors that are arranged on the compaction roller and configured to detect a local compaction pressure on the laid reinforcement fiber band;

wherein the compaction roller is, at least in regions, transparent to radiation emitted by the radiation source; and

wherein at least some of the plurality of pressure sensors are transparent to radiation emitted by the radiation source.

2. The fiber composite laying device of claim 1 , wherein the compaction roller is configured to adjust an average compaction pressure on a basis of local compaction pressure detected by the plurality of pressure sensors.

3. The fiber composite laying device of claim 1 , comprising

a plurality of actuators arranged on the compaction roller and configured to adjust the local compaction pressure based on the local compaction pressure detected by the plurality of pressure sensors.

4. The fiber composite laying device of claim 1 , wherein at least some of the plurality of pressure sensors are actuators.

5. The fiber composite laying device of claim 1 , wherein at least some of the plurality of pressure sensors are configured as at least one sensor array along a compaction surface of the compaction roller.

6. The fiber composite laying device of claim 1 , wherein the plurality of pressure sensors substantially cover an entire compaction surface of the compaction roller.

7. The fiber composite laying device of claim 1 , wherein at least some of the plurality of pressure sensors comprise a pressure-sensitive flexible diaphragm.

8. The fiber composite laying device of claim 1 , wherein at least some of the plurality of pressure sensors comprise piezoelectric elements.

9. The fiber composite laying device of claim 1 , wherein at least some of the plurality of pressure sensors are embedded in a protective layer on the compaction roller.

10. The fiber composite laying device of claim 1 , wherein the radiation source is positioned within the compaction roller.

11. The fiber composite laying device of claim 10 , wherein the radiation sensor is positioned inside the compaction roller.

12. The fiber composite laying device of claim 1 , wherein the radiation sensor is positioned inside the compaction roller.

13. A method for producing a fiber composite scrim for forming a fiber composite component, the method comprising:

supplying, via a laying head, a reinforcement fiber band;

receiving, at a compaction roller, the reinforcement fiber band;

laying the reinforcement fiber band on a laying surface; and

pressing, via the compaction roller, the reinforcement fiber band onto the laying surface at an average compaction pressure to produce a laid reinforcement fiber band;

irradiating, using a radiation source, the laid reinforcement fiber band, at least in regions;

detecting, using a radiation sensor, reflection radiation that is reflected by the laid reinforcement fiber;

evaluating, using an evaluation unit, the reflection radiation detected by the radiation sensor to determine any occurrences of laying errors of the laid reinforcement fiber band; and

detecting, via a plurality of pressure sensors that are arranged on the compaction roller, a local compaction pressure on the laid reinforcement fiber band;

wherein the compaction roller is, at least in regions, transparent to radiation emitted by the radiation source; and

wherein at least some of the plurality of pressure sensors are transparent to radiation emitted by the radiation source.

14. The method of claim 13 , comprising

adjusting the average compaction pressure of the compaction roller based on the local compaction pressure detected by the plurality of pressure sensors.

15. The method of claim 13 , wherein at least some of the plurality of pressure sensors are actuators, the method comprising

adjusting, via the actuators, the local compaction pressure based on the local compaction pressure detected by the plurality of pressure sensors.

16. The method of claim 13 , wherein at least some of the plurality of pressure sensors are embedded in a protective layer on the compaction roller.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 27, 2018
From: SCHLEGEL, KATHARINA; FRIEDBERGER, ALOIS; LOPEZ-BRAVO, DAVID
To: AIRBUS DEFENCE AND SPACE GMBH; AIRBUS OPERATIONS, S.L.
Reel/Frame 046993/0598 →
Priority Claims (1)
DE 10 2017 212 068.1 · Jul 14, 2017 · national
Continuity (1)
Related Publication 20190016066A1 · Jan 17, 2019