Applicator

Patent metadata

Field	Value
Publication number	US-11000877-B2
Application number	US-201816130231-A
Country	US
Kind code	B2
Filing date	Sep 13, 2018
Priority date	Apr 9, 2014
Publication date	May 11, 2021
Grant date	May 11, 2021

Abstract

An applicator for application onto and embossing microprofiling of a fluidic medium on a substrate, in particular in the aerospace sector, and a corresponding application device having such an applicator. The applicator has a circumferentially moving die that has an embossing profile, a press for the die and a stabilizing device, in particular a hardening device, for the applied medium. In addition, the applicator has a hollow support body, surrounded by the die at a distance forming a gap, the press being arranged in the gap. The application device has, in addition to the applicator, a handling device for a relative movement between the applicator and a workpiece.

First claim

The invention claimed is:

1. An applicator for applying and embossing a microprofile on a fluidic medium on an outer skin of an aircraft, the applicator comprising:
a circumferentially movable die comprising an embossing profile for embossing the microprofile in the fluidic medium on the outer skin of the aircraft;
a frame;
a feeding device;
a hollow support body, which is rotatably mounted on the frame and within the die, the hollow support body being surrounded, when mounted on the frame, by the die at a distance to form a gap between the support body and the die; and
a press for the die, wherein the press is arranged in the gap and is configured to act on the die from an inside of the die to exert a pressure force on the die, so that the die is rotatably locked to the support body;
wherein the die is configured to receive the fluidic medium from the feeding device using the embossing profile when the die moves circumferentially;
wherein the die is in a form of an endless annular path; and
wherein the die is configured to be rolled over the outer skin of the aircraft to transfer the fluidic medium to the outer skin of the aircraft.

2. The applicator according to claim 1 , comprising a drive for circumferential movement of the die.

3. The applicator according to claim 2 , wherein the support body is coupled to the drive.

4. The applicator according to claim 1 , wherein the die is configured to form the microprofile on the outer skin of the aircraft to comprise a microstructure having elevations and indentions in a form of at least one stripe.

5. The applicator according to claim 1 , wherein the die is configured to emboss a plurality of parallel stripes in one application path.

6. The applicator according to claim 5 , wherein a width of the die is greater than a width of the application path, and the embossing profile extends only over a partial area of the width of the die.

7. The applicator according to claim 6 , comprising a stabilizer and a barrier arranged at an edge of the die that prevents passage of the stabilizer and allows a region of the fluidic medium to remain unstabilized.

8. The applicator according to claim 7 , wherein the stabilizer is configured to solidify the unstabilized region during an adjacent application path.

9. The applicator according to claim 1 , further comprising a fluidic medium stabilizer.

10. The applicator according to claim 1 , wherein the feeding device is mounted on the frame.

11. An application device for applying and embossing a fluidic medium to form a microprofile on a flat or curved surface of an outer skin of an aircraft, the application device comprising a handling device and at least one applicator, the applicator comprising;
a circumferentially movable die comprising an embossing profile for embossing the microprofile in the fluidic medium on the surface;
a fluidic medium stabilizer;
a frame;
a feeding device mounted on the frame;
a hollow support body, which is rotatably mounted on the frame and within the die, the hollow support body being surrounded, when mounted on the frame, by the die at a distance to form a gap between the support body and the die; and
a press for the die, wherein the press is arranged in the gap and is configured to act on the die from an inside of the die to exert a pressure force on the die, so that the die is rotatably locked to the support body;
wherein the die is configured to receive the fluidic medium from the feeding device using the embossing profile when the die moves circumferentially;
wherein the die is configured to be rolled over the surface to transfer the fluidic medium to the surface; and
wherein the die is in a form of an endless annular path.

12. The application device according to claim 11 , wherein the handling device comprises a multi-axis programmable industrial robot for a relative motion between the at least one applicator and the outer skin of the aircraft.

13. The application device according to claim 11 , comprising a plurality of applicators, wherein the applicators are connected to a common handler mount by articulated mounting arms and/or an adjusting device.

14. An applicator for applying and embossing a microprofile on a fluidic medium on an outer skin of an aircraft, the applicator comprising:
a die for receiving a fluidic medium, the die comprising an embossing profile for embossing the microprofile in the fluidic medium on the outer skin of the aircraft;
a frame;
a feeding device mounted on the frame;
a hollow support body, which is rotatably mounted on the frame and within the die, the hollow support body being surrounded, when mounted on the frame, by the die at a distance to form a gap between the support body and the die; and
a press for the die, wherein the press is arranged in the gap and is configured to act on the die from an inside of the die to exert a pressure force on the die, so that the die is rotatably locked to the support body;
wherein the die is circumferentially movable to roll over the outer skin of the aircraft to transfer the fluidic medium to the outer skin of the aircraft; and
wherein the die is in a form of an endless annular path.

15. The applicator according to claim 14 , wherein the hollow support body is surrounded by the die at a distance, thereby forming a gap, and wherein the press is in the gap.

16. The applicator according to claim 14 , comprising a drive for circumferential movement of the die.

17. The applicator according to claim 14 , wherein the support body is coupled to the drive.

18. The applicator according to claim 14 , further comprising a fluidic medium stabilizer.

Assignees

• Airbus Operations Gmbh

Inventors

• Sturm Thomas
• Huber Helmut

Classifications

• B29C59/046 Primary

  for layered or coated substantially flat surfaces · CPC title

• B05D3/067

  Curing or cross-linking the coating · CPC title

• B05C1/0808 Primary

  Details thereof, e.g. surface characteristics · CPC title

• B05D1/40

  Distributing applied liquids or other fluent materials by members moving relatively to surface · CPC title

• B29C2035/0827

  using UV radiation · CPC title