Applicator

US10173238B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10173238-B2
Application numberUS-201615288516-A
CountryUS
Kind codeB2
Filing dateOct 7, 2016
Priority dateApr 9, 2014
Publication dateJan 8, 2019
Grant dateJan 8, 2019

How to read this patent

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  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

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  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

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Abstract

Official abstract text for this publication.

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

Opening claim text (preview).

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 press for the die; a fluidic medium stabilizer; a frame comprising a connector configured to connect with a power takeoff element arranged thereon, wherein the frame is connected in a rotationally locked manner to the die; and a feeding device mounted on the frame; 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 applicator is configured to roll the die over the outer skin of the aircraft to transfer the fluidic medium to the outer skin of the aircraft, and wherein the applicator comprises a hollow support body, surrounded by the die at a distance, thereby forming a gap, the press being arranged in the gap, and the support body being rotatably mounted on the frame of the applicator. 2. The applicator according to claim 1 , wherein the stabilizer is arranged in or on the support body. 3. The applicator according to claim 1 , wherein the applicator comprises a connector for a handling device. 4. The applicator according to claim 3 , wherein the handling device is an industrial robot. 5. The applicator according to claim 1 , wherein the support body is tubular and has a dimensionally stable outer cover. 6. The applicator according to claim 1 , wherein the applicator has its own drive for circumferential movement of the die and the support body is coupled to the drive. 7. The applicator according claim 1 , wherein the support body can be controlled or regulated. 8. The applicator according claim 1 , wherein the press is formed as a deformable pressure pad filling the gap. 9. The applicator according to claim 8 , wherein the pressure pad is connected in a rotationally locked manner with the support body and with the die. 10. The applicator according claim 8 , wherein the pressure pad comprises a fluidic pressure medium in a sealing, bending elastic enclosure. 11. The applicator according to claim 10 , wherein the fluidic pressure medium is a pressure gas. 12. The applicator according claim 1 , wherein the press comprises a control for controlling or regulating an inner pressure force on the die. 13. The applicator according to claim 1 , wherein the die is formed as a bendable elastic endless annular path. 14. The applicator according to claim 1 , wherein the embossing profile is arranged on an outer side of the die or on an outer side coating of the die. 15. The applicator according claim 1 , wherein the stabilizer is configured to emit a stabilizing agent, wherein an outer cover of the support body, the press, and the die are permeable for the stabilizing agent. 16. The applicator according claim 15 , wherein the stabilizer comprises a light source and the stabilizing agent comprises light. 17. The applicator according to claim 16 , wherein the light source is a UV lamp and the stabilizing agent is UV light. 18. The applicator according to claim 15 , wherein the applicator, at an edge thereof, has a local barrier for the stabilizing agent. 19. The applicator according to claim 1 , wherein the fluidic medium comprises a hardenable varnish. 20. The applicator according claim 1 , wherein the applicator comprises a cleaning device. 21. An application device for applying and embossing a microprofile on a fluidic medium on an outer skin of an aircraft, the application device comprising an applicator according to claim 1 , wherein the application device is configured to allow a relative motion between the applicator and the outer skin of the aircraft. 22. The application device according to claim 21 , wherein the application device is configured to move the applicator along the outer skin of the aircraft and, in doing so, to press the applicator against the outer skin of the aircraft to apply a force configured to deform the circumferentially moved die in a pressing area, which is a contact area between the die and the outer skin of the aircraft, and to conform to the outer skin of the aircraft and a contour thereof in a planar manner. 23. The application device according to claim 21 , wherein the application device comprises a multi-axis programmable industrial robot for the relative motion between the applicator and the outer skin of the aircraft. 24. The application device according to claim 23 , wherein the multi-axis programmable industrial robot comprises a jointed-arm robot. 25. The application device according to claim 23 , comprising a movable carrier having one or more movement axes for the multi-axis programmable industrial robot. 26. The application device according to claim 21 , wherein the application device is configured to measure a position and orientation of the applicator in a process, for a process quality, or a pressing force to the substrate.

Assignees

Inventors

Classifications

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

  • using UV radiation · CPC title

  • applying pressure locally · CPC title

  • B05C9/02Primary

    for applying liquid or other fluent material to surfaces by single means not covered by groups B05C1/00 - B05C7/00, whether or not also using other means · CPC title

  • Curing or cross-linking the coating · CPC title

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Frequently asked questions

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What does patent US10173238B2 cover?
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 addi…
Who is the assignee on this patent?
Airbus Operations Gmbh
What technology area does this patent fall under?
Primary CPC classification B05C9/02. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Jan 08 2019 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).