Connection system, connection arrangement and method

US10272529B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10272529-B2
Application numberUS-201615269317-A
CountryUS
Kind codeB2
Filing dateSep 19, 2016
Priority dateSep 21, 2015
Publication dateApr 30, 2019
Grant dateApr 30, 2019

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  1. Title

    What the patent document calls the invention.

  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  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.

A connection system includes two connecting elements each having a respective connecting flange on which a plurality of coupling elements are arranged along a peripheral direction and which has a substantially round external profile; and a coupling belt, on which a plurality of opposing coupling elements are arranged which are configured to form a positive-locking connection with the coupling elements of the two connecting elements for the mutual rotation-proof fixing of the two connecting elements.

First claim

Opening claim text (preview).

The invention claimed is: 1. A connection arrangement, comprising: two connecting elements having a respective connecting flange on which a plurality of coupling elements are arranged along a peripheral direction and which has a substantially round external profile; a coupling belt on which a plurality of opposing coupling elements are arranged which are configured to form a positive-locking connection with the coupling elements of the two connecting elements for the mutual rotation-proof fixing of the two connecting elements; and a joint-connecting rod which is provided with an axial external thread, wherein the coupling belt is placed around the external profiles of the connecting flanges; wherein the coupling elements of the two connecting elements are connected positively to the opposing coupling elements of the coupling belt; wherein one of the connecting elements is configured as a connecting strut of an aircraft or spacecraft and the other connecting element is configured as a joint, a joint housing, a joint connection, or a connection adapter for attaching the connecting strut in an aircraft or spacecraft; wherein the connecting element configured as a connecting strut is provided with an axial threaded hole which is configured to receive the axial external thread of the joint-connecting rod; wherein the other connecting element is configured as an annular connection adapter which is configured with an internal contour which corresponds to the external contour of the joint-connecting rod, for attachment onto the joint-connecting rod; wherein the connecting element, configured as an annular connection adapter, is attached onto the joint-connecting rod; and wherein the joint-connecting rod engages in the axial threaded hole in the connecting element, configured as a connecting strut, via the axial external thread. 2. The connection arrangement of claim 1 , wherein the joint-connecting rod is provided with an external longitudinal groove, wherein the internal contour of the connecting element configured as an annular connection adapter has a sliding knuckle for sliding in the longitudinal groove in the joint-connecting rod, and wherein the sliding knuckle engages in the longitudinal groove. 3. A method for fixing, in a rotation-proof manner, the connection arrangement of claim 1 , the method comprising: coaxially aligning the connecting flanges of the connecting elements; placing the coupling belt jointly around the external profiles of the connecting flanges; and positively connecting the coupling elements of the two connecting elements to the opposing coupling elements of the coupling belt. 4. The connection system of claim 1 , wherein the coupling elements or the opposing coupling elements are configured as pins and correspondingly the opposing coupling elements or the coupling elements are configured as complementarily formed pin apertures or pin seats. 5. The connection system of claim 4 , wherein the coupling belt is a cable tie. 6. The connection system of claim 1 , wherein the coupling elements or the opposing coupling elements are configured as barbs and correspondingly the opposing coupling elements or the coupling elements are configured as loops. 7. The connection system of claim 6 , wherein during interplay, the coupling elements and the opposing coupling elements form a hook-and-loop fastening. 8. The connection system of claim 1 , wherein the coupling elements and the opposing coupling elements are configured as pins. 9. The connection system of claim 8 , wherein the coupling elements and the opposing coupling elements are identically formed mushroom-shaped pins. 10. The connection system of claim 1 , wherein the coupling elements are produced integrally with the respective connecting flange. 11. The connection system of claim 10 , wherein the connecting elements are produced from a plastic material or metal by a 3D printing process. 12. The connection system of claim 1 , wherein the coupling belt is configured to vary in length in a peripheral direction.

Assignees

Inventors

Classifications

  • F16D1/101Primary

    without axial retaining means rotating with the coupling · CPC title

  • Adjustable connecting-rods · CPC title

  • the torque is transmitted via polygon shaped connections · CPC title

  • F16B2/08Primary

    using bands · CPC title

  • Couplings comprising a chain or strip surrounding two wheels arranged side by side and provided with teeth or the equivalent · CPC title

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What does patent US10272529B2 cover?
A connection system includes two connecting elements each having a respective connecting flange on which a plurality of coupling elements are arranged along a peripheral direction and which has a substantially round external profile; and a coupling belt, on which a plurality of opposing coupling elements are arranged which are configured to form a positive-locking connection with the coupling e…
Who is the assignee on this patent?
Airbus Operations Gmbh
What technology area does this patent fall under?
Primary CPC classification F16D1/101. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Apr 30 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).