Immobilised insert

Leigh  Shippen; Ashley Clack; David Lambert; Balaji Aresh; Paul Snowdon

Immobilised insert

Leigh Shippen (Inventor), Ashley Clack (Inventor), David Lambert (Inventor), Balaji Aresh (Inventor), Paul Snowdon (Inventor)

Research output: Patent

Abstract

A method and apparatus are disclosed. The method includes the steps of providing an elongate sheet having a uniform thickness and a first and further spaced apart long edge, to a first pair of a plurality of spaced apart pairs of opposed forming roller elements, and via the pairs of roller elements, progressively forming a cross-sectional profile in the sheet that comprises a body portion comprising a folded central region of the sheet and a first and further wing portion that each extend away from the body portion and terminate at a respective long edge of the sheet, and securing adjacent regions of the wing portions and/or opposed regions of the body portion together thereby providing a windable elongate tape element having laterally immobilised wing portions.

Original language	English
Patent number	US20190316711A1
IPC	F16L 11/16,B21C 37/12 ,F16L 11/08
Priority date	6/12/16
Filing date	1/12/17
Publication status	Published - 17 Oct 2019

Access to Document

https://patentimages.storage.googleapis.com/15/24/95/7f6e61f9272e61/US20190316711A1.pdf

1 Patent

Immobilised insert
Shippen, L., Clack, A., Lambert, D., Aresh, B. & Snowdon, P., 10 Aug 2021, IPC No. F16L 11/16 , B21C 37/12 , F16L 11/08 , Patent No. US11085561B2, 30 Nov 2017, Priority date 6 Dec 2016, Priority No. GB1620745.8
Research output: Patent

Open Access

Cite this

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abstract = "A method and apparatus are disclosed. The method includes the steps of providing an elongate sheet having a uniform thickness and a first and further spaced apart long edge, to a first pair of a plurality of spaced apart pairs of opposed forming roller elements, and via the pairs of roller elements, progressively forming a cross-sectional profile in the sheet that comprises a body portion comprising a folded central region of the sheet and a first and further wing portion that each extend away from the body portion and terminate at a respective long edge of the sheet, and securing adjacent regions of the wing portions and/or opposed regions of the body portion together thereby providing a windable elongate tape element having laterally immobilised wing portions.",

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TY - PAT

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AU - Shippen, Leigh

AU - Clack, Ashley

AU - Lambert, David

AU - Aresh, Balaji

AU - Snowdon, Paul

PY - 2019/10/17

Y1 - 2019/10/17

N2 - A method and apparatus are disclosed. The method includes the steps of providing an elongate sheet having a uniform thickness and a first and further spaced apart long edge, to a first pair of a plurality of spaced apart pairs of opposed forming roller elements, and via the pairs of roller elements, progressively forming a cross-sectional profile in the sheet that comprises a body portion comprising a folded central region of the sheet and a first and further wing portion that each extend away from the body portion and terminate at a respective long edge of the sheet, and securing adjacent regions of the wing portions and/or opposed regions of the body portion together thereby providing a windable elongate tape element having laterally immobilised wing portions.

AB - A method and apparatus are disclosed. The method includes the steps of providing an elongate sheet having a uniform thickness and a first and further spaced apart long edge, to a first pair of a plurality of spaced apart pairs of opposed forming roller elements, and via the pairs of roller elements, progressively forming a cross-sectional profile in the sheet that comprises a body portion comprising a folded central region of the sheet and a first and further wing portion that each extend away from the body portion and terminate at a respective long edge of the sheet, and securing adjacent regions of the wing portions and/or opposed regions of the body portion together thereby providing a windable elongate tape element having laterally immobilised wing portions.

M3 - Patent

M1 - US20190316711A1

Y2 - 2017/12/01

ER -

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Abstract

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Research output

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Cite this