GB2017857A - An insert for installation in a sandwich panel - Google Patents

An insert for installation in a sandwich panel

Info

Publication number
GB2017857A
GB2017857A GB7910535A GB7910535A GB2017857A GB 2017857 A GB2017857 A GB 2017857A GB 7910535 A GB7910535 A GB 7910535A GB 7910535 A GB7910535 A GB 7910535A GB 2017857 A GB2017857 A GB 2017857A
Authority
GB
United Kingdom
Prior art keywords
sandwich panel
panel
insert
installation
hole
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
GB7910535A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Fairchild Fasteners Europe Camloc GmbH
Original Assignee
Camloc Fastener GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Camloc Fastener GmbH filed Critical Camloc Fastener GmbH
Publication of GB2017857A publication Critical patent/GB2017857A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
    • F16B5/01—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening elements specially adapted for honeycomb panels

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Plates (AREA)
  • Insertion Pins And Rivets (AREA)
  • Dowels (AREA)
  • Laminated Bodies (AREA)

Abstract

An insert for installation in a sandwich panel having a fragile, low-density core comprises two sleeve members each of which has a shank portion 24, 34 and a flange portion 28, 42 on one end thereof. The flange portions fit into a through-hole in this panel. The shank portions have such outer and inner diameters, respectively, as to get telescopically pushed together within this through-hole. Further the flange portions 24, 34 are provided with circumferential lips 32, 46 resting against the outer surfaces of said sandwich panel. At least one of the flanged portions 28 is provided with eccentrically located passages 48, 50 for filling in potting compound and for venting the space inside the sandwich panel thus providing for reinforcement of a fastener hole in said light-weight panel after curing of said compound. <IMAGE>
GB7910535A 1978-03-25 1979-03-26 An insert for installation in a sandwich panel Withdrawn GB2017857A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19782813098 DE2813098A1 (en) 1978-03-25 1978-03-25 USE FOR REINFORCEMENT OF A FASTENING HOLE IN A LIGHTWEIGHT STRUCTURAL COMPOSITE PANEL

Publications (1)

Publication Number Publication Date
GB2017857A true GB2017857A (en) 1979-10-10

Family

ID=6035441

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7910535A Withdrawn GB2017857A (en) 1978-03-25 1979-03-26 An insert for installation in a sandwich panel

Country Status (5)

Country Link
JP (1) JPS54132052A (en)
DE (1) DE2813098A1 (en)
FR (1) FR2420681A1 (en)
GB (1) GB2017857A (en)
IT (1) IT1112374B (en)

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2506405A1 (en) * 1981-05-19 1982-11-26 Matra Assembly piece for lightweight panels - has cylindrical central section with pair of coaxial collars fitting into ends to abut against opposite faces of panel
EP0266638A2 (en) * 1986-11-05 1988-05-11 Dürkopp Systemtechnik GmbH Tool support beam for a jet-cutting apparatus
EP0316190A1 (en) * 1987-11-11 1989-05-17 Avdel Systems Limited Bush
US6656603B2 (en) * 1996-01-12 2003-12-02 The Boeing Company Multisheet sandwich structures with throughholes
EP1537983A1 (en) * 2003-12-04 2005-06-08 Airbus France Device for equipping a hole in a panel and equipped panel
WO2009130082A1 (en) * 2008-04-24 2009-10-29 Airbus Operations Gmbh Process for inserting a bushing into a component, and bushing
DE102014014624A1 (en) 2014-10-01 2016-04-07 Frank Weidermann Insert for a connection with sandwich components
WO2017049130A1 (en) * 2015-09-17 2017-03-23 Sps Technologies, Llc Adjustable insert for sandwich structures
EP3217022A1 (en) * 2016-03-07 2017-09-13 The Boeing Company Adjustable-height inserts and related methods
US9976583B2 (en) 2016-04-04 2018-05-22 The Boeing Company Threaded adjustable-height inserts and related methods
US10099767B2 (en) 2015-08-04 2018-10-16 The Boeing Company Sandwich panel inserts and related methods
US10197078B2 (en) 2015-09-17 2019-02-05 Sps Technologies, Llc Robust adjustable panel insert
CN109668044A (en) * 2019-01-03 2019-04-23 耿世超 A kind of magnalium titanium alloy pressure-resisting plate and its method with sandwich
GB2568756A (en) * 2017-11-28 2019-05-29 Airbus Operations Ltd Fastener
GB2607711A (en) * 2021-04-23 2022-12-14 Illinois Tool Works Method of retaining a sleeve with low force
US11850810B2 (en) 2021-05-18 2023-12-26 The Boeing Company Skin-bonded threaded inserts, sandwich panels including the same, and related methods

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3213213A1 (en) * 1982-04-08 1983-10-13 Messerschmitt-Bölkow-Blohm GmbH, 8000 München INSTALLATION DEVICE FOR DOWELS IN LAYER COMPOSITE PANELS
US4653246A (en) * 1984-01-05 1987-03-31 Hepler Jacque P Insulation board for attachment to walls
DE19812814B4 (en) * 1998-03-17 2006-08-24 Gebo Glas-Elemente-Befestigungssysteme Oftersheim Gmbh Glass bar connection
DE10128054C2 (en) * 2001-06-01 2003-07-10 Inst Konstruktion Und Verbundb Laminated composite panel with openings as well as methods and tools for their manufacture
DE10241289B4 (en) * 2002-09-06 2004-12-09 Sacs Gmbh Use for lightweight panels or the like
DE102017112174A1 (en) * 2017-06-01 2018-12-06 Inspire AG für mechatronische Produktionssysteme und Fertigungstechnik Power transmission assembly and insert

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2506405A1 (en) * 1981-05-19 1982-11-26 Matra Assembly piece for lightweight panels - has cylindrical central section with pair of coaxial collars fitting into ends to abut against opposite faces of panel
EP0266638A2 (en) * 1986-11-05 1988-05-11 Dürkopp Systemtechnik GmbH Tool support beam for a jet-cutting apparatus
EP0266638A3 (en) * 1986-11-05 1990-02-07 Durkopp Systemtechnik Gmbh Tool support beam for a jet-cutting apparatus
EP0316190A1 (en) * 1987-11-11 1989-05-17 Avdel Systems Limited Bush
US6656603B2 (en) * 1996-01-12 2003-12-02 The Boeing Company Multisheet sandwich structures with throughholes
EP1537983A1 (en) * 2003-12-04 2005-06-08 Airbus France Device for equipping a hole in a panel and equipped panel
FR2863185A1 (en) * 2003-12-04 2005-06-10 Airbus France DEVICE FOR EQUIPPING A HOLE IN A PANEL AND PANEL THUS EQUIPPED
US7503524B2 (en) 2003-12-04 2009-03-17 Airbus France Device for equipping a hole in a panel, and panel thus equipped
WO2009130082A1 (en) * 2008-04-24 2009-10-29 Airbus Operations Gmbh Process for inserting a bushing into a component, and bushing
DE102014014624A1 (en) 2014-10-01 2016-04-07 Frank Weidermann Insert for a connection with sandwich components
US10730604B2 (en) 2015-08-04 2020-08-04 The Boeing Company Sandwich panel inserts and related methods
US10099767B2 (en) 2015-08-04 2018-10-16 The Boeing Company Sandwich panel inserts and related methods
WO2017049130A1 (en) * 2015-09-17 2017-03-23 Sps Technologies, Llc Adjustable insert for sandwich structures
US11009055B2 (en) * 2015-09-17 2021-05-18 Sps Technologies, Llc Robust adjustable panel insert
US10197078B2 (en) 2015-09-17 2019-02-05 Sps Technologies, Llc Robust adjustable panel insert
US9975309B2 (en) 2015-09-17 2018-05-22 Sps Technologies, Llc Adjustable insert for sandwich structures
US9862166B2 (en) 2016-03-07 2018-01-09 The Boeing Company Adjustable-height inserts and related methods
EP3217022A1 (en) * 2016-03-07 2017-09-13 The Boeing Company Adjustable-height inserts and related methods
US10228003B2 (en) 2016-04-04 2019-03-12 The Boeing Company Threaded adjustable-height inserts and related methods
US9976583B2 (en) 2016-04-04 2018-05-22 The Boeing Company Threaded adjustable-height inserts and related methods
GB2568756A (en) * 2017-11-28 2019-05-29 Airbus Operations Ltd Fastener
US11332231B2 (en) 2017-11-28 2022-05-17 Airbus Operations Limited Hollow fastener for coupling aerospace structures
CN109668044A (en) * 2019-01-03 2019-04-23 耿世超 A kind of magnalium titanium alloy pressure-resisting plate and its method with sandwich
CN109668044B (en) * 2019-01-03 2021-05-28 浙江松发复合新材料有限公司 Aluminum-magnesium-titanium alloy compression-resistant plate with sandwich structure
GB2607711A (en) * 2021-04-23 2022-12-14 Illinois Tool Works Method of retaining a sleeve with low force
GB2607711B (en) * 2021-04-23 2023-07-19 Illinois Tool Works Method of retaining a sleeve with low force
US11850810B2 (en) 2021-05-18 2023-12-26 The Boeing Company Skin-bonded threaded inserts, sandwich panels including the same, and related methods

Also Published As

Publication number Publication date
DE2813098A1 (en) 1979-10-04
FR2420681A1 (en) 1979-10-19
FR2420681B3 (en) 1982-03-26
JPS54132052A (en) 1979-10-13
IT7921268A0 (en) 1979-03-23
IT1112374B (en) 1986-01-13

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)