GB1478174A - Method of fixing - Google Patents

Method of fixing

Info

Publication number
GB1478174A
GB1478174A GB4037274A GB4037274A GB1478174A GB 1478174 A GB1478174 A GB 1478174A GB 4037274 A GB4037274 A GB 4037274A GB 4037274 A GB4037274 A GB 4037274A GB 1478174 A GB1478174 A GB 1478174A
Authority
GB
United Kingdom
Prior art keywords
panel
flange
support member
hole
ferrule
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.)
Expired
Application number
GB4037274A
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.)
Novartis AG
Original Assignee
Ciba Geigy AG
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 Ciba Geigy AG filed Critical Ciba Geigy AG
Priority to GB4037274A priority Critical patent/GB1478174A/en
Priority to JP11101675A priority patent/JPS587781B2/en
Priority to US05/755,607 priority patent/US4056878A/en
Publication of GB1478174A publication Critical patent/GB1478174A/en
Expired 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)
  • Joining Of Building Structures In Genera (AREA)
  • Connection Of Plates (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)

Abstract

1478174 Building panels CIBA-GEIGY (UK) Ltd 18 Aug 1975 [17 Sept 1974] 40372/74 Heading E1B [Also in Division F2] A sandwich panel 21, 22, e.g. forming the floor of an aircraft fuselage, is secured to a support member 26, e.g. of an airframe, by a method comprising the steps of inserting a ferrule 23 which consists of a cylindrical body with a flange 24 into a hole extending through the thickness of the panel so that the flange contacts one of the skins, e.g. the lower skin, of the panel, bonding the flange to the skin, e.g. by a thermosetting adhesive, placing the panel against the support member 26 with the face of the panel carrying the flange 24 in contact with the support member, passing a bolt 25 into the hole in the panel on the side opposite the flange and then passing its shank through a hole in the flange 24 of smaller diameter than the head of the bolt, so that the latter is seated within the ferrule, and screwing the bolt to the support member, e.g. by utilizing a nut as shown. The ferrule may not extend wholly through the panel (Fig. 2B, not shown). In either arrangement, the entrance to the hole on the side of the panel opposite the flange may be afterwards closed by a plug 27.
GB4037274A 1974-09-17 1974-09-17 Method of fixing Expired GB1478174A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB4037274A GB1478174A (en) 1974-09-17 1974-09-17 Method of fixing
JP11101675A JPS587781B2 (en) 1974-09-17 1975-09-16 Sand Germany Chippanel Nokoteihouhou
US05/755,607 US4056878A (en) 1974-09-17 1976-12-29 Method of fixing a sandwich panel to a support

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4037274A GB1478174A (en) 1974-09-17 1974-09-17 Method of fixing

Publications (1)

Publication Number Publication Date
GB1478174A true GB1478174A (en) 1977-06-29

Family

ID=10414565

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4037274A Expired GB1478174A (en) 1974-09-17 1974-09-17 Method of fixing

Country Status (2)

Country Link
JP (1) JPS587781B2 (en)
GB (1) GB1478174A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0316190A1 (en) * 1987-11-11 1989-05-17 Avdel Systems Limited Bush
DE102005034891A1 (en) * 2005-07-26 2007-02-01 Airbus Deutschland Gmbh Lateral force joint for airplane, has fuselage strap comprising hollow cylinder having diameter corresponding to diameter of through-bore of spar, so that cylinder is fitted into through-bore of spar
EP3730747A1 (en) * 2019-04-25 2020-10-28 Airbus Operations Limited Joining components

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0316190A1 (en) * 1987-11-11 1989-05-17 Avdel Systems Limited Bush
DE102005034891A1 (en) * 2005-07-26 2007-02-01 Airbus Deutschland Gmbh Lateral force joint for airplane, has fuselage strap comprising hollow cylinder having diameter corresponding to diameter of through-bore of spar, so that cylinder is fitted into through-bore of spar
DE102005034891B4 (en) * 2005-07-26 2007-06-14 Airbus Deutschland Gmbh Cross-cage connection
US8104709B2 (en) 2005-07-26 2012-01-31 Airbus Deutschland Gmbh Lateral force joint
EP3730747A1 (en) * 2019-04-25 2020-10-28 Airbus Operations Limited Joining components
US11505329B2 (en) 2019-04-25 2022-11-22 Airbus Operations Limited Joining components

Also Published As

Publication number Publication date
JPS587781B2 (en) 1983-02-12
JPS5156521A (en) 1976-05-18

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Legal Events

Date Code Title Description
PS Patent sealed
PE20 Patent expired after termination of 20 years

Effective date: 19950817