GB1381276A - Repair of bottom plates of ingot moulds - Google Patents

Repair of bottom plates of ingot moulds

Info

Publication number
GB1381276A
GB1381276A GB3931271A GB3931271A GB1381276A GB 1381276 A GB1381276 A GB 1381276A GB 3931271 A GB3931271 A GB 3931271A GB 3931271 A GB3931271 A GB 3931271A GB 1381276 A GB1381276 A GB 1381276A
Authority
GB
United Kingdom
Prior art keywords
repair
plate
bottom plate
recess
crack
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
GB3931271A
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.)
Hilti AG
Original Assignee
Hilti 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 Hilti AG filed Critical Hilti AG
Priority to GB3931271A priority Critical patent/GB1381276A/en
Publication of GB1381276A publication Critical patent/GB1381276A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00Restoring or reconditioning objects
    • B23P6/04Repairing fractures or cracked metal parts or products, e.g. castings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Surgical Instruments (AREA)

Abstract

1381276 Welding by fusion; ingot moulds; jointing HILTI AG 10 July 1972 [21 Aug 1971] 39312/71 Headings B3R B3F and B3V A method of repairing a crack 14 in the haematite iron bottom plate 11 of an ingot mould, comprises forming a recess 36 in the top surface of said bottom plate so as to extend across the crack, forming at least one anchorage hole 37, as by burning with a thermic lance, in said bottom plate at each side of the crack so as to open into said recess, each said hole, e.g. bulb or pear shaped, having a cross-section, at a distance from, but parallel to, the plane of, its opening into the recess, at least one dimension of which is greater than the corresponding dimension at said opening, positioning in said recess a repair plate 38 having apertures 39 corresponding with the anchorage holes, and filling said holes and apertures with weld metal which fuses with the repair plate and anchors with the bottom plate. As shown, two repair plates are used for respective cracks 13, 14. The repair may be further improved by welding around the periphery of the repair plate(s), by using a repair plate having an H-shape (Fig. 9, not shown), or widened ends (Fig. 10, not shown), so as to provide repair plate/bottom plate interlock, by repeating the repair at the bottom surface of the bottom plate, or by securing auxiliary strengthening plates 44 to the side faces of the bottom plate by nail-like fasteners 45 driven in by a cartridge-actuated tool. A method using the repair plate 38 and weld metal filled holes and apertures, wherein the plate is applied to the bottom plate side faces (Figs. 3, 4, not shown), is disclosed but not claimed. Reference has been directed by the Comptroller to Specification 1,150,014.
GB3931271A 1971-08-21 1971-08-21 Repair of bottom plates of ingot moulds Expired GB1381276A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3931271A GB1381276A (en) 1971-08-21 1971-08-21 Repair of bottom plates of ingot moulds

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3931271A GB1381276A (en) 1971-08-21 1971-08-21 Repair of bottom plates of ingot moulds

Publications (1)

Publication Number Publication Date
GB1381276A true GB1381276A (en) 1975-01-22

Family

ID=10408880

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3931271A Expired GB1381276A (en) 1971-08-21 1971-08-21 Repair of bottom plates of ingot moulds

Country Status (1)

Country Link
GB (1) GB1381276A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0258596A2 (en) * 1986-07-21 1988-03-09 The Boeing Company Method and apparatus for repairing a hole in a structural wall of composite laminate
US4916880A (en) * 1986-07-21 1990-04-17 The Boeing Company Apparatus for repairing a hole in a structural wall of composite material
US5190611A (en) * 1991-02-13 1993-03-02 The Boeing Company Bearing load restoration method for composite structures
US6291555B1 (en) 2000-07-26 2001-09-18 Illinois Tool Works Inc Highly viscous chemical anchoring adhesive
US6403678B1 (en) 2000-07-26 2002-06-11 Illinois Tool Works, Inc. Rope of chemical anchoring adhesive
US6402434B1 (en) 2000-07-26 2002-06-11 Illinois Tool Works, Inc. Method of applying chemical anchoring adhesive
US6420458B1 (en) 2000-07-26 2002-07-16 Illinois Tool Works, Inc. Solid amine-cured anchoring adhesive
US7226650B2 (en) 2004-07-01 2007-06-05 Illinois Tool Works Inc. Wrapped highly viscous chemical anchoring adhesive
US8517641B2 (en) 2009-07-21 2013-08-27 Illinois Tool Works Inc. Anchoring adhesive combination and integrated method of applying it
US8725446B2 (en) 2009-07-08 2014-05-13 Hommel-Etamic Gmbh Method for determining the shape of a workpiece
CN103846611A (en) * 2012-12-06 2014-06-11 中国二十冶集团有限公司 Repair method for base frame crack of cutting equipment

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0258596A2 (en) * 1986-07-21 1988-03-09 The Boeing Company Method and apparatus for repairing a hole in a structural wall of composite laminate
EP0258596A3 (en) * 1986-07-21 1989-08-23 The Boeing Company Method and apparatus for repairing a hole in a structural wall of composite laminate
US4916880A (en) * 1986-07-21 1990-04-17 The Boeing Company Apparatus for repairing a hole in a structural wall of composite material
US4978404A (en) * 1986-07-21 1990-12-18 The Boeing Company Method for repairing a hole in a structural wall of composite material
US5190611A (en) * 1991-02-13 1993-03-02 The Boeing Company Bearing load restoration method for composite structures
US6403678B1 (en) 2000-07-26 2002-06-11 Illinois Tool Works, Inc. Rope of chemical anchoring adhesive
US6291555B1 (en) 2000-07-26 2001-09-18 Illinois Tool Works Inc Highly viscous chemical anchoring adhesive
US6402434B1 (en) 2000-07-26 2002-06-11 Illinois Tool Works, Inc. Method of applying chemical anchoring adhesive
US6420458B1 (en) 2000-07-26 2002-07-16 Illinois Tool Works, Inc. Solid amine-cured anchoring adhesive
US7226650B2 (en) 2004-07-01 2007-06-05 Illinois Tool Works Inc. Wrapped highly viscous chemical anchoring adhesive
US8725446B2 (en) 2009-07-08 2014-05-13 Hommel-Etamic Gmbh Method for determining the shape of a workpiece
US8517641B2 (en) 2009-07-21 2013-08-27 Illinois Tool Works Inc. Anchoring adhesive combination and integrated method of applying it
CN103846611A (en) * 2012-12-06 2014-06-11 中国二十冶集团有限公司 Repair method for base frame crack of cutting equipment

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee