GB1381276A - Repair of bottom plates of ingot moulds - Google Patents
Repair of bottom plates of ingot mouldsInfo
- 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
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P6/00—Restoring or reconditioning objects
- B23P6/04—Repairing 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.
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)
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 |
-
1971
- 1971-08-21 GB GB3931271A patent/GB1381276A/en not_active Expired
Cited By (13)
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 |