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GB642602A - Improvements in method of repairing cracked or fractured metal walls - Google Patents

Improvements in method of repairing cracked or fractured metal walls

Info

Publication number
GB642602A
GB642602A GB21241/47A GB2124147A GB642602A GB 642602 A GB642602 A GB 642602A GB 21241/47 A GB21241/47 A GB 21241/47A GB 2124147 A GB2124147 A GB 2124147A GB 642602 A GB642602 A GB 642602A
Authority
GB
United Kingdom
Prior art keywords
groove
crack
metal
bars
lugs
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
GB21241/47A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB642602A publication Critical patent/GB642602A/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)
  • Working Measures On Existing Buildindgs (AREA)

Abstract

642,602. Dowel pins. SCOTT. L. B. Aug. 5, 1947, No. 21241. Convention date, March 3,1939. [Class 89(ii)] [Also in Group XXII] To repair a body at points subjected to strain or to reinforce or prevent leakage from a cracked or fractured body, e.g., engine cylinder or manifold, the metal adjacent the crack, &c., is removed, recesses are formed in two opposite walls of the opening so formed, and pliable metal sealing means is pressed in to engage said recesses. A groove 11 may be cut in a casting 10 to overlie a crack a and holes 14 be drilled in the side walls of said groove. One of each pair of opposed holes may be threaded at 14<1> and bars 17 successively screwed in after pliable metal or other packing 16 has been inserted. Each bar of the first row is pressed to enter the unscrewed end and flatten it before further packing and another row of bars are introduced, This is repeated until the groove is filled as at Fig. 6. If desired the groove may be cut at right angles to the crack so that the repair will distribute the strain over a greater area of sound metal. Any number of bars may be used and the greater part of the groove may be filled with packing only as in Fig. 8. The side walls of the groove may be sloped. A strip 18, Fig. 16, with pairs of lugs 19 to enter the holes 14 may be arranged lengthwise of the crack in place of a row of bars 17. Fig. 13 shows a modified strip, the groove being cut to fit the lugs 20. Figs. 14, 15 show a form for surface application, the lugs 25 engaging corresponding recesses giving additional strength. When the weakened metal surrounding a crack is extensive, a long bar, Fig. 19, with 'pins at its ends to engage sound metal. may be used.
GB21241/47A 1939-03-03 1947-08-05 Improvements in method of repairing cracked or fractured metal walls Expired GB642602A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US642602XA 1939-03-03 1939-03-03

Publications (1)

Publication Number Publication Date
GB642602A true GB642602A (en) 1950-09-06

Family

ID=22054672

Family Applications (1)

Application Number Title Priority Date Filing Date
GB21241/47A Expired GB642602A (en) 1939-03-03 1947-08-05 Improvements in method of repairing cracked or fractured metal walls

Country Status (1)

Country Link
GB (1) GB642602A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4916880A (en) * 1986-07-21 1990-04-17 The Boeing Company Apparatus for repairing a hole in a structural wall of composite material
EP1857218A1 (en) * 2006-05-18 2007-11-21 Siemens Aktiengesellschaft Method for repairing a component and a component
CN102101220A (en) * 2011-03-30 2011-06-22 储勤旺 Method for welding rupture of large casting equipment

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4916880A (en) * 1986-07-21 1990-04-17 The Boeing Company Apparatus for repairing a hole in a structural wall of composite material
EP1857218A1 (en) * 2006-05-18 2007-11-21 Siemens Aktiengesellschaft Method for repairing a component and a component
WO2007134883A1 (en) * 2006-05-18 2007-11-29 Siemens Aktiengesellschaft Method of repairing a component, and a component
CN102101220A (en) * 2011-03-30 2011-06-22 储勤旺 Method for welding rupture of large casting equipment

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