FR2149990A5 - Metal parts prodn from several elements - eg for aircraft using process which reduces fatigue - Google Patents

Metal parts prodn from several elements - eg for aircraft using process which reduces fatigue

Info

Publication number
FR2149990A5
FR2149990A5 FR7228632A FR7228632A FR2149990A5 FR 2149990 A5 FR2149990 A5 FR 2149990A5 FR 7228632 A FR7228632 A FR 7228632A FR 7228632 A FR7228632 A FR 7228632A FR 2149990 A5 FR2149990 A5 FR 2149990A5
Authority
FR
France
Prior art keywords
aircraft
metal parts
parts
several elements
reduces fatigue
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
FR7228632A
Other languages
French (fr)
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.)
Imperial Metal Industries Kynoch Ltd
Imperial Metal Industries Ltd
Original Assignee
Imperial Metal Industries Kynoch Ltd
Imperial Metal Industries Ltd
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 Imperial Metal Industries Kynoch Ltd, Imperial Metal Industries Ltd filed Critical Imperial Metal Industries Kynoch Ltd
Application granted granted Critical
Publication of FR2149990A5 publication Critical patent/FR2149990A5/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21DWORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21D47/00Making rigid structural elements or units, e.g. honeycomb structures
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21HMAKING PARTICULAR METAL OBJECTS BY ROLLING, e.g. SCREWS, WHEELS, RINGS, BARRELS, BALLS
    • B21H7/00Making articles not provided for in the preceding groups, e.g. agricultural tools, dinner forks, knives, spoons
    • B21H7/16Making articles not provided for in the preceding groups, e.g. agricultural tools, dinner forks, knives, spoons turbine blades; compressor blades; propeller blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Agronomy & Crop Science (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)

Abstract

Process for mfr. of metal assemblies which have >=2 elements comprises assembling two metal elements of which one is two parts produced from a single piece and is connected at one point so that the two parts have a free end which is remote from the connection point and at which the second element comes into contact when it is in its posn. for assembly with the first element. The two elements are joined by diffusion by pressure, or by rolling the first element through its free end onto the second element. The process is applied to aircraft parts comprising metal plates with spacers and is designed to reduce fatigue in the parts.
FR7228632A 1971-08-09 1972-08-08 Metal parts prodn from several elements - eg for aircraft using process which reduces fatigue Expired FR2149990A5 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3730271 1971-08-09

Publications (1)

Publication Number Publication Date
FR2149990A5 true FR2149990A5 (en) 1973-03-30

Family

ID=10395400

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7228632A Expired FR2149990A5 (en) 1971-08-09 1972-08-08 Metal parts prodn from several elements - eg for aircraft using process which reduces fatigue

Country Status (2)

Country Link
DE (1) DE2239214A1 (en)
FR (1) FR2149990A5 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4219469A1 (en) * 1992-06-13 1993-12-16 Asea Brown Boveri Component subject to high temperatures, in particular turbine blade, and method for producing this component
DE4219470A1 (en) * 1992-06-13 1993-12-16 Asea Brown Boveri Component for high temperatures, in particular turbine blade, and method for producing this component

Also Published As

Publication number Publication date
DE2239214A1 (en) 1973-02-22

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Legal Events

Date Code Title Description
ST Notification of lapse