BE561327A - - Google Patents

Info

Publication number
BE561327A
BE561327A BE561327DA BE561327A BE 561327 A BE561327 A BE 561327A BE 561327D A BE561327D A BE 561327DA BE 561327 A BE561327 A BE 561327A
Authority
BE
Belgium
Prior art keywords
blank
sleeve
valve spring
punch
desc
Prior art date
Application number
Other languages
English (en)
French (fr)
Publication of BE561327A publication Critical patent/BE561327A/fr

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES, PROFILES OR LIKE SEMI-MANUFACTURED PRODUCTS OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C23/00Extruding metal; Impact extrusion
    • B21C23/02Making uncoated products
    • B21C23/03Making uncoated products by both direct and backward extrusion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21KMAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K21/00Making hollow articles not covered by a single preceding sub-group
    • B21K21/08Shaping hollow articles with different cross-section in longitudinal direction, e.g. nozzles, spark-plugs

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Forging (AREA)
BE561327D BE561327A (en:Method)

Publications (1)

Publication Number Publication Date
BE561327A true BE561327A (en:Method)

Family

ID=183311

Family Applications (1)

Application Number Title Priority Date Filing Date
BE561327D BE561327A (en:Method)

Country Status (1)

Country Link
BE (1) BE561327A (en:Method)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1984003130A1 (en) * 1983-02-07 1984-08-16 Boeing Co Unitary fastener insert for structural sandwich panels

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1984003130A1 (en) * 1983-02-07 1984-08-16 Boeing Co Unitary fastener insert for structural sandwich panels

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