METHOD OF MAKING CONNECTING ROD

A method of manufacturing a component formed of parts capable of being separated for reassembly around another component. The process starts by taking separate, e.g., rod (3, 3') and cap (5, 5') forgings and coining or forging them together prior to machining. The mating surfaces of the fo...

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Hauptverfasser: MCINERNEY, TERRY, M, BECKER, PAUL, C, SHORT, JAMES, M, BIGGERSTAFF, PAUL, MYERS, MARTIN, R, PATTEN, JAMES, W, STEVENS, ROBERT, POTTER, DENNIS, P
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creator MCINERNEY, TERRY, M
BECKER, PAUL, C
SHORT, JAMES, M
BIGGERSTAFF, PAUL
MYERS, MARTIN, R
PATTEN, JAMES, W
STEVENS, ROBERT
POTTER, DENNIS, P
description A method of manufacturing a component formed of parts capable of being separated for reassembly around another component. The process starts by taking separate, e.g., rod (3, 3') and cap (5, 5') forgings and coining or forging them together prior to machining. The mating surfaces of the forgings are formed with a ridge-groove (9) or a dimple/lug-recess (12) configuration giving them a self-locating ability. After machining, the forgings are fractured along the original division to obtain two uniquely matched surfaces that need no further processing before being reassembled, e.g., to form a connecting rod for an internal combustion engine. L'invention a pour objet un procédé de fabrication d'un élément constitué de parties pouvant être séparées pour être ultérieurement ré-assemblées autour d'un autre élément. Ce procédé consiste à prendre des pièces forgées séparées, par exemple une bielle (3, 3') et un chapeau (5, 5') pour les forger ou les emboutir ensemble avant de les usiner. Les surfaces correspondantes des pièces forgées présentent une configuration de type arête-rainure (9) ou bosse/évidement-oeillet (12), ce qui leur permet de s'auto-positionner. Après l'usinage, les pièces forgées sont fracturées le long de leur division initiale pour donner deux pièces correspondantes uniques ne nécessitant pas d'autre traitement avant leur ré-assemblage, par exemple, pour former une bielle pour un moteur à combustion interne.
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Les surfaces correspondantes des pièces forgées présentent une configuration de type arête-rainure (9) ou bosse/évidement-oeillet (12), ce qui leur permet de s'auto-positionner. 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The process starts by taking separate, e.g., rod (3, 3') and cap (5, 5') forgings and coining or forging them together prior to machining. The mating surfaces of the forgings are formed with a ridge-groove (9) or a dimple/lug-recess (12) configuration giving them a self-locating ability. After machining, the forgings are fractured along the original division to obtain two uniquely matched surfaces that need no further processing before being reassembled, e.g., to form a connecting rod for an internal combustion engine. L'invention a pour objet un procédé de fabrication d'un élément constitué de parties pouvant être séparées pour être ultérieurement ré-assemblées autour d'un autre élément. Ce procédé consiste à prendre des pièces forgées séparées, par exemple une bielle (3, 3') et un chapeau (5, 5') pour les forger ou les emboutir ensemble avant de les usiner. 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The process starts by taking separate, e.g., rod (3, 3') and cap (5, 5') forgings and coining or forging them together prior to machining. The mating surfaces of the forgings are formed with a ridge-groove (9) or a dimple/lug-recess (12) configuration giving them a self-locating ability. After machining, the forgings are fractured along the original division to obtain two uniquely matched surfaces that need no further processing before being reassembled, e.g., to form a connecting rod for an internal combustion engine. L'invention a pour objet un procédé de fabrication d'un élément constitué de parties pouvant être séparées pour être ultérieurement ré-assemblées autour d'un autre élément. Ce procédé consiste à prendre des pièces forgées séparées, par exemple une bielle (3, 3') et un chapeau (5, 5') pour les forger ou les emboutir ensemble avant de les usiner. Les surfaces correspondantes des pièces forgées présentent une configuration de type arête-rainure (9) ou bosse/évidement-oeillet (12), ce qui leur permet de s'auto-positionner. Après l'usinage, les pièces forgées sont fracturées le long de leur division initiale pour donner deux pièces correspondantes uniques ne nécessitant pas d'autre traitement avant leur ré-assemblage, par exemple, pour former une bielle pour un moteur à combustion interne.</abstract><edition>6</edition><oa>free_for_read</oa></addata></record>
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subjects BEARINGS
BLASTING
BROACHING
CASTING
COMBINED OPERATIONS
ELEMENTS OR CRANKSHAFT MECHANISMS
ENGINEERING ELEMENTS AND UNITS
FILING
FLEXIBLE SHAFTS
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
HEATING
LIGHTING
LIKE OPERATIONS FOR WORKING METAL BY REMOVING MATERIAL, NOTOTHERWISE PROVIDED FOR
MACHINE TOOLS
MAKING METALLIC POWDER
MANUFACTURE OF ARTICLES FROM METALLIC POWDER
MECHANICAL ENGINEERING
METAL-WORKING NOT OTHERWISE PROVIDED FOR
OTHER WORKING OF METAL
PERFORMING OPERATIONS
PLANING
POWDER METALLURGY
ROTARY BODIES OTHER THAN GEARING ELEMENTS
SAWING
SCRAPING
SHAFTS
SHEARING
SLOTTING
THERMAL INSULATION IN GENERAL
TRANSPORTING
UNIVERSAL MACHINE TOOLS
WEAPONS
WORKING METALLIC POWDER
title METHOD OF MAKING CONNECTING ROD
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