GB2197228A - Method of assembling components - Google Patents

Method of assembling components Download PDF

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Publication number
GB2197228A
GB2197228A GB08627244A GB8627244A GB2197228A GB 2197228 A GB2197228 A GB 2197228A GB 08627244 A GB08627244 A GB 08627244A GB 8627244 A GB8627244 A GB 8627244A GB 2197228 A GB2197228 A GB 2197228A
Authority
GB
United Kingdom
Prior art keywords
assembly
sub
components
liquid
cooling
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.)
Withdrawn
Application number
GB08627244A
Other versions
GB8627244D0 (en
Inventor
Robert Anthony Marshall
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.)
Ford Motor Co
Original Assignee
Ford Motor Co
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 Ford Motor Co filed Critical Ford Motor Co
Priority to GB08627244A priority Critical patent/GB2197228A/en
Publication of GB8627244D0 publication Critical patent/GB8627244D0/en
Priority to US07/118,686 priority patent/US4843697A/en
Priority to ES87310034T priority patent/ES2022375B3/en
Priority to DE8787310034T priority patent/DE3771176D1/en
Priority to JP62287184A priority patent/JPS63221930A/en
Priority to EP87310034A priority patent/EP0267800B1/en
Priority to CA000551794A priority patent/CA1293113C/en
Publication of GB2197228A publication Critical patent/GB2197228A/en
Withdrawn legal-status Critical Current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
    • B23P19/00Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
    • B23P19/04Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for assembling or disassembling parts
    • B23P19/042Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for assembling or disassembling parts specially adapted for combustion engines
    • B23P19/043Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for assembling or disassembling parts specially adapted for combustion engines for inserting piston-connecting rods assemblies in cylinders
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P19/00Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F7/00Casings, e.g. crankcases or frames
    • F02F7/0043Arrangements of mechanical drive elements
    • F02F7/0046Shape of casings adapted to facilitate fitting or dismantling of engine parts
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49229Prime mover or fluid pump making
    • Y10T29/49231I.C. [internal combustion] engine making
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/4981Utilizing transitory attached element or associated separate material
    • Y10T29/49812Temporary protective coating, impregnation, or cast layer
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/53Means to assemble or disassemble
    • Y10T29/536Piston ring inserter or remover

Description

1 GB2197228A 1
SPECIFICATION
Method of assembling components The present invention relates to the auto70 mated assembly of components.
Some engine parts present problems. in au tomated assembly on account of the fact that one of the parts being assembled is itself a sub-assembly of components which are free to move relative to one another. One case where this problem is encounted is in fitting a piston and connecting rod assembly complete with piston rings into a cylinder bore. The rings are free to move and project from the piston, making it necessary for them to be compressed during insertion. Furthermore the piston can swivel on the connecting rod and this makes alignment awkward. However, alignment is necessary since the connecting rod must be used to drive the piston into the cylinder bore.
The current trend is to assemble a complete crankshaft for a cylinder block and to intro duce all the pistons at the same time. into their respective bores and here there is a still further degree of movement between the con necting rods and the crankshaft.
Another case where this problem is encoun tered is in fitting a rocker shaft complete with all the rockers onto a cylinder head. The rock ers are again free to swivel and it is difficult for an automated process using robots to align all the rockers with their respective valves and push rods or cams prior to tighten- 100 ing the shaft mountings.
Other situations where this problem is en counted will be apparent from the examples given above but for purposes of illustration, the invention will be described only by refer ence to the assembly of a crankshaft in a cylinder block.
This case has been selected as it exempli fies a situation with a large number of rela tively movable parts and it also demonstrates the difficulty presented by the fact that there is little space available for all the clamping devices that would be required to restrict the various degrees of freedom of the sub-as sembly during its introduction into the cylinder block.
Because of these problems, it has hitherto been necessary for the sub-assembly of the crankshaft, connecting rods and pistons to be mounted manually into an engine block but this of course is costly and the invention seeks to provide a method of assembly which enables the mounting of such sub-assemblies to be automated.
According to the present invention, there is provided a method of assembling two parts of which one part is a sub-assembly formed of a plurality of relatively movable components, the method comprising the steps of holding the components of the sub-assembly in their de- sired relative positions for assembly, cooling the sub-assembly sufficiently to prevent relative movement between the components of the sub-assembly, and offering the sub-assembly to the other part while the components of the sub-assembly are locked against one another.
It is common in an engine for two of the relatively movable components of a sub-as- sembly to be formed of different metals or alloys of which the coefficients of thermal expansion differ. For example, the connecting rod may be made of aluminium and the gudgeon pin of steel with the result that freezing alone is sufficient to create an interference fit between the two components and prevent their relative movement during assembly.
However, though temperature change alone will work satisfactorily in some situations as outlined above, it cannot be applied where the difference in thermal expansion coefficients is not capable of creating the desired interference fit, either by virtue of the nature of the materials or in view of the clearance between the components. Even when freezing alone does suffice to lock the components, the temperature at which locking occurs will vary on account of manufacturing tolerances.
It is therefore preferred to coat the compo- nents with a liquid prior to cooling the sub- assembly and to cool the sub-assembly at least to the freezing point of the liquid. Here, the liquid takes up any gaps arising from tolerances or otherwise and upon freezing locks the components firmly to one another. The freezing point is of course constant and the temperature at which the locking up of the components will occur does not vary with tolerances. 105 Some of the requirements which should be satisfied by the liquid are as follows: 1. the liquid should freeze at a safe temperature, and should not be a wax but relatively incompressible when solid, 110 2. the liquid should not be corrosive to the components as it may remain for a considerable time in contact with them, 3. the liquid should key into the surface of the components and form a high friction bond, and 4. the surface tension of the liquid should permit it to creep readily into gaps between the components.
Water and oil mixtures are particularly pre- ferred for use as the liquid in the present invention as they are readily available, being often used as lubricants during machining of components. Furthermore, they satisfy the conditions set out above, they are inexpensive and do not present any form of hazard. However, other liquids may be used in at least some applications, for example vegetable oils.
If water is used in the liquid, then inhibitors are preferably added to prevent corrosion.
Water has the further advantage of expand- 2 GB2197228A 2 ing on freezing and this creates very considerable forces capable of holding even the piston rings compressed after they have been removed from the freezing rig.
The invention will now be described further, by way of example, with reference to the accompanying drawing which shows the mounting of a crankshaft sub-assembly into an engine block.
A crankshaft sub-assembly 10 in the draw- ing is to be introduced into an engine block 30. The crankshaft sub-assembly 10 com prises the crankshaft 12, the pistons 14 with their piston rings, the connecting rods 16, the big end bearings 18 and the main bearings 20. The main bearings are formed of a bear ing housing 22, a bearing cap 24 and bearing shells (not shown) arranged between the crankshaft and the pillar block formed by the housing 22 and the cap 24.
The bolts 26 for tightening the main bear ings are also used for securing the main bear ings to the cylinder block 30 and therefore in the sub-assembly the main bearings are not tightened. To prevent their falling apart, the bearing housing is formed with a wire strap 32 which engages in a groove or over a ridge in the bearing cap 24 to hold the two to gether temporarily during the assembly proce dure.
It should be mentioned that in a conven tional engine, the bearing housing 22 is formed integrally with the engine block 30.
However the separation of the bearing hous ings 22 irom the engine block simplifies as sembly and is itself the subject of copencling Patent Application No. 8625171 filed in the United Kingdom on 21st October, 1986.
The crankshaft sub-assembly can be seen to comprise several parts which are free to ro tate. In particular, the connecting rods 16 can move relative to the crankshaft 18, the pis tons 14 can pivot relative to the connecting rods 16 and the bearing housings 22 can ro tate about the crankshaft. A complicated ro bot would be needed to hold such an as sembly in the position illustrated to enable the sub-assembly 10 to be introduce into the en gine block 30. Furthermore, during this intro duction, the piston rings would need to be compressed and while the engine block illus trated has been designed to facilitate access to the rings (by the separation from the en gine block of the bearing housings 22 and of the skirt of the crank case) in other engines 120 access to the rings is very limited.
During the course of mass production of en gines, the crankshaft sub-assemblies are pre pared off line and a stack of sub-assemblies are made available to the main engine pro duction line ready for mounting in engine blocks. To facilitate the mounting of the sub assemblies in the engine blocks, the sub-as semblies 10 are immersed in or sprayed with a liquid. The liquid is preferably water with added soluble oil and corrosion inhibitors. The coated sub-assemblies are now mounted in suitable jigs which hold their components as required and they are then stored in a freezer.
The liquid penetrates all the gaps between the component parts of the subassembly and on freezing locks the components together so that they remain in the required position even after removal from the jig.
The jig in which the sub-assembly is mounted will in this case compress the piston rings, correctly line up the connecting rods, the bearing housing and the crankshaft and will maintain the pistons on the centre lines of the cylinder bores 40.
After removal of the sub-assemblies 10 from the freezer, they are merely lowered into the engine blocks without any additional complication since the entire sub-assembly is now rigid and all its components are correctly aligned with the mating parts of the engine block. Furthermore, the clearance has been in creased for the pistons since they are now at a lower temperature than the engine block.
Water and oil mixtures are used as lubri cants during machining of most crankshaft parts and it is usual to smear the surface of a bearing with a lubricant during assembly. The required liquid coating on the relatively mov- able components of the sub-assembly may therefore in practice already be present on the surfaces and no separate coating step may be required. It can also be seen that the components are usually covered with a liquid during conventional assembly of an engine and no additional problem is created as regards corrosion or contamination by using the present invention.
It can be seen therefore that the invention considerably reduces the complexity of any automated machine required for the mounting of the crankshaft and also reduces the risk of damage being caused to components by a robot trying to assemble them by force when they are not correctly aligned.

Claims (4)

  1. CLAIMS 1. A method of assembling two parts of which one part is a sub-
    assembly formed of a 11 plurality of relatively movable components, the method comprising the steps of holding the components of the sub-assembly in their desired relative positions for assembly, cooling the subassembly sufficiently to prevent relative movement between the components of the sub-assembly, and offering the sub-assembly to the other part while the components of the sub-assembly are locked against one another. 125
  2. 2. A method as claimed in claim 1, wherein prior to cooling, the subassembly is coated with a liquid and the sub-assembly is cooled at least sufficiently to freeze the liquid.
  3. 3. A method as claimed in claim 2, wherein the liquid is water containing soluble 3 GB2197228A 3 oils and corrosion inhibitors.
  4. 4. A method as claimed in any preceding claim, wherein the sub-assembly includes an engine crankshaft, connecting rods, pistons and piston rings, and in which the piston rings are compressed into the piston grooves prior to the cooling the sub-assembly.
    Published 1988 at The Patent Office, State House, 66/7 1 HighHolborn, London WC1R 4TP. Further copies may be obtained from The Patent Office, Sales Branch, St Mary Cray, Orpington, Kent BR5 3RD. Printed by Burgess & Son (Abingdon) Ltd. Con. 1/87.
GB08627244A 1986-11-14 1986-11-14 Method of assembling components Withdrawn GB2197228A (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
GB08627244A GB2197228A (en) 1986-11-14 1986-11-14 Method of assembling components
US07/118,686 US4843697A (en) 1986-11-14 1987-11-09 Method of assembling components
ES87310034T ES2022375B3 (en) 1986-11-14 1987-11-13 METHOD FOR ASSEMBLING COMPONENTS.
DE8787310034T DE3771176D1 (en) 1986-11-14 1987-11-13 METHOD FOR ASSEMBLING PARTS.
JP62287184A JPS63221930A (en) 1986-11-14 1987-11-13 Method of assembling part
EP87310034A EP0267800B1 (en) 1986-11-14 1987-11-13 Method of assembling components
CA000551794A CA1293113C (en) 1986-11-14 1987-11-13 Method of assemblying components

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08627244A GB2197228A (en) 1986-11-14 1986-11-14 Method of assembling components

Publications (2)

Publication Number Publication Date
GB8627244D0 GB8627244D0 (en) 1986-12-17
GB2197228A true GB2197228A (en) 1988-05-18

Family

ID=10607347

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08627244A Withdrawn GB2197228A (en) 1986-11-14 1986-11-14 Method of assembling components

Country Status (7)

Country Link
US (1) US4843697A (en)
EP (1) EP0267800B1 (en)
JP (1) JPS63221930A (en)
CA (1) CA1293113C (en)
DE (1) DE3771176D1 (en)
ES (1) ES2022375B3 (en)
GB (1) GB2197228A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10024768A1 (en) * 2000-05-19 2001-11-22 Volkswagen Ag Method and device for assembling a composite of housing, shafts and rotating masses

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5271487A (en) * 1992-11-27 1993-12-21 Dana Corporation Stabilized driven disk assembly and method of installing a clutch including same
US6745465B1 (en) * 1994-05-11 2004-06-08 Caterpillar Inc Method for assembling an apparatus, such as a fuel injector, using select fit of dimensional control features
DE19713996C2 (en) * 1997-04-04 1999-04-22 Abb Patent Gmbh Device for installing an internal combustion engine assembly consisting of a piston and a connecting rod
FR2784043B1 (en) * 1998-10-02 2000-10-27 Renault METHOD AND DEVICE FOR MOUNTING A CONNECTING ROD-PISTON ASSEMBLY IN A CYLINDER HOUSING
US6516511B1 (en) * 2000-06-29 2003-02-11 Caterpillar Inc Position sensor for piston ring compressor
DE10150717A1 (en) * 2001-10-13 2003-04-17 Daimler Chrysler Ag Mounting device for an internal combustion engine and assembly method for this purpose
US8667657B2 (en) * 2006-01-18 2014-03-11 Abb Technology Ag Method and apparatus for engine piston installation by use of industrial robots
CN102416551A (en) * 2011-09-08 2012-04-18 龙工(上海)挖掘机制造有限公司 Assembly method of excavator structural member steel jacket
GB2568070B (en) * 2017-11-03 2020-05-06 Caterpillar Energy Solutions Gmbh Coupling mechanism
AT522976B1 (en) * 2020-03-13 2021-04-15 Avl List Gmbh LARGE COMBUSTION ENGINE

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2387971A (en) * 1942-01-14 1945-10-30 Aspin Frank Metcalf Cylinder liner and cylinder
US2855664A (en) * 1955-12-21 1958-10-14 Rohr Aircraft Corp Method of machining honeycomb core
FR1590582A (en) * 1968-05-10 1970-04-20
DD203274A1 (en) * 1981-12-18 1983-10-19 Hans Standhardt DEVICE FOR ASSEMBLING A CYLINDER ASSEMBLY OF PISTON PISTON ENGINES
US4480368A (en) * 1983-05-02 1984-11-06 Caterpillar Tractor Co. Unitary installation of engine cylinder liner, piston and rod
US4530141A (en) * 1983-05-02 1985-07-23 Caterpillar Tractor Co. Unitary removal of engine cylinder liner, piston and rod

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10024768A1 (en) * 2000-05-19 2001-11-22 Volkswagen Ag Method and device for assembling a composite of housing, shafts and rotating masses

Also Published As

Publication number Publication date
DE3771176D1 (en) 1991-08-08
JPS63221930A (en) 1988-09-14
ES2022375B3 (en) 1991-12-01
US4843697A (en) 1989-07-04
CA1293113C (en) 1991-12-17
EP0267800B1 (en) 1991-07-03
EP0267800A1 (en) 1988-05-18
GB8627244D0 (en) 1986-12-17

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WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)