GB2193282A - Cranking mechanism - Google Patents

Cranking mechanism Download PDF

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Publication number
GB2193282A
GB2193282A GB08600078A GB8600078A GB2193282A GB 2193282 A GB2193282 A GB 2193282A GB 08600078 A GB08600078 A GB 08600078A GB 8600078 A GB8600078 A GB 8600078A GB 2193282 A GB2193282 A GB 2193282A
Authority
GB
United Kingdom
Prior art keywords
connecting rod
crankpins
crankshaft
cranking mechanism
slide ways
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.)
Granted
Application number
GB08600078A
Other versions
GB2193282B (en
GB8600078D0 (en
Inventor
Dr Thomas Tsoi-Hei Ma
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 GB8600078A priority Critical patent/GB2193282B/en
Publication of GB8600078D0 publication Critical patent/GB8600078D0/en
Publication of GB2193282A publication Critical patent/GB2193282A/en
Application granted granted Critical
Publication of GB2193282B publication Critical patent/GB2193282B/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H21/00Gearings comprising primarily only links or levers, with or without slides
    • F16H21/10Gearings comprising primarily only links or levers, with or without slides all movement being in, or parallel to, a single plane
    • F16H21/16Gearings comprising primarily only links or levers, with or without slides all movement being in, or parallel to, a single plane for interconverting rotary motion and reciprocating motion
    • F16H21/18Crank gearings; Eccentric gearings
    • F16H21/22Crank gearings; Eccentric gearings with one connecting-rod and one guided slide to each crank or eccentric
    • F16H21/28Crank gearings; Eccentric gearings with one connecting-rod and one guided slide to each crank or eccentric with cams or additional guides
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B41/00Engines characterised by special means for improving conversion of heat or pressure energy into mechanical power
    • F02B41/02Engines with prolonged expansion
    • F02B41/04Engines with prolonged expansion in main cylinders

Abstract

A cranking mechanism comprising a crankshaft (26), two non-aligned crankpins (12, 24) on the crankshaft (26), two slider blocks (18, 20) journalled for rotation about the respective crankpins (12, 24), and a connecting rod (10) having two mutually inclined slide ways (14, 16) each receiving and guiding a respective one of the slide blocks (18, 20). By appropriate selection of the inclination of the slide ways (14, 16) relative to the longitudinal axis of the connecting rod (10), and the direction and the extent of the offset of the crankpins (12, 24) the locus of the connecting rod can be varied within broad limits. <IMAGE>

Description

SPECIFICATION Cranking mechanism The present invention relates to a cranking mechanism that is to say a mechanism for converting reciprocating motion into rotary motion or vice versa.
The conventional form of cranking mechanism used in an internal combustion engine comprises a crankshaft having an eccentric crank pin which follows a circular path. The cranking pin is connected by way of a connecting rod to a piston which is guided in a cylinder to undergo a reciprocating motion during rotation of the crankshaft.
If the crankshaft rotates with constant speed, the result of this geometry is that the position of the piston as a function of time approximates to a sinusoid. The minor variation from a perfect sinusoid results from the fact that the connecting rod pivots during the course of the cycle and this causes the projection of the length of the connecting rod onto the axis of the cylinder to vary.
From the thermodynamic viewpoint, this relationship of the piston position with respect to time is not ideal and it is desirable to be able deviate from this generally sinusoidal relationship so as to vary the proportion of the cycle time that the piston spends in different positions in the cylinder.
The present invention seeks to provide a cranking mechansim which enables the lower end of a connecting rod to follow other than a circular path during the course of rotation of a crankshaft to which the connecting rod is coupled.
According to the present invention, there is provided a cranking mechanism comprising a crankshaft, two non-aligned crankpins on the crankshaft, two slider blocks journalled for rotation about the respective crankpins, and a connecting rod having two mutually inclined slide ways each receiving and guiding a respective one of the slide blocks.
Preferably, the slide ways on the connecting rod are mutually orthogonal.
The angle of inclipation of the slide ways in relation to the longitudinal axis of the connecting rod determines the proportion of the load or thrust which must be born by the respective slideways and crankpins. To spread the load evenly between the two crankpins and slide ways, it is preferred to arrange the slide ways at an angle in the range of from 30 to 60 to the axis of the connecting rod. This inclination also affects the locus of the connecting rod and must be taken into consideration when designing the cranking mechanism to meet particular objectives.
In the preferred embodiment, the slideways are each disposed at an angle of 45" to the longitudinal axis of the connecting rod.
The axes of the crankpins may be offset from one another in a radial or tangential direction in relation to the rotational axis of the crankshaft.
For an internal combustion, it is preferred to offset the crankpins in a radial direction. This has the effect of causing the locus of the lower end of the connecting rod to follow a path which resembles an inclined egg. The result of this locus on the motion of the piston is that the piston dwells slightly near the top dead centre position giving more time to complete combustion. The modified motion of the piston also assists in scavenging and generally improves the engine efficiency.
It is important to note that though the invention finds use in an internal combustion engine, it can be used in other reciprocating machines and in each case it provides the freedom to determine the locus of the connecting rod so as to adapt the reciprocating motion to the needs of the cycle carried out by the machine.
The invention will now be described further, by way of example, with reference to the accompanying drawings, in which: Figure 1 is a schematic exploded view of a cranking mechanism of the invention, and Figure 2 is a diagram illustrating the locus of the ends of the connecting rod.
In Fig. 1, a connecting rod 10 is formed with a conventional little end 12. In place of the usual big end bearing, the connecting rod is formed at its lower end with two orthogonal slide ways 14 and 16 which are formed one on each side of the connecting rod 10.
Each slide way 14, 16 receives and guides a respective one of two slider 18, 20, the connecting rod lower end being split to permit assembly. When received in the slide ways, the sliders 18, 20 can move in the directions indicated by arrows without applying any force to the connecting rod whereas movement at right angles to this direction moves the connecting rod 10. It can be seen therefore that the movement of the lower end of the connecting rod has two orthogonal components each determined by the position of a respective slider in the direction of that component.
The sliders 18 and 20 are slit so that they may be assembled about crankpins 22 and 24 eccentrically mounted on a crankshaft 26. The locus of the lower of the connecting rod is determined by the positions of the two crankpins pins relative to the axis of the crankshaft and upon the angle of inclication of the slide ways 14 and 16 relative to the longitudinal axis of the connecting rod 10.
For the arrangement illustrated in Fig. 1, the locus of movement of the connecting rod ends is shown in Fig. 2 calibrated in degrees of rotation of the crankshaft. This locus can readily be computed given that the nominal centre of the crossover of the two slide ways will always be determined uniquely by the po sition of the two crankpins.
As can be seen from Fig. 2, the locus of the lower end of the connecting rod is egg shaped and is inclined relative to the axis of the piston. This shape gives rise to several advantages which will now be described.
There is a dwell period in the piston displacement just behind tdc (from tdc to 30 deg atdc) where the combustion chamber volume increment above the clearance volume is reduced by approximately 50%. This approaches the ideal combustion condition at constant volume with positive work to a greater degree than the conventional crank giving better ther mal efficiency, extended lean burn capability and lower hydrocarbon emission because of higher gas temperatures.
This is followed by a faster expansion stroke, another dwell period of the piston just behind bdc (from bdc to 30 abtc), and a faster exhaust stroke.
The same piston-crank movements repeated for the next two strokes give a faster induction and better dynamic charging immediately behind bdc (larger trapped volume), followed by a faster compression to reach tdc.
The thrust angle of the controd is reduced by about 15% allowing a smaller l/r ratio and and/or less friction, less side-thrust.
The locus of the lower end of the connecting rod is determined by the separation of the crankpins, the direction of the offset of the crankpins in relation to the crank radius and the inclination of the slide ways in relation to the longitudinal axis of the connecting rod.
Variations of these parameters can allow the locus to be varied at will.
The asymmetrical configuration described above is preferred for the reasons stated but it should be mentioned that other arrangement also yield certain advantages. In particular, it is possible to retain symmetry of the locus of the connecting rod and while this looses the ideal of constant volume combustion it reduces the side-thrust by up to 30%.

Claims (6)

1. A cranking mechanism comprising a crankshaft, two non-aligned crankpins on the crankshaft, two slider blocks journalled for rotation about the respective crankpins, and a connecting rod having two mutually inclined slide ways each receiving and guiding a respective one of the slide blocks.
2. A cranking mechanism as claimed in claim 1, wherein the slide ways on the connecting rod are mutually orthogonal.
3. A cranking mechanism as claimed in claim 2, wherein the slideways are each disposed at an angle in the range from 30 to 60 to the longitudinal axis of the connecting rod.
4. A cranking mechanism as claimed in claim 3, wherein the slideways are each disposed at an angle of 45" to the longitudinal axis of the connecting rod.
5. A cranking mechanism as claimed in any preceding claim, wherein the crankpins are offset in a radial direction with respect to the crankshaft axis.
6. A cranking mechanism constructed and adapted to operate substantially as herein described with reference to and as illustrated in the accompanying drawings.
GB8600078A 1986-01-03 1986-01-03 Cranking mechanism Expired GB2193282B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8600078A GB2193282B (en) 1986-01-03 1986-01-03 Cranking mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8600078A GB2193282B (en) 1986-01-03 1986-01-03 Cranking mechanism

Publications (3)

Publication Number Publication Date
GB8600078D0 GB8600078D0 (en) 1986-02-12
GB2193282A true GB2193282A (en) 1988-02-03
GB2193282B GB2193282B (en) 1989-10-25

Family

ID=10590886

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8600078A Expired GB2193282B (en) 1986-01-03 1986-01-03 Cranking mechanism

Country Status (1)

Country Link
GB (1) GB2193282B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2409884A (en) * 2004-01-09 2005-07-13 Ford Global Tech Llc Variable length connecting rod for variable compression ratio i.c. engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2409884A (en) * 2004-01-09 2005-07-13 Ford Global Tech Llc Variable length connecting rod for variable compression ratio i.c. engine
US7028647B2 (en) 2004-01-09 2006-04-18 Ford Global Technologies, Llc Variable compression ratio connecting rod for internal combustion engine
GB2409884B (en) * 2004-01-09 2007-09-05 Ford Global Tech Llc Variable compression ratio connecting rod for internal combustion engine

Also Published As

Publication number Publication date
GB2193282B (en) 1989-10-25
GB8600078D0 (en) 1986-02-12

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PCNP Patent ceased through non-payment of renewal fee