GB1577352A - Gudgeon pin - Google Patents
Gudgeon pin Download PDFInfo
- Publication number
- GB1577352A GB1577352A GB1443877A GB1443877A GB1577352A GB 1577352 A GB1577352 A GB 1577352A GB 1443877 A GB1443877 A GB 1443877A GB 1443877 A GB1443877 A GB 1443877A GB 1577352 A GB1577352 A GB 1577352A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pin
- gudgeon
- piston
- bosses
- inner edge
- 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
Links
- 241001125877 Gobio gobio Species 0.000 title 1
- 241001125879 Gobio Species 0.000 claims description 28
- 238000003776 cleavage reaction Methods 0.000 claims description 2
- 230000007017 scission Effects 0.000 claims description 2
- 230000003014 reinforcing effect Effects 0.000 description 2
- 206010053615 Thermal burn Diseases 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000737 periodic effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J1/00—Pistons; Trunk pistons; Plungers
- F16J1/10—Connection to driving members
- F16J1/14—Connection to driving members with connecting-rods, i.e. pivotal connections
- F16J1/16—Connection to driving members with connecting-rods, i.e. pivotal connections with gudgeon-pin; Gudgeon-pins
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
- Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)
Description
(54) GUDGEON PIN
(71) We, KARL SCHMIDT GmbH, a body corporate organised under the laws of the German Federal Republic, of Christian
Schmidt-Strasse 8/12, 7107 Neckarsulm,
German Federal Republic, do hereby declare the invention, for which we pray that a patent may be granted to us, and the method by which it is to be performed, to be particularly described in and by the following statement:
This invention relates to a gudgeon pin for a piston, particularly for a piston for an internal combustion engine.
A gudgeon pin is a force-transmitting member, which connects a piston to a connecting rod. The forces acting on the piston deflect the latter and result in an oval deformation thereof. The periodic deformation of the pin, consisting of deflection and flattening, stresses the bosses for the pin in horizontal and vertical planes. When the gudgeon pin is dimensioned for adequate strength, the mean bearing load for the bosses for the pins is also tolerable, as a rule.
Because the lubrication is inadequate in most cases, the average bearing load must not exceed 600 kg./cm.2 with aluminium. Nevertheless, the deflection of the pin results in an application of loads to the inner upper portion of the bosses for the pin and these loads may be a multiple of the above mentioned mean value. Very high peak pressures arise particularly as the engine is started, as a rule, and in conjunction with a small clearance between the pin and the boss may result in excessively high stresses due to the oval deformation of the pin.
Extensive investigations have shown that, particularly in diesel engines, the highest stress arises in the piston at the upper inner edge of the hole for the pin.
In order to reduce the peak stresses in that
region, it is known, e.g., from W.-D. Ben
singer and A. Meyer: "Kolben, Pleuel und
Kurbelwelle bei schnellaufenden Verbrennungs - motren", Berlin/Göttingen/Heidel- berg, 1961, page 10, to form the inner end of
the gudgeon pin bosses with a radius of 1 mm. or to make the bosses for the pin so elastic in that region that the bosses can substantially conform to the deflection of the gudgeon pin without overstressing the piston material. It has also been proposed to form the inner edge of the bosses for the pin with a taper of 1:100.
It has also been proposed to shrink rightangled reinforcing rings on the outside periphery of the gudgeon pin bosses. As a result, that portion of the bosses on which the reinforcing ring has been shrunk expands less in the operating condition than the remaining portion of the bosses. In order to compnesate for this differential expansion, the bore in the boss is narrower toward the side of the shrunkon ring so that under operating conditions the bores will become cylindrical and assume the function of non-reinforced bores.
A gudgeon pin boss which has a bore that has an oval cross-sectional shape, the minor aixs of which is parallel to the longitudinal axis of the piston has also been proposed.
This design results in a minimum clearance between the pin boss and the pin and in a lower tendency to seize and lower noise.
It has further been proposed to shape the bores in the gudgeon pin bosses to allow for the mechanical and thermal loads applied by the piston pin. Because such a design of the bores in the piston bosses involves a relatively high expenditure, the provision of the bore with an edge which is radiussed circularly is still preferred in practice even though this design deos not minimize the load on the bosses for the pin.
According to the present invention there is provided a gudgeon pin for a piston, wherein the pin is recessed throughout a region which, when the pin is in a position in a piston, extends from the inner edge of each of the gudgeon bosses of the piston to the ajacent inner edge of a connecting rod small end bearing and around the entire periphery or part of the periphery of the pin, each recess having a conical taper in cross section and a depth at a given point which is at least as large as the deflection of the pin will be at the same point when the pin is in use under the design load.
With this design it is possible to arrange for the stresses which arise under maximum load at the apex, particularly adjacent to the upper inner edge of the bosses for the pin, to be distributed as uniformly as possible throughout the length over which the pin engages the boss in the bore thereof.
In order to ensure that the gudgeon pin will not be loaded at the edges, the depth of the recess at a given point is suitably slightly larger than the deflection of the pin will be at the same point. The recess is preferably conically tapered at an angle of 8 to 14'.
As a result of these measures, the stresses in the gudgeon pin bosses and in the connecting rod are kept within a permissible range so that an application of pressure by the edges and resulting cleavages are avoided.
In order to enable the invention to be more readily understood, reference will now be made to the accompanying drawing, which illustrates diagrammatically and by way of example an embodiment thereof, and which is an axial section through a piston.
Referring now to the drawing, there is shown a piston 3 having a gudgeon pin 4 mounted in bores 1 of the gudgeon pin bosses 2. The gudgeon pin 4 has two recesses 6, each of which extends from the inner edge of each boss into the region of the adjacent inner edge of a connecting rod small end bearing 5 and has a conical taper in cross-section, and a depth at a given point which is slightly larger than the deflection of the pin 4 will be at the same point when in use under the design load.
WHAT WE CLAIM IS:- 1. A gudgeon pin for a piston, wherein the pin is recessed throughout a region which, when the pin is in position in a piston, extends from the inner edge of each of the gudgeon bosses of the piston to the adjacent inner edge of a connecting rod small end bearing and around the entire periphery or part of the periphery of the pin, each recess having a conical taper in crosssection and a depth at a given point which is as least as great as the deflection of the pin at the same point will be under the design load.
2. A gudgeon pin as claimed in claim 1, wherein each recess has an angle of taper of 8 to 14'.
3. A gudgeon pin for a piston substantially as hereinbefore described with reference to the accompanying drawing.
**WARNING** end of DESC field may overlap start of CLMS **.
Claims (3)
1. A gudgeon pin for a piston, wherein the pin is recessed throughout a region which, when the pin is in position in a piston, extends from the inner edge of each of the gudgeon bosses of the piston to the adjacent inner edge of a connecting rod small end bearing and around the entire periphery or part of the periphery of the pin, each recess having a conical taper in crosssection and a depth at a given point which is as least as great as the deflection of the pin at the same point will be under the design load.
2. A gudgeon pin as claimed in claim 1, wherein each recess has an angle of taper of 8 to 14'.
3. A gudgeon pin for a piston substantially as hereinbefore described with reference to the accompanying drawing.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE19762615212 DE2615212A1 (en) | 1976-04-08 | 1976-04-08 | PISTON PIN |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1577352A true GB1577352A (en) | 1980-10-22 |
Family
ID=5974776
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1443877A Expired GB1577352A (en) | 1976-04-08 | 1977-04-05 | Gudgeon pin |
Country Status (5)
| Country | Link |
|---|---|
| JP (1) | JPS6027865B2 (en) |
| BR (1) | BR7702209A (en) |
| DE (1) | DE2615212A1 (en) |
| FR (1) | FR2347586A1 (en) |
| GB (1) | GB1577352A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2131518A (en) * | 1982-12-09 | 1984-06-20 | Teledyne Ind | Piston pin of internal combustion engine |
| WO2000000761A1 (en) * | 1998-06-27 | 2000-01-06 | Federal-Mogul Wiesbaden Gmbh | Piston-pin bushing |
| WO2003010446A1 (en) * | 2001-07-25 | 2003-02-06 | Empresa Brasileira De Compressores S.A. - Embraco | Mounting arrangement for the piston of a reciprocating hermetic compressor |
Families Citing this family (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE2927410A1 (en) * | 1979-07-06 | 1981-01-08 | Siemens Ag | Monitoring profiles of ground combustion engine cylinder bolts - using laser projection and position dependent transducer intensity comparison |
| DE2952117C2 (en) * | 1979-12-22 | 1983-11-17 | Deutsche Forschungs- Und Versuchsanstalt Fuer Luft- Und Raumfahrt E.V., 5300 Bonn | Piston pin |
| DE3036062C2 (en) * | 1980-09-25 | 1984-06-07 | Karl Schmidt Gmbh, 7107 Neckarsulm | Pistons for internal combustion engines |
| DE3120842A1 (en) * | 1981-05-26 | 1982-12-23 | Mahle Gmbh, 7000 Stuttgart | PISTON BOLT BEARING FOR A LIGHT METAL PISTON OF COMBUSTION ENGINES |
| US4712941A (en) * | 1985-12-16 | 1987-12-15 | Chrysler Motors Corporation | Tapered piston pin |
| DE3609019C1 (en) * | 1986-03-18 | 1987-09-10 | Mahle Gmbh | Method for the production of the hub hole of a trunk piston, particularly for internal combustion engines |
| DE4008242A1 (en) * | 1990-03-15 | 1991-09-19 | Mahle Gmbh | Method of reducing noise of IC engine - by mounting gudgeon pin in spring-loaded sliding bearings |
| JP2583557Y2 (en) * | 1991-10-23 | 1998-10-22 | 光洋精工株式会社 | Connecting rod connection structure of internal combustion engine |
| JP2565951Y2 (en) * | 1992-04-03 | 1998-03-25 | 株式会社ユニシアジェックス | Piston structure for internal combustion engine |
| US5542341A (en) * | 1994-08-24 | 1996-08-06 | Bristol Compressors, Inc. | Wrist pin construction |
| DE19522210C1 (en) * | 1995-06-23 | 1997-01-16 | Danfoss Compressors Gmbh | Piston compressor |
| US5549034A (en) * | 1995-10-06 | 1996-08-27 | Chrysler Corporation | Wrist pin for piston and connecting rod assembly |
| DE102004061097A1 (en) * | 2004-12-18 | 2006-06-22 | Schaeffler Kg | End profiling on plain bearing counterpart partners to reduce surface pressure |
| DE102005019984A1 (en) * | 2005-04-27 | 2006-11-09 | A. Friedr. Flender Ag | plain bearing |
| WO2007057320A1 (en) * | 2005-11-16 | 2007-05-24 | Schaeffler Kg | Plain bearing unit |
| WO2009097060A1 (en) * | 2008-01-31 | 2009-08-06 | The Timken Company | Piston and connecting rod assembly |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2387634A (en) * | 1944-01-24 | 1945-10-23 | Aluminum Co Of America | Piston connection |
| US2435935A (en) * | 1945-06-25 | 1948-02-10 | Eaton Mfg Co | Pin |
-
1976
- 1976-04-08 DE DE19762615212 patent/DE2615212A1/en not_active Ceased
-
1977
- 1977-03-31 FR FR7709676A patent/FR2347586A1/en active Pending
- 1977-04-05 GB GB1443877A patent/GB1577352A/en not_active Expired
- 1977-04-06 BR BR7702209A patent/BR7702209A/en unknown
- 1977-04-08 JP JP4088577A patent/JPS6027865B2/en not_active Expired
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2131518A (en) * | 1982-12-09 | 1984-06-20 | Teledyne Ind | Piston pin of internal combustion engine |
| WO2000000761A1 (en) * | 1998-06-27 | 2000-01-06 | Federal-Mogul Wiesbaden Gmbh | Piston-pin bushing |
| US6540403B1 (en) | 1998-06-27 | 2003-04-01 | Federal-Mogul Wiesbaden Gmbh | Piston-pin bushing |
| WO2003010446A1 (en) * | 2001-07-25 | 2003-02-06 | Empresa Brasileira De Compressores S.A. - Embraco | Mounting arrangement for the piston of a reciprocating hermetic compressor |
| US8549988B2 (en) | 2001-07-25 | 2013-10-08 | Whirlpool S.A. | Mounting arrangement for the piston of a reciprocating hermetic compressor |
| US9353862B2 (en) | 2001-07-25 | 2016-05-31 | Whirlpool S.A. | Piston for a reciprocating hermetic compressor |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS6027865B2 (en) | 1985-07-01 |
| DE2615212B2 (en) | 1979-04-05 |
| JPS52124564A (en) | 1977-10-19 |
| BR7702209A (en) | 1978-01-17 |
| DE2615212A1 (en) | 1977-10-13 |
| FR2347586A1 (en) | 1977-11-04 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PCNP | Patent ceased through non-payment of renewal fee |