US3769880A - Cylinder housing with dry cylinder liners - Google Patents
Cylinder housing with dry cylinder liners Download PDFInfo
- Publication number
- US3769880A US3769880A US00230413A US3769880DA US3769880A US 3769880 A US3769880 A US 3769880A US 00230413 A US00230413 A US 00230413A US 3769880D A US3769880D A US 3769880DA US 3769880 A US3769880 A US 3769880A
- Authority
- US
- United States
- Prior art keywords
- liner
- bore
- wall surfaces
- arrangement according
- cylinder
- 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 - Lifetime
Links
- 238000002485 combustion reaction Methods 0.000 claims abstract description 8
- 229910052751 metal Inorganic materials 0.000 claims description 10
- 239000002184 metal Substances 0.000 claims description 10
- 230000008646 thermal stress Effects 0.000 claims description 3
- 238000002360 preparation method Methods 0.000 claims description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 4
- 230000035882 stress Effects 0.000 description 3
- 238000010276 construction Methods 0.000 description 2
- 239000000543 intermediate Substances 0.000 description 2
- 238000003754 machining Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- 240000006927 Foeniculum vulgare Species 0.000 description 1
- 235000004204 Foeniculum vulgare Nutrition 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- -1 for example Inorganic materials 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F1/00—Cylinders; Cylinder heads
- F02F1/004—Cylinder liners
Definitions
- the present invention relates to a cylinder housing with dry cylinder liners especially for internal combustionengines.
- Such types of liners are normally oversize inder liners and of the cylinder bores. This makes necessary repeated after'finishing operations. Further form-changes lead to the-formation of gaps and hollow spaces between the cylinder bore and the cylinder liner. In internal combustion engines hot gasespenetrate from the. combustion space into these hollow spaces andattackthesurfaces thereof.
- a further disadvantage are the large forces which have to be applied during the disassembly of the cylinder liners.
- the cylinder bores may be, considerably damaged'by the strong frictionconnected therewith.
- a press is not necessary therefor. Under certain circumstances, already asingle hammer blow on an emplaced interme diate platesuffices in order to drive the cylinder liner intoitsend position within the cylinder bore. Stresses and subsequent deformations of the cylinder liner resulting therefrom are avoided by the slight pressing-in force or pressure.
- the further significant advantage results therefrom that the cylinder liners can be finishmachined already prior to installation so that afterfinishing. operations may be dispensed with.
- a good abutment of the cylinder liner. in the cylinder bore with sufficient adhesion and favorable heat transfer is achieved according .to the present invention in that also the cylinder bore tapers or converges in a conical shape.
- the cylinder liner additionally centers itself automatically during the introduction into the cylinder bore so that any canting is precluded.
- the angle of inclination of the outer surface-of the cylinder liner is larger than the angle'of inclination of the housingbore.
- the abutment pressure of the cylinder liner is largest at the hottest and most heavily stressed place within the area of the outer wall of the cylinder housing.
- the outer surface of the cylinder liner and/or the cylinder bore may be provided with a soft metal layer, for example, made from tin. Small surface inaccuracies are compensated thereby and the heat. transfer between cylinder liner and cylinder bore is considerably improved. ln-contradistinction to the bushes with a cylindrical .outer surface in which such a layer is destroyed during the pressing-in operation and is stripped off for the most part, this layer remains preserved with the cylinder liner in accordance with the present invention adapted to be inserted easily.
- I Accordingly, it is an objectof the present invention to provide'a cylinder housing with dry cylinder liners which obviates the disadvantages and drawbacks encountered in the prior art. 1 I i Another object of the present invention resides in a cylinder housing with dry cylinder liners which eliminates the need for large forces to assemble anddisassemble the cylinder liners in and from the cylinder bores. i r A further object of the presentinvention resides in a cylinder housing with dry cylinder liners whichpractically completely eliminates the danger of wear, ovalization and warping of the cylinder lizners and/or cylinder bores. I
- Still another object of the present invention resides in'a cylinder, housing with dry cylinder liners which not. only greatly reduces the amount of machining operations necessary but also reduces the. price for the manufacture and assembly thereof.
- a further object of thepresent invention resides in a cylinder housing with dry cylinder liners which eliminates special forms for the liner and/or the'cylinder bore, which avoids stresses and which improves the heat transfer.
- The'single figure is a cross-sectionalview through a cylinder housing of a piston internal combustion engine with a dry cylinder liner in accordance with thepresent invention.
- reference numeral 1 designates therein the cylinder bore of a cylinder housing 2 into which is inserted a dry cylinder liner 3.
- the flangeless end face 4 of the cylinder liner 3 is disposed in one and the same plane with the outer walls of the cylinder housing 2.
- the outersurface 6 of the cylinder liner 3 tapers conically in the inward direction from the end face 4 thereof.
- the angle of inclination a of the outer surface 6 amounts to about 25 minutes.
- the cylinder bore 1 also tapers conically in the inward direction.
- the angle of inclination a of the outer surface 6 of the cylinder liner 3 is about 4 minutes larger than the angle ofinclination B of the cylinder bore 1.
- Preferred dimensions for the tapering of the outer surface of the cylinder liner 3 lie between a cone of about 1 50 to a cone of about 1 125.
- the fine-finished or machined outer surface 6 is provided with a tin coating having a thickness of about five thousandths of a millimeter.
- the cylinder liner 3 can be secured rapidly and with out costly auxiliary means in the cylinder housing 2. For this purpose, one introduces the cylinder liner 3 into the cylinder bore 1 until it abuts with its outer surface 6 at the upper edge thereof. The cylinder liner 3 therefore immerses almost with its entire length into the cylinder bore 1. As a result of the conical construction of the cylinder bore 1 and of the cylinder liner 3, the latter centers itself. One places an intermediate plate (not shown) on the end face 4 of the cylinder liner 3 which projects, for example, with l/lO of its length, and one is able to press-in the cylinder liner 3 thereafter with a relatively small pressure until its end face 4 is flush with the outer wall 5 of the cylinder housing 2.
- the end face 4 of the cylinder liner 3 may also project by a small amount, for example, by a tenth of a millimeter, beyond the outer wall 5 of the cylinder housing 2. These differences in height may be compensated for in the assembled internal combustion engines by the seal inserted between the cylinder housing 2 and the cylinder head.
- the cylinder liner 3 is securely seated in the cylinder housing 2 after the pressing-in operation. its outer surface 6 abuts over the entire length or nearly over the entire length thereof in the cylinder bore 1. The abutment pressure is thereby largest in the most strongly loaded zone withinthe area of the outer wall 6 of the cylinder housing 2 and decreases from there uniformly in the inward direction.
- the soft tin layer at the outer surface 6 of the cylinder liner 3 equalizes any still existing, local form-deviations and improves the heat transfer from the cylinder liner 3 to the cylinder housing 2.
- any other soft metal for example, aluminum or copper may also be applied onto the outer surface of the cylinder liner 3.
- the cylinder liner 3 becomes disengaged readily from the cylinder bore 1 after overcoming an initial resistance and can be pulled out of the cylinder housing 2 simply and without damage to the outer surface 6 or to the cylinder bore 1.
- An arrangement for an internal combustion engine comprising: a cylinder housing having a bore delimited by inwardly facing bore walls, and a cylinder liner having outwardly facing liner wall surfaces, wherein said liner is positioned in said bore, wherein both said bore walls and liner wall surfaces are conically tapered with the angle of inclination of said bore walls with respect to a longitudinally extending central bore axis being different than the angle of inclination of said liner wall surfaces with respect to said bore axis, and wherein said liner is held in position in said bore exclusively by frictional engagement of said bore walls and liner wall surfaces.
- an upper end of said liner has a larger cross-sectional size than an opposite lower end of said liner such that the liner can be inserted from above into said bore.
- an upper end of said liner has a larger cross-sectional size than an opposite lower end of saidliner such that the liner can be inserted from above into said bore.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19691916168 DE1916168A1 (de) | 1969-03-28 | 1969-03-28 | Zylindergehaeuse mit trockenen Zylinderlaufbuechsen |
Publications (1)
Publication Number | Publication Date |
---|---|
US3769880A true US3769880A (en) | 1973-11-06 |
Family
ID=5729709
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US00230413A Expired - Lifetime US3769880A (en) | 1969-03-28 | 1972-02-29 | Cylinder housing with dry cylinder liners |
Country Status (4)
Country | Link |
---|---|
US (1) | US3769880A (enrdf_load_stackoverflow) |
DE (1) | DE1916168A1 (enrdf_load_stackoverflow) |
FR (1) | FR2039974A5 (enrdf_load_stackoverflow) |
GB (1) | GB1258705A (enrdf_load_stackoverflow) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3972234A (en) * | 1974-12-30 | 1976-08-03 | Osojnak Boris M | Liquid level indicator |
US4249381A (en) * | 1978-03-27 | 1981-02-10 | The Bendix Corporation | Master cylinder |
USRE31080E (en) * | 1978-03-27 | 1982-11-16 | The Bendix Corporation | Master cylinder |
US4385595A (en) * | 1980-12-09 | 1983-05-31 | Cummins Engine Company, Inc. | Bottom stop cylinder liner and engine assembly |
US4726571A (en) * | 1986-03-17 | 1988-02-23 | Lear Siegler, Inc. | Height control valve with spring return actuator |
US5320158A (en) * | 1993-01-15 | 1994-06-14 | Ford Motor Company | Method for manufacturing engine block having recessed cylinder bore liners |
US5365997A (en) * | 1992-11-06 | 1994-11-22 | Ford Motor Company | Method for preparing an engine block casting having cylinder bore liners |
WO2002068844A1 (en) * | 2001-02-21 | 2002-09-06 | Utex Industries, Inc. | Pump liner |
US6615901B2 (en) * | 2001-06-11 | 2003-09-09 | General Motors Corporation | Casting of engine blocks |
WO2003106842A1 (en) * | 2002-06-14 | 2003-12-24 | Jetstream Of Houston, Llp | High pressure reciprocating pump |
US6675699B1 (en) | 2000-09-25 | 2004-01-13 | Utex Industries, Inc. | Composite components for use in pumps |
US20060042770A1 (en) * | 2004-02-20 | 2006-03-02 | Newcomb Thomas P | Liner seat design for a foundry mold with integrated bore liner and barrel core features |
RU2382220C2 (ru) * | 2008-04-24 | 2010-02-20 | Федеральное государственное образовательное учреждение высшего профессионального образования "Чувашская государственная сельскохозяйственная академия" | Способ сборки цилиндропоршневой группы автотракторных двигателей |
US20150240741A1 (en) * | 2012-09-17 | 2015-08-27 | Federal-Mogul Burscheied GmbH | Cylinder sleeve with wear-resistant inner layer |
US11480131B2 (en) | 2018-09-17 | 2022-10-25 | GM Global Technology Operations LLC | Engine block for an internal combustion engine |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5340104U (enrdf_load_stackoverflow) * | 1976-04-27 | 1978-04-07 | ||
RU2162159C2 (ru) * | 1999-04-13 | 2001-01-20 | Государственное научно-производственное предприятие "Мотор" (ГНПП "Мотор") | Цилиндр поршневого двигателя |
DE102009024227B4 (de) * | 2009-06-08 | 2013-07-04 | Daimler Ag | Zylinderkurbelgehäuse |
Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US489949A (en) * | 1893-01-17 | harring- | ||
US970903A (en) * | 1910-04-23 | 1910-09-20 | John M Fennell | Steam-engine. |
US1420551A (en) * | 1921-05-10 | 1922-06-20 | Ivins Ellwood | Working-barrel tube |
US1788950A (en) * | 1929-04-11 | 1931-01-13 | Glen P Heiner | Cylinder |
US2060034A (en) * | 1933-06-22 | 1936-11-10 | Marvel Carbureter Co | Bonded metal bearings and method of making the same |
US2094254A (en) * | 1934-04-14 | 1937-09-28 | John T Brubaker | Packing for internal combustion engine cylinders |
US2204626A (en) * | 1936-11-12 | 1940-06-18 | Super Diesel Tractor Corp | Pump liner |
US2566769A (en) * | 1949-02-11 | 1951-09-04 | Kay Frank | Pipe coupling |
DE880411C (de) * | 1951-09-19 | 1953-06-22 | Carl Becken Fa | Schnellverbindung fuer Rohre verschiedenen Durchmessers |
DE886551C (de) * | 1951-01-10 | 1953-08-13 | Glacier Co Ltd | Gleitlager |
US3567257A (en) * | 1968-10-11 | 1971-03-02 | Connecticut Research & Mfg Cor | Tapered pipe joint |
-
1969
- 1969-03-28 DE DE19691916168 patent/DE1916168A1/de active Pending
-
1970
- 1970-03-20 GB GB1258705D patent/GB1258705A/en not_active Expired
- 1970-03-25 FR FR7010748A patent/FR2039974A5/fr not_active Expired
-
1972
- 1972-02-29 US US00230413A patent/US3769880A/en not_active Expired - Lifetime
Patent Citations (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US489949A (en) * | 1893-01-17 | harring- | ||
US970903A (en) * | 1910-04-23 | 1910-09-20 | John M Fennell | Steam-engine. |
US1420551A (en) * | 1921-05-10 | 1922-06-20 | Ivins Ellwood | Working-barrel tube |
US1788950A (en) * | 1929-04-11 | 1931-01-13 | Glen P Heiner | Cylinder |
US2060034A (en) * | 1933-06-22 | 1936-11-10 | Marvel Carbureter Co | Bonded metal bearings and method of making the same |
US2094254A (en) * | 1934-04-14 | 1937-09-28 | John T Brubaker | Packing for internal combustion engine cylinders |
US2204626A (en) * | 1936-11-12 | 1940-06-18 | Super Diesel Tractor Corp | Pump liner |
US2566769A (en) * | 1949-02-11 | 1951-09-04 | Kay Frank | Pipe coupling |
DE886551C (de) * | 1951-01-10 | 1953-08-13 | Glacier Co Ltd | Gleitlager |
DE880411C (de) * | 1951-09-19 | 1953-06-22 | Carl Becken Fa | Schnellverbindung fuer Rohre verschiedenen Durchmessers |
US3567257A (en) * | 1968-10-11 | 1971-03-02 | Connecticut Research & Mfg Cor | Tapered pipe joint |
Cited By (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3972234A (en) * | 1974-12-30 | 1976-08-03 | Osojnak Boris M | Liquid level indicator |
US4249381A (en) * | 1978-03-27 | 1981-02-10 | The Bendix Corporation | Master cylinder |
USRE31080E (en) * | 1978-03-27 | 1982-11-16 | The Bendix Corporation | Master cylinder |
US4385595A (en) * | 1980-12-09 | 1983-05-31 | Cummins Engine Company, Inc. | Bottom stop cylinder liner and engine assembly |
US4726571A (en) * | 1986-03-17 | 1988-02-23 | Lear Siegler, Inc. | Height control valve with spring return actuator |
US5365997A (en) * | 1992-11-06 | 1994-11-22 | Ford Motor Company | Method for preparing an engine block casting having cylinder bore liners |
US5771955A (en) * | 1992-11-06 | 1998-06-30 | Ford Global Technologies, Inc. | Core assembly manufacturing apparatus of casting engine blocks and method for making the assembly |
US5320158A (en) * | 1993-01-15 | 1994-06-14 | Ford Motor Company | Method for manufacturing engine block having recessed cylinder bore liners |
US6463843B2 (en) * | 1999-06-11 | 2002-10-15 | Fredrick B. Pippert | Pump liner |
US6675699B1 (en) | 2000-09-25 | 2004-01-13 | Utex Industries, Inc. | Composite components for use in pumps |
WO2002068844A1 (en) * | 2001-02-21 | 2002-09-06 | Utex Industries, Inc. | Pump liner |
US6615901B2 (en) * | 2001-06-11 | 2003-09-09 | General Motors Corporation | Casting of engine blocks |
WO2003106842A1 (en) * | 2002-06-14 | 2003-12-24 | Jetstream Of Houston, Llp | High pressure reciprocating pump |
US20050249615A1 (en) * | 2002-06-14 | 2005-11-10 | Jetstream Of Houston, Llp | High pressure reciprocating pump |
US20060042770A1 (en) * | 2004-02-20 | 2006-03-02 | Newcomb Thomas P | Liner seat design for a foundry mold with integrated bore liner and barrel core features |
US7204293B2 (en) * | 2004-02-20 | 2007-04-17 | Gm Global Technology Operations, Inc. | Liner seat design for a foundry mold with integrated bore liner and barrel core features |
RU2382220C2 (ru) * | 2008-04-24 | 2010-02-20 | Федеральное государственное образовательное учреждение высшего профессионального образования "Чувашская государственная сельскохозяйственная академия" | Способ сборки цилиндропоршневой группы автотракторных двигателей |
US20150240741A1 (en) * | 2012-09-17 | 2015-08-27 | Federal-Mogul Burscheied GmbH | Cylinder sleeve with wear-resistant inner layer |
US10006399B2 (en) * | 2012-09-17 | 2018-06-26 | Federal-Mogul Burscheid Gmbh | Cylinder sleeve with wear-resistant inner layer |
US11480131B2 (en) | 2018-09-17 | 2022-10-25 | GM Global Technology Operations LLC | Engine block for an internal combustion engine |
Also Published As
Publication number | Publication date |
---|---|
FR2039974A5 (enrdf_load_stackoverflow) | 1971-01-15 |
DE1916168A1 (de) | 1970-10-08 |
GB1258705A (enrdf_load_stackoverflow) | 1971-12-30 |
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