EP3317508A1 - Kolben für eine brennkraftmaschine - Google Patents
Kolben für eine brennkraftmaschineInfo
- Publication number
- EP3317508A1 EP3317508A1 EP16740950.7A EP16740950A EP3317508A1 EP 3317508 A1 EP3317508 A1 EP 3317508A1 EP 16740950 A EP16740950 A EP 16740950A EP 3317508 A1 EP3317508 A1 EP 3317508A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- piston
- crown
- thermal barrier
- barrier coating
- 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.)
- Withdrawn
Links
- 238000002485 combustion reaction Methods 0.000 title claims abstract description 13
- 239000012720 thermal barrier coating Substances 0.000 claims description 33
- 239000010410 layer Substances 0.000 claims description 22
- 239000002318 adhesion promoter Substances 0.000 claims description 7
- 239000012790 adhesive layer Substances 0.000 claims description 2
- 239000000919 ceramic Substances 0.000 claims description 2
- 230000003247 decreasing effect Effects 0.000 claims description 2
- 229910001092 metal group alloy Inorganic materials 0.000 claims description 2
- RVTZCBVAJQQJTK-UHFFFAOYSA-N oxygen(2-);zirconium(4+) Chemical compound [O-2].[O-2].[Zr+4] RVTZCBVAJQQJTK-UHFFFAOYSA-N 0.000 claims description 2
- 229910001928 zirconium oxide Inorganic materials 0.000 claims description 2
- 238000009413 insulation Methods 0.000 abstract description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 6
- 229910052799 carbon Inorganic materials 0.000 description 6
- 230000015572 biosynthetic process Effects 0.000 description 2
- 230000002349 favourable effect Effects 0.000 description 2
- 239000000758 substrate Substances 0.000 description 2
- 230000008646 thermal stress Effects 0.000 description 2
- 229910001233 yttria-stabilized zirconia Inorganic materials 0.000 description 2
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- 239000007767 bonding agent Substances 0.000 description 1
- 238000004939 coking Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 229910002076 stabilized zirconia Inorganic materials 0.000 description 1
- 230000035882 stress Effects 0.000 description 1
- 238000005382 thermal cycling Methods 0.000 description 1
- 238000005050 thermomechanical fatigue Methods 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
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
- F02F3/00—Pistons
- F02F3/10—Pistons having surface coverings
- F02F3/12—Pistons having surface coverings on piston heads
-
- 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
- F02F3/00—Pistons
- F02F3/02—Pistons having means for accommodating or controlling heat expansion
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2251/00—Material properties
- F05C2251/04—Thermal properties
- F05C2251/048—Heat transfer
Definitions
- the invention relates to a piston for an internal combustion engine with the features of the preamble of claim 1, as well as an internal combustion engine.
- the object of the invention is to reduce carbon deposits.
- the cover layer is arranged on the adhesion promoter layer and the adhesion promoter layer is arranged on the crown edge. It has proven to be particularly advantageous to build the thermal barrier coating in two layers.
- the bonding agent layer is preferably matched in terms of their thermal expansion coefficient between the substrate, so the piston, and the cover layer, so as to keep thermal stresses as low as possible.
- the thermal barrier coating extends on the piston crown near the crown edge in the direction of a center of the piston crown.
- the Thermal insulation layer thus preferably forms a circumferential ring on the piston crown, which extends in the direction of the center of the piston.
- the thermal barrier coating extends on the piston crown near the crown edge in the direction of a radial position spaced from the center of the piston crown, preferably to a radial position of about 80% of the distance between the crown edge and the center of the piston crown, measured from the Middle of the piston crown.
- the heat-insulating layer preferably covers a seam of the piston crown with a width of about 20% based on the radial dimension of the thermal barrier coating in the direction of the center of the piston crown.
- the thermal barrier coating has a decreasing thickness in the direction of the center of the piston crown. Due to this gradual course of the thermal barrier coating, a particularly favorable adhesion to the substrate is given and thermal stresses are reduced.
- a land area or a piston skirt of the piston is free of the thermal barrier coating. It is usually provided that a plurality of grooves is arranged in a land area of the piston near the piston crown.
- the cover layer of the thermal barrier coating consists of a ceramic, preferably of yttrium-stabilized zirconium oxide, and preferably has a dense-vertically-cracked structure.
- yttrium-stabilized zirconia yttria stabilized zirconia (YSZ)
- YSZ yttria stabilized zirconia
- thermal barrier coatings with DVC structure are superior to conventional layered structures in terms of thermal cycling.
- the adhesive layer of the thermal barrier coating consists of a metal alloy. Protection is also desired for an internal combustion engine, preferably a stationary internal combustion engine. Advantages of the invention are in particular:
- the invention allows the use of narrower flames, which is advantageous in terms of hydrocarbon emissions.
- the invention differs quite fundamentally from known from the prior art measures against carbon deposits. Instead of reducing coking by anti-adhesion layers on the surface, the invention reduces the temperature in the region of the upper land and the upper annular groove and thus prevents the formation of carbon deposits at all.
- FIG. 2 is a thermal barrier coating in one embodiment.
- Figure 1 shows a schematic representation of a piston 1 in cross-section for orientation and naming of the components.
- the piston 1 has a piston crown 2 and a crown edge 3.
- the piston skirt 9, fire bars 1 1 are formed. These are those areas between which the annular grooves 10 are located for receiving piston rings.
- a thermal barrier coating 4 extends starting near the outer periphery of the piston 1, ie near the crown edge 3 in the direction of the center 7 of the piston first
- the thermal barrier coating 4 has an adhesion promoter layer 6 and a cover layer 5.
- the thickness of the thermal barrier coating 4 is indicated by the reference numeral d.
- the thermal barrier coating 4 extends as a circumferential ring or hem on the piston crown 2 to near an edge 8.
- the thickness d of the thermal barrier coating 4 is reduced in a region of the edge 8, resulting in a favorable gradual transition to the uncoated region of the piston crown. 2 results.
- the radial distance r from the center 7 of the piston 1 is introduced to describe a radial extent of the thermal barrier coating 4.
- Figure 2 shows a piston 1 with a thermal barrier coating 4 in an embodiment of the invention.
- the thermal barrier coating 4 is not pulled to the crown edge 3, but runs immediately before this. The layer is therefore only close to the crown edge 3 zoom.
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ATA429/2015A AT517589B1 (de) | 2015-07-03 | 2015-07-03 | Kolben für eine Brennkraftmaschine |
PCT/AT2016/050239 WO2017004645A1 (de) | 2015-07-03 | 2016-06-30 | Kolben für eine brennkraftmaschine |
Publications (1)
Publication Number | Publication Date |
---|---|
EP3317508A1 true EP3317508A1 (de) | 2018-05-09 |
Family
ID=56463980
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP16740950.7A Withdrawn EP3317508A1 (de) | 2015-07-03 | 2016-06-30 | Kolben für eine brennkraftmaschine |
Country Status (5)
Country | Link |
---|---|
US (1) | US10634090B2 (de) |
EP (1) | EP3317508A1 (de) |
AT (1) | AT517589B1 (de) |
CA (1) | CA2990953A1 (de) |
WO (1) | WO2017004645A1 (de) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3440230B1 (de) * | 2016-04-08 | 2020-01-08 | Volvo Truck Corporation | Kolben für einen zylinder für einen verbrennungsmotor |
DE102019203650A1 (de) * | 2019-03-18 | 2020-09-24 | Mahle Lnternational Gmbh | Kolben für eine Brennkraftmaschine |
US11719184B1 (en) | 2022-01-21 | 2023-08-08 | Tenneco Inc. | Piston with engineered crown coating and method of manufacturing |
Family Cites Families (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3189010A (en) | 1963-11-21 | 1965-06-15 | Continental Aviat & Eng Corp | Piston for internal combustion engine |
US3976809A (en) * | 1973-08-13 | 1976-08-24 | Dowell Robert D | Coating for metal surfaces and method for application |
JPS6036551B2 (ja) * | 1980-09-09 | 1985-08-21 | 宇部興産株式会社 | セメント原料等粉末原料の仮焼炉 |
DE3137731A1 (de) | 1981-09-23 | 1983-04-14 | Battelle-Institut E.V., 6000 Frankfurt | Hochtemperatur- und thermoschockbestaendige kompaktwerkstoffe und beschichtungen |
JPS6036551U (ja) * | 1983-08-18 | 1985-03-13 | 富士重工業株式会社 | ピストン |
DE3330554A1 (de) * | 1983-08-24 | 1985-03-07 | Kolbenschmidt AG, 7107 Neckarsulm | Kolben fuer brennkraftmaschinen |
JPS60119348A (ja) * | 1983-11-30 | 1985-06-26 | Izumi Jidosha Kogyo Kk | 内燃機関用ピストンおよびその製造方法 |
JPS60240856A (ja) * | 1984-05-12 | 1985-11-29 | Honda Motor Co Ltd | エンジン用断熱ピストン |
JPS6158915A (ja) * | 1984-08-29 | 1986-03-26 | Nissan Motor Co Ltd | 内燃機関の燃焼室壁面構造 |
JPS6261770A (ja) * | 1985-09-09 | 1987-03-18 | Toyota Motor Corp | 長繊維の断熱層を有する金属部材及びその製造方法 |
US5477820A (en) * | 1994-09-29 | 1995-12-26 | Ford Motor Company | Thermal management system for heat engine components |
US20030084858A1 (en) | 1998-02-20 | 2003-05-08 | Kracklauer John J. | Method for providing and maintaining catalytically active surface in internal combustion engine |
DE10029810A1 (de) * | 2000-06-16 | 2001-12-20 | Mahle Gmbh | Kolben für Dieselmotoren |
DE10242261A1 (de) * | 2002-09-12 | 2004-03-25 | Daimlerchrysler Ag | Kolbenmuldenrandverstärkung |
US6803135B2 (en) | 2003-02-24 | 2004-10-12 | Chromalloy Gas Turbine Corporation | Thermal barrier coating having low thermal conductivity |
KR20060111665A (ko) | 2004-01-07 | 2006-10-27 | 가부시키가이샤 고마쓰 세이사쿠쇼 | 내연기관용 피스톤 |
DE102005006670A1 (de) | 2005-02-15 | 2006-08-17 | Ks Kolbenschmidt Gmbh | Antiadhäsive Beschichtung von Bauteilen zur Verhinderung von Ölkohleanbackungen |
US8272843B1 (en) | 2005-09-12 | 2012-09-25 | Florida Turbine Technologies, Inc. | TBC with fibrous reinforcement |
EP2096290B1 (de) | 2008-02-29 | 2014-06-18 | Caterpillar Motoren GmbH & Co. KG | Kolben für Brennkraftmaschinen mit einem Kühlraum mit Antihaftbeschichtung |
JP2010071134A (ja) * | 2008-09-17 | 2010-04-02 | Nissan Motor Co Ltd | エンジンの燃料噴射時期制御装置 |
JP5117986B2 (ja) | 2008-10-08 | 2013-01-16 | アート金属工業株式会社 | 内燃機関用ピストンスカート部の表面処理方法及び内燃機関用ピストン |
JP5248379B2 (ja) | 2009-03-17 | 2013-07-31 | 日立オートモティブシステムズ株式会社 | 複層被膜組成物が施された内燃機関のピストン及び該ピストンの表面処理方法 |
JP5642157B2 (ja) | 2010-03-19 | 2014-12-17 | 本田技研工業株式会社 | 内燃機関用ピストン |
US8813357B2 (en) | 2010-10-06 | 2014-08-26 | GM Global Technology Operations LLC | Piston with bi-metallic dome |
US20130025561A1 (en) | 2011-07-28 | 2013-01-31 | Dieter Gabriel | Bowl rim and root protection for aluminum pistons |
JP2013087721A (ja) * | 2011-10-20 | 2013-05-13 | Isuzu Motors Ltd | 遮熱膜の形成方法及び内燃機関 |
KR101372565B1 (ko) * | 2012-07-02 | 2014-03-13 | 자동차부품연구원 | 내연기관 및 그 제조방법 |
JP5998696B2 (ja) * | 2012-07-19 | 2016-09-28 | マツダ株式会社 | エンジン燃焼室の断熱構造 |
JP2014105619A (ja) * | 2012-11-27 | 2014-06-09 | Toyota Motor Corp | ピストン |
WO2015076317A1 (ja) * | 2013-11-19 | 2015-05-28 | 日本碍子株式会社 | 断熱膜、および断熱膜構造 |
-
2015
- 2015-07-03 AT ATA429/2015A patent/AT517589B1/de not_active IP Right Cessation
-
2016
- 2016-06-30 CA CA2990953A patent/CA2990953A1/en not_active Abandoned
- 2016-06-30 EP EP16740950.7A patent/EP3317508A1/de not_active Withdrawn
- 2016-06-30 US US15/738,642 patent/US10634090B2/en active Active
- 2016-06-30 WO PCT/AT2016/050239 patent/WO2017004645A1/de active Application Filing
Also Published As
Publication number | Publication date |
---|---|
US20190093596A1 (en) | 2019-03-28 |
CA2990953A1 (en) | 2017-01-12 |
AT517589B1 (de) | 2017-03-15 |
WO2017004645A1 (de) | 2017-01-12 |
US10634090B2 (en) | 2020-04-28 |
AT517589A4 (de) | 2017-03-15 |
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Legal Events
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Effective date: 20180205 |
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AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
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AX | Request for extension of the european patent |
Extension state: BA ME |
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DAV | Request for validation of the european patent (deleted) | ||
DAX | Request for extension of the european patent (deleted) | ||
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: INNIO JENBACHER GMBH & CO OG |
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STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: EXAMINATION IS IN PROGRESS |
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Effective date: 20200717 |
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Effective date: 20201128 |