JPS6093161A - Heat-insulated piston structure - Google Patents
Heat-insulated piston structureInfo
- Publication number
- JPS6093161A JPS6093161A JP20046683A JP20046683A JPS6093161A JP S6093161 A JPS6093161 A JP S6093161A JP 20046683 A JP20046683 A JP 20046683A JP 20046683 A JP20046683 A JP 20046683A JP S6093161 A JPS6093161 A JP S6093161A
- Authority
- JP
- Japan
- Prior art keywords
- piston body
- crown
- projection
- receiving hole
- piston
- 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
Links
- 239000000919 ceramic Substances 0.000 abstract description 12
- 229910052782 aluminium Inorganic materials 0.000 abstract description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 abstract description 6
- 238000002485 combustion reaction Methods 0.000 abstract description 6
- 238000010438 heat treatment Methods 0.000 abstract description 3
- 230000002093 peripheral effect Effects 0.000 abstract description 3
- 229910052581 Si3N4 Inorganic materials 0.000 abstract description 2
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 abstract description 2
- 229910001018 Cast iron Inorganic materials 0.000 abstract 1
- 230000008878 coupling Effects 0.000 abstract 1
- 238000010168 coupling process Methods 0.000 abstract 1
- 238000005859 coupling reaction Methods 0.000 abstract 1
- 239000011810 insulating material Substances 0.000 description 3
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000005266 casting Methods 0.000 description 2
- 239000000835 fiber Substances 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 239000010935 stainless steel Substances 0.000 description 2
- 229910001220 stainless steel Inorganic materials 0.000 description 2
- 230000035882 stress Effects 0.000 description 2
- 229910000851 Alloy steel Inorganic materials 0.000 description 1
- 235000017399 Caesalpinia tinctoria Nutrition 0.000 description 1
- 229910000531 Co alloy Inorganic materials 0.000 description 1
- 241000388430 Tara Species 0.000 description 1
- 230000032683 aging Effects 0.000 description 1
- 238000012271 agricultural production Methods 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000009940 knitting Methods 0.000 description 1
- 229910000833 kovar Inorganic materials 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 210000004279 orbit Anatomy 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000008646 thermal stress 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
- F02F3/0015—Multi-part pistons
-
- 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
- F02F2200/00—Manufacturing
- F02F2200/04—Forging of engine parts
-
- 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
- F05C2201/00—Metals
- F05C2201/02—Light metals
- F05C2201/021—Aluminium
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Abstract
Description
【発明の詳細な説明】
本発明は断熱エンジンに供される断熱ピストンの構造に
関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to the structure of an adiabatic piston used in an adiabatic engine.
エンジンの燃焼室を囲む壁部にセラミクスを用いること
によって燃焼ガスの外部放散を防ぎ、高温の状態で排気
ガスを排気ターボ過給機などの前回II?装置へ送り出
し、これによって機関の出力増大と熱効率の向上を図る
ようにした断熱エンジンが既に提案されている。By using ceramics in the wall surrounding the combustion chamber of the engine, the combustion gas is prevented from dissipating to the outside, and the exhaust gas is exhausted under high temperature conditions. An adiabatic engine has already been proposed in which the engine is fed to a device, thereby increasing the output and improving the thermal efficiency of the engine.
断熱エンジンのピストンは、アルミニウムなどのピスト
ン本体とセラミクスからなるクラウンとを耐熱性を有す
るボルトなどで締結するかまたは詩ぐるみ法によって結
合するのが一般的である。In the piston of an adiabatic engine, a piston body made of aluminum or the like and a crown made of ceramic are generally fastened together using heat-resistant bolts or the like, or by the cylindrical method.
しかし、ポルl〜による締結では熟サイクルや燃焼圧の
変動によって弛みが発生し、また鋳くるんだものでは熱
応力により破壊される恐れがあり、まだ実用の城に達し
ていない。However, when fastening with POL~, loosening occurs due to aging cycles and fluctuations in combustion pressure, and cast-wrapped ones may break due to thermal stress, so they have not yet reached a level of practical use.
また、特開昭57−2445号公報に示すように、ピス
トンについて燃焼室を区画するクラウンにセラミクスを
用いたものが提案されているが、これはアルミニウムな
どからなるピストン本体との結合構造が複雑であり、ぞ
の帽イ」けに手数と時間がlトる。Furthermore, as shown in Japanese Patent Application Laid-Open No. 57-2445, a piston using ceramics for the crown that partitions the combustion chamber has been proposed, but this requires a complicated connection structure with the piston body made of aluminum or the like. However, it takes a lot of effort and time to do so.
本発明の目的は、構成および組(4けが簡単でi産に適
した断熱ピストンの構造を提供することにある。An object of the present invention is to provide a structure of an insulating piston that is simple in construction and assembly and suitable for industrial use.
このため、本発明の構成はピストン本体の上端部に嵌合
穴を設け、該嵌合穴にクラウンに形成した突部を嵌合し
、前記ピストン本体の嵌合穴周囲を加熱加圧し、ピスト
ン本体とクラウンとを接合したものである。For this reason, the configuration of the present invention is such that a fitting hole is provided at the upper end of the piston body, a protrusion formed on the crown is fitted into the fitting hole, and the area around the fitting hole of the piston body is heated and pressurized. The main body and the crown are joined together.
本発明を実施例に基づいて説明する。第1図に示づJ、
うに、本発明にJ:るピストン目スノJ−1〜部を含む
ピストン本体2と、この、1一端部に結合される窒化珪
素などのセラミクスからなるクラウン1とを勾いに結合
して構成される。ピストン本体2はアルミニウムま/、
:I;1 i4鍛u鉄によって構成され、この外周面に
リンク満10.11.12が削設される。そして、上端
部に嵌合穴15が設けられるとともに、周壁には公知の
ピストンピンを嵌合するピン穴13が股1らl’lる。The present invention will be explained based on examples. J shown in Figure 1,
According to the present invention, a piston main body 2 including a piston eye socket J-1 and a crown 1 made of ceramics such as silicon nitride connected to one end of the piston main body 2 are joined in an inclined manner. be done. The piston body 2 is made of aluminum.
:I;1 It is constructed of I4 forged U iron, and links 10, 11, and 12 are cut into the outer peripheral surface. A fitting hole 15 is provided at the upper end, and a pin hole 13 into which a known piston pin is fitted is provided from the crotch 1 in the peripheral wall.
クラウン1σ月一端而11平坦であり、下端部の周縁部
にビスト2本142の1−縁部にリング4を介して重合
される突条19 /J”8’U Ltられるとともに、
中央部に燃焼室9をト画【、1、かつ下方l\突出4る
突部5が一体に形成される。そして、この突部5がビス
(−ン本体2の嵌合穴1!:iにhy+自されるととも
に、突条19と突部5との間の空部にセラミクスファイ
バまたはステン1ノスメッシ]からなる断熱材3が挾ま
れる。The crown 1σ is flat at one end and 11 is flat, and a protrusion 19 is attached to the periphery of the lower end of the two screws 142 and is overlapped with the edge of the ring 4 through the ring 4.
A protrusion 5 that defines a combustion chamber 9 and projects downward is integrally formed in the center. Then, this protrusion 5 is screwed into the fitting hole 1 of the main body 2, and a ceramic fiber or stainless steel mesh is inserted into the space between the protrusion 19 and the protrusion 5. The heat insulating material 3 is sandwiched.
リング4はピストン本体2の、E端部に形成()た環状
溝に係合される。断熱材3と1ノではセラミクスファイ
バまたはステンレス細線を編成するか、または絡み合せ
て形成したものを用いる。The ring 4 is engaged with an annular groove formed at the E end of the piston body 2. The heat insulating materials 3 and 1 are formed by knitting or intertwining ceramic fibers or stainless steel wires.
本発明では特に突部5の外周面の而粗ざを予め粗く成形
しておき、これをビス1ヘン本体2の嵌合穴15に嵌合
したうえ、第2図に示すように、ピストン本体2の内端
壁2aの突部5に接近する部分をダイス6をもって加熱
加圧し、これによって突部5との嵌合部を緊密に圧接さ
せる。このダイス6は圧縮荷重に耐える好ましくはセラ
ミクスから形成されるカップ状のもので、予め適当な手
段により加熱したうえ、下端部6aをピストン本体2の
内@’I!2aに強く押付けて、ピストン本体2の上段
部の壁部を変形させ、嵌合穴15に対する突部5の嵌合
部を密接させる。ダイス6は加熱が終っても加圧状態を
維持しつつ冷却し、事後の熱膨張による弛みの発生を防
止する。In the present invention, in particular, the outer circumferential surface of the protrusion 5 is formed in advance to have a rough surface, and this is fitted into the fitting hole 15 of the screw body 2, and as shown in FIG. The portion of the inner end wall 2a of the inner end wall 2a approaching the protrusion 5 is heated and pressurized using a die 6, thereby bringing the fitting portion with the protrusion 5 into tight pressure contact. The die 6 is a cup-shaped die preferably made of ceramics that can withstand compressive loads, and is heated in advance by an appropriate means, and then the lower end 6a is inserted into the piston body 2. 2a to deform the upper wall of the piston body 2 and bring the fitting portion of the protrusion 5 into the fitting hole 15 into close contact. Even after heating, the die 6 is cooled while maintaining the pressurized state to prevent loosening due to subsequent thermal expansion.
ダイス6はカップ状とする代りに、この端部6aに円周
方向に沿って複数個の突部を設け、これによって嵌合穴
15と突部5との嵌合部を局部的に加熱変形させるよう
にしてもよい。Instead of having a cup shape, the die 6 is provided with a plurality of protrusions along the circumferential direction on the end portion 6a, whereby the fitting portion between the fitting hole 15 and the protrusion 5 is locally heated and deformed. You may also do so.
クラウン1をピストン本体2に結合ケる場合。When connecting the crown 1 to the piston body 2.
予めピストン本体2を高周波加熱手段などにより金属の
軟化点、炭県#MCは400へ一500°C1合金鋼で
は600℃、アルミニウムでは300℃程度に加熱し、
イの後にダイス6によ′つて加圧する。The piston body 2 is heated in advance by high frequency heating means or the like to the softening point of the metal, MC = 400-500°C, 600°C for 1 alloy steel, and 300°C for aluminum.
After step A, pressure is applied using die 6.
このようにしてピストン本体2の軟化した部分がセラミ
クスからなるクラウン1の突部5に圧着され、かつ加圧
状態で冷fJlさhるために、圧検出ノコが残留し、突
Ni5との結合力が強化される。In this way, the softened portion of the piston body 2 is crimped to the protrusion 5 of the crown 1 made of ceramics, and since it is cooled under pressure, the pressure detection saw remains and the connection with the protrusion Ni5 Power is strengthened.
第3図に承りように、ビス1ヘン本体2とクラウン1の
突部5との嵌合部に(、L、セラミクスと同等の熱膨張
率を有するコバール(F e−N 1−Co合金)など
の合金からなるリング1Bを突部5に外挿1ノ、かつ内
端!12aを加熱しながら強く押付けて、内端壁2aの
内部へ埋入きせるようにすれば、さらに緊密な結合が得
られる。As shown in Fig. 3, the fitting part between the screw body 2 and the protrusion 5 of the crown 1 is made of Kovar (F e-N 1-Co alloy) which has the same coefficient of thermal expansion as ceramics. An even tighter connection can be achieved by inserting a ring 1B made of an alloy such as can get.
なお、燃料が燃焼室9の壁部に向って直接噴射される形
式のティービルエンジンでは、燃料が当る部分のピスト
ンピン
うに、第4図に示づ゛ように、嵌合穴15に溝225−
を設けて、突部5との間に空部を形成することが好まし
い。In addition, in a T-bill engine in which fuel is injected directly toward the wall of the combustion chamber 9, a groove 225 is formed in the fitting hole 15 on the piston pin in the part that is in contact with the fuel, as shown in FIG. - It is preferable to provide a space between the protrusion 5 and the protrusion 5.
本発明は上述のように、従来のボルトや鋳ぐるみによる
手段と異なり、セラミクスからなるクラウン1がアルミ
ニウムなどからなるピストン本体2に嵌合され、かつこ
の嵌合部が機械的に圧接されるものであるから、クラウ
ン1とピストン本体2とのボルトの締め過ぎにより過大
な締付応力が生じたり、鋳ぐるみ時に高温溶融時の内部
応力が生じるなどの従来の不具合を解消することができ
るとともに、構造および組立が簡単であるので農産化が
容易であり、断熱ピストンを安価に提供することができ
る。As mentioned above, the present invention differs from the conventional means using bolts or castings, in that the crown 1 made of ceramics is fitted into the piston body 2 made of aluminum or the like, and this fitting part is mechanically pressure-welded. Therefore, it is possible to eliminate conventional problems such as excessive tightening stress caused by over-tightening the bolt between the crown 1 and the piston body 2, and internal stress caused by high temperature melting during casting. Since the structure and assembly are simple, agricultural production is easy, and the heat insulating piston can be provided at low cost.
第1図は本発明に係る断熱ピストンの構造についての正
面断面図、第2図および第3図は同断熱ピストンの製造
過程を示す正面断面図、第4図は本発明の一部変更実施
例に係る断熱ピストンの構造についての平面断面図であ
る。
6−
1:タラS7ン 2:ピストン本体 3:断熱材5:突
部 15:嵌合穴
特許出願人 い′1讐自動車株式会社
代叩人 弁理1111本俊夫
7一Fig. 1 is a front sectional view of the structure of the heat insulating piston according to the present invention, Figs. 2 and 3 are front sectional views showing the manufacturing process of the heat insulating piston, and Fig. 4 is a partially modified embodiment of the present invention. FIG. 3 is a plan sectional view of the structure of the heat insulating piston according to the invention. 6- 1: Tara S7n 2: Piston body 3: Insulating material 5: Protrusion 15: Fitting hole Patent applicant I'1 Toshio Jidosha Co., Ltd. Patent attorney 1111 Toshio Moto 71
Claims (1)
ウンに形成した突部を嵌合し、前記ビス]〜ン本体の嵌
合穴周囲を加熱加圧し、ビス;−ン本体とクラウンとを
接合したことを特徴とする断熱ビスi〜ンの構造A fitting hole is provided at the upper end of the piston body, a protrusion formed on the crown is fitted into the fitting hole, and the area around the fitting hole of the screw body is heated and pressurized to connect it to the screw body. The structure of a heat insulating screw characterized by joining the crown.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP20046683A JPS6093161A (en) | 1983-10-26 | 1983-10-26 | Heat-insulated piston structure |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP20046683A JPS6093161A (en) | 1983-10-26 | 1983-10-26 | Heat-insulated piston structure |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS6093161A true JPS6093161A (en) | 1985-05-24 |
JPH0372830B2 JPH0372830B2 (en) | 1991-11-19 |
Family
ID=16424779
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP20046683A Granted JPS6093161A (en) | 1983-10-26 | 1983-10-26 | Heat-insulated piston structure |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6093161A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0155160A2 (en) * | 1984-03-12 | 1985-09-18 | Ngk Insulators, Ltd. | An internal combustion engine piston and a method of producing the same |
JPS61164449U (en) * | 1985-04-01 | 1986-10-13 | ||
JPS61275547A (en) * | 1985-05-30 | 1986-12-05 | Kyocera Corp | Direct injection diesel engine piston |
JPS63255551A (en) * | 1987-04-11 | 1988-10-21 | Isuzu Motors Ltd | Heat insulated piston |
JPS63255553A (en) * | 1987-04-11 | 1988-10-21 | Isuzu Motors Ltd | Heat insulated piston |
DE102004028459A1 (en) * | 2004-06-11 | 2005-12-29 | Mahle Gmbh | Built piston for internal combustion engine consists of upper part with bearing edge, recess and nose part on bottom and under part shaped to form a shrink fit with upper part thereby joining them together |
JP2008267205A (en) * | 2007-04-18 | 2008-11-06 | Nishishiba Electric Co Ltd | Piston and oilless compressor |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5575977A (en) * | 1978-11-29 | 1980-06-07 | Rosenthal Technik Ag | Bonding body between ceramic member and metal member |
JPS59179261U (en) * | 1983-05-19 | 1984-11-30 | 日本特殊陶業株式会社 | Piston for internal combustion engine |
-
1983
- 1983-10-26 JP JP20046683A patent/JPS6093161A/en active Granted
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5575977A (en) * | 1978-11-29 | 1980-06-07 | Rosenthal Technik Ag | Bonding body between ceramic member and metal member |
JPS59179261U (en) * | 1983-05-19 | 1984-11-30 | 日本特殊陶業株式会社 | Piston for internal combustion engine |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0155160A2 (en) * | 1984-03-12 | 1985-09-18 | Ngk Insulators, Ltd. | An internal combustion engine piston and a method of producing the same |
JPS61164449U (en) * | 1985-04-01 | 1986-10-13 | ||
JPS61275547A (en) * | 1985-05-30 | 1986-12-05 | Kyocera Corp | Direct injection diesel engine piston |
JPS63255551A (en) * | 1987-04-11 | 1988-10-21 | Isuzu Motors Ltd | Heat insulated piston |
JPS63255553A (en) * | 1987-04-11 | 1988-10-21 | Isuzu Motors Ltd | Heat insulated piston |
JPH0745851B2 (en) * | 1987-04-11 | 1995-05-17 | いすゞ自動車株式会社 | Structure of adiabatic piston |
DE102004028459A1 (en) * | 2004-06-11 | 2005-12-29 | Mahle Gmbh | Built piston for internal combustion engine consists of upper part with bearing edge, recess and nose part on bottom and under part shaped to form a shrink fit with upper part thereby joining them together |
JP2008267205A (en) * | 2007-04-18 | 2008-11-06 | Nishishiba Electric Co Ltd | Piston and oilless compressor |
Also Published As
Publication number | Publication date |
---|---|
JPH0372830B2 (en) | 1991-11-19 |
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