JPH0730909Y2 - Piston combustion chamber - Google Patents

Piston combustion chamber

Info

Publication number
JPH0730909Y2
JPH0730909Y2 JP1040688U JP1040688U JPH0730909Y2 JP H0730909 Y2 JPH0730909 Y2 JP H0730909Y2 JP 1040688 U JP1040688 U JP 1040688U JP 1040688 U JP1040688 U JP 1040688U JP H0730909 Y2 JPH0730909 Y2 JP H0730909Y2
Authority
JP
Japan
Prior art keywords
piston
combustion chamber
axis
injector
spray
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
Application number
JP1040688U
Other languages
Japanese (ja)
Other versions
JPH01114921U (en
Inventor
英治 溝手
直哉 酒井
洋 中川
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP1040688U priority Critical patent/JPH0730909Y2/en
Publication of JPH01114921U publication Critical patent/JPH01114921U/ja
Application granted granted Critical
Publication of JPH0730909Y2 publication Critical patent/JPH0730909Y2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Description

【考案の詳細な説明】 (産業上の利用分野) 本考案は内燃機関、特に直接噴射式のディーゼル機関の
ピストンの燃焼室に関するものである。
DETAILED DESCRIPTION OF THE INVENTION (Industrial field of application) The present invention relates to a combustion chamber of a piston of an internal combustion engine, particularly a direct injection diesel engine.

(従来の技術) 従来から、機関の内部で燃料を燃焼させて空気を直接加
熱し、その膨張によってピストンを往復動させ、仕事を
行う内燃機関が知られており、大型車等においては、高
圧縮比で熱効率の良いディーゼル機関が良く用いられて
いる。このディーゼル機関のピストン並びにその近傍部
は第5図に示される如く構成されている。同図におい
て、シリンダライナ5により形成されるシリンダ空間内
にはピストン1が配置されており、該ピストン1はシリ
ンダ空間内を摺動自在である。このピストン1の上部に
は燃焼室(キャビティーとも言う)2が形成されてお
り、該燃焼室は略円柱状空洞部をなしている。この燃焼
室2及びシリンダライナ5の上部にはシリンダヘッド4
が搭載されており、該シリンダヘッド4にはインジェク
タ3が設けられている。そして、ピストン1を上方に摺
動させて吸入空気を圧縮高熱化し、その時に上記インジ
ェクタ3から燃焼室2に向かって軽油(燃料)を噴射さ
せて自然発火するようになっている。
(Prior Art) Conventionally, there is known an internal combustion engine that burns fuel inside an engine to directly heat air and reciprocally moves a piston by its expansion to perform work. Diesel engines with good compression ratio and good thermal efficiency are often used. The piston of this diesel engine and its vicinity are constructed as shown in FIG. In the figure, a piston 1 is arranged in a cylinder space formed by a cylinder liner 5, and the piston 1 is slidable in the cylinder space. A combustion chamber (also referred to as a cavity) 2 is formed in the upper portion of the piston 1, and the combustion chamber forms a substantially cylindrical hollow portion. A cylinder head 4 is provided above the combustion chamber 2 and the cylinder liner 5.
Is mounted, and the cylinder head 4 is provided with an injector 3. Then, the piston 1 is slid upward to compress and heat the intake air high, and at that time, light oil (fuel) is injected from the injector 3 toward the combustion chamber 2 to spontaneously ignite.

(考案が解決しようとする問題点) ところで、上記インジェクタ3の中には、例えばピスト
ン1とシリンダヘッド4との間に形成される渦流(スワ
ールとも称す)が極端に強い場合等においては、その対
応策として、第5図に示されるように、インジェクタ3
をピストン1の軸心に対して傾斜させることがある。し
かし、このように構成すると、第5図に示されるよう
に、インジェクタ3の軸心3aと、インジェクタ3の噴口
6A,6B…6Xのそれぞれの軸心6a,6b…6xとのなす角θa,θ
b…θxが大きくなる程その噴霧量が減少することにな
る。すなわち第5図において説明すれば、θd>θaな
る大小関係となっているので、軸心6d側の噴霧の方が軸
心6a側の噴霧に比べてその噴霧量は少なくなる。ここで
未知数Xは噴口の数を表している。ところが上述のよう
に、噴口毎の噴霧量が異なるにも拘らず、噴霧が当接す
る燃焼室の形状を一定な略円柱状空洞部としたままで
は、それぞれの噴霧火炎の形成が異なるようになってし
まい、その結果、混合、燃焼が充分に行われずに、性能
が狙い道り向上しない等の問題点を生じていた。特にイ
ンジェクタ3を傾斜して配置する上記場合においては、
インジェクタ3の先端部がピストン1の軸心(燃焼室2
の軸心)上にない場合が多いので、その傾向はさらに助
長される。
(Problems to be Solved by the Invention) By the way, in the injector 3, for example, when a vortex (also called swirl) formed between the piston 1 and the cylinder head 4 is extremely strong, As a countermeasure, as shown in FIG. 5, the injector 3
May be inclined with respect to the axis of the piston 1. However, with this configuration, as shown in FIG. 5, the axis 3a of the injector 3 and the injection port of the injector 3
Angles 6a, 6B ... 6X formed by the respective axes 6a, 6b ... 6x
The larger the b ... θx, the smaller the spray amount. That is, in the explanation with reference to FIG. 5, since there is a magnitude relation of θd> θa, the spray amount on the shaft center 6d side is smaller than that on the shaft center 6a side. Here, the unknown number X represents the number of nozzles. However, as described above, despite that the spray amount is different for each injection port, if the shape of the combustion chamber with which the spray is in contact is a substantially cylindrical hollow portion, the formation of each spray flame will be different. As a result, there has been a problem that the mixing and combustion are not sufficiently performed, and the performance is not improved on the target. Particularly in the above case in which the injector 3 is inclined,
The tip of the injector 3 is the axial center of the piston 1 (the combustion chamber 2
Often, it is not on the axis, and this tendency is further promoted.

本考案の目的は各噴口の噴射量の差に拘らず一様の噴霧
火炎をそれぞれ形成、燃焼効率を向上させ、性能の改善
を図るピストンの燃焼室を提供することにある。
It is an object of the present invention to provide a combustion chamber of a piston that forms uniform spray flames regardless of the difference in injection amount of each injection port, improves combustion efficiency, and improves performance.

この考案の前記並びにその他の目的と新規な特徴につい
ては、本明細書の記述及び添付図面から明らかになるで
あろう。
The above and other objects and novel features of the present invention will be apparent from the description of this specification and the accompanying drawings.

(問題点を解決するための手段) 本考案のピストンの燃焼室は上記目的を達成するため
に、ピストンの軸心を軸心として、その噴口の数分、均
等分割した仮想分割面の方向の空洞部の壁面を、その方
向面上に前記ピストンの軸心と方向が一致する軸心を有
し、底面に行くに従って大となる円弧状に切欠き、該切
欠き部を噴霧方向に略一致対向させ、インジェクタの軸
心と噴口の軸心とのなす角が大きくなる程、その噴口に
対応する切欠き部の容量を小さくするよう構成したこと
を特徴としている。
(Means for Solving Problems) In order to achieve the above-mentioned object, the combustion chamber of the piston of the present invention has the axial center of the piston as the axis, and the number of the nozzles is equal to the direction of the virtual divided surface. The wall surface of the cavity has an axial center whose direction coincides with the axial center of the piston on the direction surface, and is cut out in an arc shape which becomes larger toward the bottom surface, and the cutout portion substantially coincides with the spray direction. It is characterized in that the capacity of the notch corresponding to the nozzle is made smaller as the angle formed by the axis of the injector and the axis of the nozzle becomes larger.

(作用) 本考案によれば、噴霧方向の燃焼室の内壁が切欠かれる
が、その切欠き部の容量、インジェクタの軸心と噴口の
軸心とのなす角が大きくなる程小さくされ、各噴口の噴
霧量を差に拘らず一様な噴霧火炎がそれぞれ形成される
ようになる。
(Effect) According to the present invention, the inner wall of the combustion chamber in the spray direction is notched, but it is made smaller as the volume of the notch and the angle between the axis of the injector and the axis of the nozzle are increased. A uniform spray flame is formed regardless of the difference in the spray amount.

(実施例) 以下本考案の実施例を図面を参照しながら説明する。第
1図は本考案の一実施例を示すピストンの上面図、第2
図は第1図の側断面図である。
Embodiment An embodiment of the present invention will be described below with reference to the drawings. FIG. 1 is a top view of a piston showing an embodiment of the present invention, and FIG.
The figure is a sectional side view of FIG.

この実施例のピストンの燃焼室が従来技術のそれと違う
点は、第1図、第2図に示される如く、噴霧方向の燃焼
室12の内壁を切欠き、その切欠き部12a,12b,12c,12dの
容量を、インジェクタ3の軸心3aと噴口6A,6B,6C,6Dの
軸心6a,6b,6c,6dとのなす角θa,θb,θc,θdが大きく
なる程小さくしている点である。ここで、θa,θb,θc,
θdの大小関係はθa<θb<θc<θdとなってい
る。また、噴口6B,6Cは図面上に表されていないが、噴
口6Bは噴口6Aの90°の時計回りの方向に、一方噴口6Cは
噴口6Dの90°時計回りの方向にそれぞれ設けられてい
る。この切欠き部12a,12b,12c,12dは、ピストン1の軸
心1aを軸心として、その噴口の数分均等分割した、すな
わち本実施例においては4等分した仮想分割面(第1図
において一点鎖線で示される)7A,7B,7C,7Dの方向の従
来の円柱状の空洞部の各壁面を、その方向面7A,7B,7C,7
D上にピストン1の軸心1aと方向が一致する軸心12A,12
B,12C,12Dを軸心として、底面に行くに従って大となる
円弧状に切欠いたものであり、該切欠き部12a,12b,12c,
12dの方向は前記噴霧方向に略一致対向している。そし
て、各切欠き部12a,12b,12c,12dの底面における軸心12
A,12B,12C,12Dを軸心とした切欠き円弧R1,R2,R3,R4の大
小関係はR1>R2>R3>R4となっている。また、各切欠き
部12a,12b,12c,12dの底面における横方向の凹み深さh1,
h2,h3,h4の大小関係はh1>h2>h3>h4となっている。
The difference between the combustion chamber of the piston of this embodiment and that of the prior art is that, as shown in FIGS. 1 and 2, the inner wall of the combustion chamber 12 in the spray direction is notched, and the notches 12a, 12b, 12c are formed. , 12d are made smaller as the angles θa, θb, θc, θd formed by the axis 3a of the injector 3 and the axes 6a, 6b, 6c, 6d of the nozzles 6A, 6B, 6C, 6D become larger. It is a point. Where θa, θb, θc,
The magnitude relationship of θd is θa <θb <θc <θd. Further, although the injection ports 6B and 6C are not shown in the drawing, the injection port 6B is provided in the clockwise direction of 90 ° of the injection port 6A, while the injection port 6C is provided in the 90 ° clockwise direction of the injection port 6D. . The cutouts 12a, 12b, 12c, 12d are evenly divided by the number of their injection ports with the shaft center 1a of the piston 1 as the shaft center, that is, in the present embodiment, are divided into four equal parts (Fig. 1). 7A, 7B, 7C, 7D in the direction of 7A, 7B, 7C, 7D
Shaft center 12A, 12 whose direction matches the shaft center 1a of piston 1 on D
B, 12C, 12D as an axis, is a notch in the shape of an arc that becomes larger toward the bottom, the notch 12a, 12b, 12c,
The direction of 12d substantially coincides with and opposes the spray direction. Then, the axial center 12 at the bottom of each notch 12a, 12b, 12c, 12d
The size relationship among the notched arcs R1, R2, R3, R4 with A, 12B, 12C, 12D as the center of axis is R1>R2>R3> R4. Further, the depth h1, which is the depth of the horizontal depression in the bottom surface of each notch 12a, 12b, 12c, 12d.
The size relationship of h2, h3, and h4 is h1>h2>h3> h4.

すなわち各切欠き部12a,12b,12c,12dの容積(容量)の
大小関係は12a>12b>12c>12dとなっており、インジェ
クタ3の軸心3aと噴口6A,6B,6C,6Dの軸心6a,6b,6c,6dと
のなす角θa,θb,θc,θdが大きくなる程、その噴霧の
対向位置に形成される切欠き部の容量は小さくなってい
る。なお、第1図中に仮想線で示される円弧は、燃焼室
底面とテーパ状円弧面の下方への延長線との交点を示し
ている。
That is, the size relationship between the volumes (capacities) of the cutouts 12a, 12b, 12c, 12d is 12a>12b>12c> 12d, and the shaft center 3a of the injector 3 and the shafts of the injection ports 6A, 6B, 6C, 6D are the same. The larger the angles θa, θb, θc, and θd formed by the cores 6a, 6b, 6c, and 6d, the smaller the volume of the notch formed at the opposing position of the spray. The arcs shown by imaginary lines in FIG. 1 indicate the points of intersection between the bottom of the combustion chamber and the downward extension of the tapered arc surface.

そして、この切欠き部12a,12b,12c,12dは、円弧R1,R2,R
3,R4を底面円弧として有する円錐形のカッタを、第2図
の仮想線で示されるように略円柱状空洞部をなす従来の
燃焼室に挿入し、各カッタの軸心を壁面に向かって仮想
分割面上でそれぞれ切削・移動することにより形成され
る。
The cutouts 12a, 12b, 12c, 12d form the arcs R1, R2, R
Insert a conical cutter having 3, R4 as a bottom arc into a conventional combustion chamber that forms a substantially cylindrical cavity as shown by the phantom line in Fig. 2, with the axial center of each cutter facing the wall surface. It is formed by cutting and moving on the virtual dividing plane.

このように構成されている本実施例の燃焼室によれば、
次のような効果を得ることができる。
According to the combustion chamber of this embodiment configured as described above,
The following effects can be obtained.

すなわち、噴霧方向の燃焼室の内壁を切欠き、その切欠
き部の容量を、インジェクタの軸心と噴口の軸心とのな
す角が大きくなる程小さくしている、すなわち噴霧量の
当接の多い壁面の切欠き部ほどその切欠き容量を多くし
ているので、インジェクタ3の軸心3aと、インジェクタ
3のそれぞれの噴口の軸心とのなす角θが大きくなる程
その噴霧量が減少するという特性により生じる各噴霧火
炎の不規則な形成を解消することが可能となり、すなわ
ち、各噴霧火炎全てが一定に形成でき、燃焼効率が向上
されるようになる。
That is, the inner wall of the combustion chamber in the spray direction is notched, and the capacity of the notch is made smaller as the angle between the axis of the injector and the axis of the injection port becomes larger, that is, the contact of the spray amount Since the notch portion of the wall surface has the larger notch volume, the spray amount decreases as the angle θ formed by the axis 3a of the injector 3 and the axis of each nozzle of the injector 3 increases. It is possible to eliminate the irregular formation of each spray flame caused by the above characteristic, that is, all spray flames can be formed uniformly and the combustion efficiency is improved.

また、このピストンの燃焼室12によれば、各切欠き部12
a,12b,12c,12dとも燃焼室上部から底面へと順次円弧状
切欠きが大きくなるよう形成されているので、燃料噴霧
がピストン1上部とシリンダヘッド4下面との間に形成
される隙間部9(第2図参照)へ移動しずらくなり、燃
焼室底面へ大半が誘導されるようになると共に、側壁面
円周の周長が長くなることから燃焼室中央部への燃料噴
霧の発達が抑えられ空気流速の大きい燃焼室側壁部(切
欠き部)へ混合気を集めることができ、燃料と空気との
混合を良好にして燃焼を行うことが可能となる。
Further, according to the combustion chamber 12 of this piston, each notch 12
Since a, 12b, 12c, and 12d are formed such that the arcuate notches gradually increase from the upper part to the bottom part of the combustion chamber, the fuel spray is formed in the gap between the upper part of the piston 1 and the lower surface of the cylinder head 4. 9 (see Fig. 2), it is difficult to move to the bottom of the combustion chamber, and most of it is guided to the bottom of the combustion chamber, and the circumferential length of the side wall circumference becomes long, so the development of fuel spray to the center of the combustion chamber Thus, the air-fuel mixture can be collected in the side wall portion (notch portion) of the combustion chamber where the air flow velocity is high, and the fuel and air can be mixed well and combustion can be performed.

次に、第2の実施例について説明する。Next, a second embodiment will be described.

この第2の実施例の燃焼室が第1の実施例のそれと異な
る点は、第3図に示されるように、切欠き部13a,13b,13
c,13dの容積の変化を、軸心13A,13B,13C,13Dを軸心とし
た切欠き円弧R1,R2,R3,R4の大きさのみで行い、横方向
の凹み深さh1,h2,h3,h4を全て等しい深さhとした点で
ある。
The difference between the combustion chamber of the second embodiment and that of the first embodiment is that, as shown in FIG. 3, the notches 13a, 13b, 13
Change the volume of c, 13d only by the size of the notched arcs R1, R2, R3, R4 with the shaft center 13A, 13B, 13C, 13D as the shaft center, and the lateral recess depths h1, h2, This is a point where h3 and h4 are all set to the same depth h.

このように燃焼室13を構成しても先の実施例と同様な効
果を得ることができるのは言うまでもない。
It goes without saying that even if the combustion chamber 13 is configured in this way, the same effects as those of the previous embodiment can be obtained.

次に、第3の実施例について説明する。Next, a third embodiment will be described.

この第3の実施例の燃焼室が第1の実施例のそれと異な
る点は、第4図に示されるように、切欠き部14a,14b,14
c,14dの容積の変化を、横方向の凹み深さh1,h2,h3,h4に
より行い、軸心14A,14B,14C,14Dを軸心とした切欠き円
弧R1,R2,R3,R4の大きさを全て等しい円弧Rとした点で
ある。
The difference between the combustion chamber of the third embodiment and that of the first embodiment is that, as shown in FIG. 4, the notches 14a, 14b, 14
Change the volume of c, 14d by the depth of the recesses h1, h2, h3, h4 in the lateral direction, and cutout arcs R1, R2, R3, R4 with the axes 14A, 14B, 14C, 14D as the axes. This is a point where all the sizes are the same circular arc R.

このように燃焼室14を構成しても第1の実施例と同様な
効果を得ることができるのは勿論のこと、切欠き部に応
じた円弧を有するカッタをそれぞれ備える必要がなく、
一個のカッタで切削ができるようになるので、製造コス
トの低減が図れるようになり、また、切欠き部の終端同
士(第4図における14P,14Q)を上記第1、第2の実施
例に比べて離間し得るので、隣同士の火炎干渉の防止が
可能となる。
Even if the combustion chamber 14 is configured in this way, it is of course possible to obtain the same effects as those of the first embodiment, and it is not necessary to provide cutters each having an arc corresponding to the cutout portion.
Since it becomes possible to cut with one cutter, the manufacturing cost can be reduced, and the ends of the notches (14P, 14Q in FIG. 4) can be changed to the first and second embodiments. Since they can be separated from each other, flame interference between adjacent ones can be prevented.

以上本考案者によってなされた考案を実施例に基づき具
体的に説明したが、本考案は上記実施例に限定されるも
のではなく、その要旨を逸脱しない範囲で種々変形可能
であることは言うまでもなく、例えば、上記実施例で
は、インジェクタの噴口の数を4個としているが、4個
に限られるものではない。
Although the invention made by the inventor has been specifically described based on the embodiments, the invention is not limited to the above-described embodiments, and it goes without saying that various modifications can be made without departing from the scope of the invention. For example, in the above-described embodiment, the number of injection holes of the injector is four, but the number is not limited to four.

なお、上記実施例は、傾斜して配置されたインジェクタ
から燃料噴霧を受ける燃料室全てに対して適用可能であ
り、インジェクタが2個以上設けられている場合等には
特に有効である。
The above-described embodiment is applicable to all the fuel chambers that receive fuel spray from the injectors arranged at an inclination, and is particularly effective when two or more injectors are provided.

(考案の効果) 以上のように本考案によれば、インジェクタの軸心と噴
口の軸心とのなす角が大きくなる程、その噴口に対応す
る切欠き部の容量を小さくするよう構成したので、各噴
口の噴霧量の差に拘らず一様な噴霧火炎がそれぞれ形成
されるようになり、燃焼効率が向上され、性能の改善が
図られるピストンの燃焼室となる。
(Effect of the Invention) As described above, according to the present invention, the larger the angle between the axis of the injector and the axis of the injection port, the smaller the volume of the notch corresponding to the injection port. , A uniform spray flame is formed regardless of the difference in the spray amount of each injection port, the combustion efficiency is improved, and the combustion chamber of the piston is improved.

【図面の簡単な説明】[Brief description of drawings]

第1図は本考案の一実施例を示すピストンの上面図、第
2図は第1図の側断面図、第3図は本考案の第2の実施
例を示すピストンの上面図、第4図は本考案の第3の実
施例を示すピストンの上面図、第5図は従来技術を示す
ディーゼル機関のピストン並びにその近傍部の要部断面
図である。 1…ピストン、1a…ピストンの軸心、2,12,13,14…燃焼
室、3…インジェクタ、3a…インジェクタの軸心、6A,6
D…噴口、6a,6d…噴口の軸心、7A,7B,7C,7D…仮想分割
面、12A〜12D,13A〜13D,14A〜14D…切欠き部の軸心、12
a〜12d,13a〜13d,14a〜14d…切欠き部、R、R1,R2,R3,R
4・…円弧、θa,θd…インジェクタの軸心と噴口の軸
心とのなす角。
1 is a top view of a piston showing an embodiment of the present invention, FIG. 2 is a side sectional view of FIG. 1, FIG. 3 is a top view of a piston showing a second embodiment of the present invention, and FIG. FIG. 5 is a top view of a piston showing a third embodiment of the present invention, and FIG. 5 is a cross-sectional view of a piston of a diesel engine showing a conventional technique and a main part in the vicinity thereof. 1 ... Piston, 1a ... Piston axis, 2, 12, 13, 14 ... Combustion chamber, 3 ... Injector, 3a ... Injector axis, 6A, 6
D ... Nozzle, 6a, 6d ... Nozzle axis, 7A, 7B, 7C, 7D ... Virtual dividing plane, 12A-12D, 13A-13D, 14A-14D ... Notch part axis, 12
a to 12d, 13a to 13d, 14a to 14d ... Notch, R, R1, R2, R3, R
4 ··· Arc, θa, θd… Angle formed by the axis of the injector and the axis of the injection port.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 【請求項1】傾斜して配置されたインジェクタの噴口か
らの燃料噴霧を受ける略円柱状空洞部をなすピストンの
燃焼室において、前記ピストンの軸心を軸心として、そ
の噴口の数分、均等分割した仮想分割面の方向の前記空
洞部の壁面を、その方向面上に前記ピストンの軸心と方
向が一致する軸心を有し、底面に行くに従って大となる
円弧状に切欠き、該切欠き部を前記噴霧方向に略一致対
向させ、前記インジェクタの軸心と前記噴口の軸心との
なす角が大きくなる程、その噴口に対応する切欠き部の
容量を小さくするよう構成したことを特徴とするピスト
ンの燃焼室。
1. In a combustion chamber of a piston having a substantially cylindrical hollow portion which receives fuel spray from an injector nozzle arranged obliquely, the axis of the piston is taken as an axis and the number of the nozzles is equal. The wall surface of the hollow portion in the direction of the divided virtual dividing surface has an axial center whose direction coincides with the axial center of the piston on the directional surface, and is cut out in an arc shape that becomes larger toward the bottom surface, The notches are arranged so as to face each other substantially in the spray direction, and the larger the angle between the axis of the injector and the axis of the injection port, the smaller the volume of the notch corresponding to the injection port. Combustion chamber of the piston.
JP1040688U 1988-01-28 1988-01-28 Piston combustion chamber Expired - Lifetime JPH0730909Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1040688U JPH0730909Y2 (en) 1988-01-28 1988-01-28 Piston combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1040688U JPH0730909Y2 (en) 1988-01-28 1988-01-28 Piston combustion chamber

Publications (2)

Publication Number Publication Date
JPH01114921U JPH01114921U (en) 1989-08-02
JPH0730909Y2 true JPH0730909Y2 (en) 1995-07-19

Family

ID=31218039

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1040688U Expired - Lifetime JPH0730909Y2 (en) 1988-01-28 1988-01-28 Piston combustion chamber

Country Status (1)

Country Link
JP (1) JPH0730909Y2 (en)

Also Published As

Publication number Publication date
JPH01114921U (en) 1989-08-02

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