JPH057526B2 - - Google Patents
Info
- Publication number
- JPH057526B2 JPH057526B2 JP12838383A JP12838383A JPH057526B2 JP H057526 B2 JPH057526 B2 JP H057526B2 JP 12838383 A JP12838383 A JP 12838383A JP 12838383 A JP12838383 A JP 12838383A JP H057526 B2 JPH057526 B2 JP H057526B2
- Authority
- JP
- Japan
- Prior art keywords
- apex seal
- sliding
- recesses
- rotary piston
- piston engine
- 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
- 229910000990 Ni alloy Inorganic materials 0.000 claims description 7
- 238000007747 plating Methods 0.000 claims description 7
- 238000005422 blasting Methods 0.000 description 3
- 239000003921 oil Substances 0.000 description 3
- 229910001018 Cast iron Inorganic materials 0.000 description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 2
- 230000002159 abnormal effect Effects 0.000 description 2
- 238000005299 abrasion Methods 0.000 description 2
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229910010271 silicon carbide Inorganic materials 0.000 description 2
- 229910052582 BN Inorganic materials 0.000 description 1
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 230000000903 blocking effect Effects 0.000 description 1
- 239000002131 composite material Substances 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
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009713 electroplating Methods 0.000 description 1
- 238000005530 etching Methods 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 239000010687 lubricating oil Substances 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- CWQXQMHSOZUFJS-UHFFFAOYSA-N molybdenum disulfide Chemical compound S=[Mo]=S CWQXQMHSOZUFJS-UHFFFAOYSA-N 0.000 description 1
- 229910052982 molybdenum disulfide Inorganic materials 0.000 description 1
- 229910052759 nickel Inorganic materials 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 239000004810 polytetrafluoroethylene Substances 0.000 description 1
- 229920001343 polytetrafluoroethylene Polymers 0.000 description 1
- 238000007788 roughening Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000002195 synergetic effect Effects 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- 239000011135 tin Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Landscapes
- Pistons, Piston Rings, And Cylinders (AREA)
- Lubrication Of Internal Combustion Engines (AREA)
Description
(産業上の利用分野)
本発明は、ロータリピストンエンジンのアペツ
クスシール、特にその摺動面の改良に関するもの
である。
(従来技術)
一般に、ロータリピストンエンジンにおいて、
ロータハウジングのトロコイド面に摺接する摺動
部を備えた合金鋳鉄製のアペツクスシールは初期
なじみ性が悪いと、アペツクスシールの摺動部
(摺動面)が異常発熱し、アペツクスシール上下
の温度差によつて中凸状に変形し、その結果、ア
ペツクスシールの中央部が溶着摩耗を起こし、ま
た、常温下(運転中止)で逆に中凹状に変形し、
ガスシール性が低下し、エンジンの圧縮圧力の低
下が発生するということが知られている。
そこで、従来、初期なじみ性を良くするため
に、錫、銅、亜鉛等の軟質金属をメツキしたり、
シヨツトブラスト等により表面を粗面化したりし
て、油保特性をもたせるとともに全当たりを避け
ることなどの方法が行われている。ところが、こ
れらの方法においては、メツキ金属のかたさが低
いことや摺動時の面圧が高くなること等によつて
摩耗速度が早くなり、わずかのラツピング時間で
効果がなくなるという不具合がある。特に、近
年、採用されつつあるターボ過給機を備えた高出
力エンジンでは問題となる。
因に、先行技術は、ロータハウジングとの摺接
面にシヨツトブラストにより梨地面を形成したも
のとして、特公昭56−50081号がある。
(発明の目的)
本発明はかかる点に鑑みてなされたもので、初
期なじみ性に優れたロータリピストンエンジンの
アペツクスシールを提供することを目的とする。
(発明の構成)
本発明は、チル加工されロータハウジングのト
ロイド面に摺接する摺動部を備えたロータリピス
トンエンジンのアペツクスシールの改良に係るも
のである。
本発明は、上述した目的を達成するために、上
記アペツクスシールの摺動部の表面が粗面化され
て多数の凹部が形成され、該多数の凹部を残した
ままでかたさHv500〜900の無電解ニツケル合金
メツキ層が積層されていることを特徴とするもの
である。
なお、無電解ニツケル合金メツキには、無電解
ニツケルで、黒鉛、二硫化モリブデン、ボロンナ
イトライド、PTFE等の粒子を複合させたものを
用いてもよい。
ここで、無電解ニツケル合金メツキの代わりに
電気メツキを用いると、つきまわり性が悪いた
め、前記多数の凹部をそのまま残すことは困難で
あり、密着性が悪いという不具合がある。
(実施例)
以下、本発明の実施例を図面に沿つて詳細に説
明する。
第1図に示すところのロータリピストンエンジ
ン1は、そのケーシング2が内周面がトロコイド
面3aとなつているロータハウジング3の両側に
サイドハウジング(図示せず)を配設して構成さ
れ、しかしてケーシング2内において、略三角形
状のロータ4が偏心軸5に支承され、矢符A方向
に遊星回転運動するようになつている。ロータ4
の各頂部に、ロータハウジング3のトロコイド面
3aに摺接する摺動部6aを備えた合金鋳鉄製の
アペツクスシール6が装着されている。
また、ロータハウジング3には、吸気ポート7
および排気ポート8がそれぞれ形成されるととも
に、トレーリング側点火プラグ9およびリーデイ
ング側点火プラグ10がそれぞれ配設され、一
方、ロータ4にはサイドシール11が取付けられ
ている。
上記アペツクスシール6は、油保持機能をもた
せて全当たりを回避するために、チル加工された
アペツクスシール素材21のチル表面(かたさ
Hv700〜900)を、エツチング、シヨツトブラス
ト等の方法により粗面化して多数の凹部21aを
形成し(第2図a参照)、その後、その多数の凹
部21aを残したままで(すなわち多数の凹凹部
21aを塞ぐことなく)、ロータハウジング3の
トロコイド面3aとのなじみ性が良く焼付きが起
こりにくく、しかもつきまわり性に優れた無電解
ニツケル合金メツク層22を積層する(第2図b
参照)ことにより、製造される。
続いて、上記アペツクスシール6に対して行つ
た試験について説明する。
試験方法
第3図に示すところのアペツクスシール6を用
いて、第4図に示す外接揺動式ドラムテスター
で、摩耗試験および焼付け試験を行つた。なお、
第3図において、L1=56mm、L2=8.5mm、L3=2
mm、L4=3mm、R1=2mmで、Pは熱電対取付位
置を示す。しかして、試験に用いたアペツクスシ
ール6は第1表に示す通りである。実施例(M)は自
己潤滑型複合メツキが施されたものである。
(Industrial Application Field) The present invention relates to an apex seal of a rotary piston engine, and particularly to improvement of its sliding surface. (Prior art) Generally, in a rotary piston engine,
If the apex seal, which is made of alloy cast iron and has a sliding part that comes into sliding contact with the trochoidal surface of the rotor housing, has poor initial conformability, the sliding part (sliding surface) of the apex seal will generate abnormal heat, causing the upper and lower parts of the apex seal to The apex seal deforms into a convex shape due to the temperature difference, resulting in welding wear at the center of the apex seal, and conversely deforms into a concave shape at room temperature (when operation is stopped).
It is known that gas sealing performance is reduced and engine compression pressure is reduced. Therefore, conventionally, in order to improve initial conformability, soft metals such as tin, copper, and zinc were plated.
Methods such as roughening the surface by shot blasting or the like to provide oil retaining properties and to avoid complete contact are being used. However, these methods have a problem in that the hardness of the plated metal is low and the surface pressure during sliding is high, so that the rate of wear increases and the wrapping becomes ineffective after a short wrapping time. This is particularly a problem with high-output engines equipped with turbochargers, which have been increasingly adopted in recent years. Incidentally, as a prior art, there is Japanese Patent Publication No. 56-50081 in which a matte surface is formed by shot blasting on the sliding contact surface with the rotor housing. (Object of the Invention) The present invention has been made in view of the above points, and an object of the present invention is to provide an apex seal for a rotary piston engine that has excellent initial conformability. (Structure of the Invention) The present invention relates to an improvement of an apex seal for a rotary piston engine, which is provided with a sliding portion that is chilled and comes into sliding contact with a toroidal surface of a rotor housing. In order to achieve the above-mentioned object, the present invention provides that the surface of the sliding part of the apex seal is roughened to form a large number of recesses, and that the surface of the sliding part of the apex seal is roughened and has a hardness of 500 to 900 Hv while leaving the large number of recesses. It is characterized by laminated electrolytic nickel alloy plating layers. Note that electroless nickel alloy plating may be made of electroless nickel composited with particles of graphite, molybdenum disulfide, boron nitride, PTFE, or the like. Here, if electroplating is used instead of electroless nickel alloy plating, it is difficult to leave the large number of recesses as they are due to poor throwing power, and there is a problem of poor adhesion. (Example) Hereinafter, an example of the present invention will be described in detail with reference to the drawings. The rotary piston engine 1 shown in FIG. 1 has a casing 2 that is constructed by disposing side housings (not shown) on both sides of a rotor housing 3 whose inner peripheral surface is a trochoidal surface 3a. Inside the casing 2, a substantially triangular rotor 4 is supported by an eccentric shaft 5 and is configured to rotate planetarily in the direction of arrow A. Rotor 4
An apex seal 6 made of alloyed cast iron and having a sliding portion 6a that comes into sliding contact with the trochoidal surface 3a of the rotor housing 3 is attached to the top of each of the rotor housings. The rotor housing 3 also has an intake port 7.
and an exhaust port 8 are formed, and a trailing side spark plug 9 and a leading side spark plug 10 are respectively provided, while a side seal 11 is attached to the rotor 4. The above-mentioned apex seal 6 has a chilled surface (hardness) of the apex seal material 21 which has been chilled in order to have an oil retaining function and avoid full contact.
Hv700 to 900) is roughened by etching, shot blasting, etc. to form a large number of recesses 21a (see Fig. 2a), and then, the large number of recesses 21a remain (that is, a large number of recesses and recesses are formed). The electroless nickel alloy mesh layer 22, which has good compatibility with the trochoidal surface 3a of the rotor housing 3, is hard to cause seizure, and has excellent throwing power, is laminated without blocking the trochoidal surface 3a of the rotor housing 3 (see Fig. 2b).
(see). Next, a test conducted on the apex seal 6 will be explained. Test Method Using the apex seal 6 shown in FIG. 3, a wear test and a seizure test were conducted using a circumscribed swinging drum tester shown in FIG. 4. In addition,
In Figure 3, L 1 = 56mm, L 2 = 8.5mm, L 3 = 2
mm, L 4 = 3 mm, R 1 = 2 mm, and P indicates the thermocouple mounting position. The Apex Seal 6 used in the test is shown in Table 1. In Example (M), self-lubricating composite plating was applied.
【表】【table】
【表】
また、上記アペツクスシール6の実施例の化学
成分は、第1表の備考において特に指定する場合
を除き、第2表に示す通りである。[Table] Furthermore, the chemical components of the examples of Apex Seal 6 are as shown in Table 2, unless otherwise specified in the notes of Table 1.
【表】
さらに、アペツクスシール6の摺動部6aの表
面仕上げは、次の通りである。
研摩仕上げ
砥石:GC#
60(JIS)
アラサ:1、6a
シヨツトブラスト仕上げ
シヨツト:カーボランダム#
20(シリコンカ
ーバイド)
アラサ:10〜40〓
また、外接揺動式ドラムテスター31におい
て、32はCrメツキした回転ドラム、33は潤
滑油を滴下するノズル、34は揺動部材で、アペ
ツクスシール6がスプリング35にて回転ドラム
32表面に常時圧接されるように取付けられ、角
度〓でもつて揺動するようになつている。しかし
て、セツト荷重:18Kg/56mm長さ、ドラム外径
176mm、潤滑油:10W−40、すべり速度6.5m/
sec(710rpm)である。
試験結果
摩耗試験後のアペツクスシール6の摺動面の形
状は、第5図に示す通りである。また、摩耗量S
は第3表に示す通りである(摩耗量Sについては
第5図の実施例(a)参照)。
したがつて、本発明に係る実施例(h)、(j)、(k)、
(l)は摺動面の形状の変化が小さく、摩耗量Sも少
なく、適度に摩耗して初期なじみ性がよいことが
わかる。なお、摩耗量Sは、具体的には第3表に
示す通りである。[Table] Furthermore, the surface finish of the sliding portion 6a of the apex seal 6 is as follows. Polishing finish Grinding wheel: GC# 60 (JIS) Abrasion: 1, 6a Shot blast finish Shot: Carborundum # 20 (silicon carbide) Abrasion: 10 to 40 Also, in the external oscillating drum tester 31, 32 is Cr plated 33 is a nozzle for dripping lubricating oil, 34 is a swinging member, and the apex seal 6 is attached to the surface of the rotating drum 32 by a spring 35 so that it is constantly pressed against it, and swings at an angle of . It's becoming like that. Therefore, set load: 18Kg/56mm length, drum outer diameter
176mm, lubricant: 10W-40, sliding speed 6.5m/
sec (710 rpm). Test Results The shape of the sliding surface of the apex seal 6 after the wear test is as shown in FIG. In addition, the amount of wear S
is as shown in Table 3 (see Example (a) in FIG. 5 for the amount of wear S). Therefore, Examples (h), (j), (k),
It can be seen that (l) has a small change in the shape of the sliding surface, a small amount of wear S, moderate wear, and good initial conformability. Note that the wear amount S is specifically as shown in Table 3.
【表】【table】
【表】
一方、焼付き試験の結果は、第6図に示す通り
で、本発明に係る実施例(h)、(j)、(k)、(l)は、他の
ものが焼付けを起こしているのに60分を経過して
も焼付けを起こさないことが判る。
(発明の効果)
本発明は上記のように構成したから、多数の凹
部による良好な摩耗促進および油保持、ならびに
適当なかたさを有する無電解型ニツケル合金メツ
キ層との相乗効果により、初期なじみ性が良くな
り、シールの焼付き→異常摩耗→圧縮圧力の低下
の発生を防止できる。[Table] On the other hand, the results of the seizure test are as shown in Figure 6, and in Examples (h), (j), (k), and (l) according to the present invention, other materials caused seizure. It can be seen that no burn-in occurs even after 60 minutes. (Effects of the Invention) Since the present invention is configured as described above, the initial conformability is improved due to the synergistic effect of the multi-recessed portions that promote wear and oil retention, and the electroless nickel alloy plating layer that has appropriate hardness. This improves seal seizing, abnormal wear, and decreases in compression pressure.
図面は本発明の実施態様を例示するもので、第
1図はロータリピストンエンジンの全体構成図、
第2図a,bはアペツクスシールの製造法の説明
図、第3図はアペツクスシール試料の説明図、第
4図は試験システムを示す説明図、第5図および
第6図は試験結果を示す図である。
1……ロータリピストンエンジン、3……ロー
タハウジング、3a……トロコイド面、6……ア
ペツクスシール、6a……摺動部、22……無電
解型ニツケル合金メツキ層。
The drawings illustrate embodiments of the present invention, and FIG. 1 is an overall configuration diagram of a rotary piston engine;
Figures 2a and b are illustrations of the manufacturing method of Apex Seal, Figure 3 is an illustration of the Apex Seal sample, Figure 4 is an illustration of the test system, and Figures 5 and 6 are the test results. FIG. DESCRIPTION OF SYMBOLS 1... Rotary piston engine, 3... Rotor housing, 3a... Trochoid surface, 6... Apex seal, 6a... Sliding part, 22... Electroless nickel alloy plating layer.
Claims (1)
面に摺接する摺動部を備えたロータリピストンエ
ンジンのアペツクスシールであつて、前記摺動部
の表面が粗面化されて多数の凹部が形成され、該
多数の凹部を残したままでかたさHv500〜900の
無電解ニツケル合金メツキ層が積層されているこ
とを特徴とするロータリピストンエンジンのアペ
ツクスシール。1. An apex seal for a rotary piston engine, which is provided with a sliding part that is chilled and comes into sliding contact with a trochoidal surface of a rotor housing, wherein the surface of the sliding part is roughened to form a large number of recesses, and the surface of the sliding part is roughened to form a large number of recesses. An apex seal for a rotary piston engine characterized by a laminated layer of electroless nickel alloy plating with a hardness of Hv500 to 900 while leaving a recessed part.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP12838383A JPS6019901A (en) | 1983-07-13 | 1983-07-13 | Apex seal for rotary piston type engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP12838383A JPS6019901A (en) | 1983-07-13 | 1983-07-13 | Apex seal for rotary piston type engine |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS6019901A JPS6019901A (en) | 1985-02-01 |
JPH057526B2 true JPH057526B2 (en) | 1993-01-29 |
Family
ID=14983455
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP12838383A Granted JPS6019901A (en) | 1983-07-13 | 1983-07-13 | Apex seal for rotary piston type engine |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6019901A (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5573390A (en) * | 1993-03-25 | 1996-11-12 | Surtec Kariya Co., Ltd. | Coated sliding material |
DE10340990A1 (en) * | 2003-09-05 | 2005-04-28 | Ks Kolbenschmidt Gmbh | Finished surface of the bolt holes of a piston |
-
1983
- 1983-07-13 JP JP12838383A patent/JPS6019901A/en active Granted
Also Published As
Publication number | Publication date |
---|---|
JPS6019901A (en) | 1985-02-01 |
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