JPS6338601A - Rotary engine - Google Patents

Rotary engine

Info

Publication number
JPS6338601A
JPS6338601A JP18254686A JP18254686A JPS6338601A JP S6338601 A JPS6338601 A JP S6338601A JP 18254686 A JP18254686 A JP 18254686A JP 18254686 A JP18254686 A JP 18254686A JP S6338601 A JPS6338601 A JP S6338601A
Authority
JP
Japan
Prior art keywords
seal
apex
rotor
rollers
apex seal
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.)
Pending
Application number
JP18254686A
Other languages
Japanese (ja)
Inventor
Yoshihiro Bando
坂東 好博
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.)
Bando Kiko Co Ltd
Original Assignee
Bando Kiko Co 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 Bando Kiko Co Ltd filed Critical Bando Kiko Co Ltd
Priority to JP18254686A priority Critical patent/JPS6338601A/en
Publication of JPS6338601A publication Critical patent/JPS6338601A/en
Priority to US07/240,434 priority patent/US4822262A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To reduce leakage of gas from axial both ends of a rotor, by smoothening a motion of an apex seal for improving the following motion of this apex seal on a sliding surface of a rotor housing, and raising air-tightness between the apex seal and said sliding surface. CONSTITUTION:Recessed grooves 7 are formed on both side walls of a seal groove, piercingly between axial both ends, plural slender rollers 5 are contained in these recessed grooves 7, and an apex seal 3 and the side walls of the seal groove are rollingly contacted with each other through these rollers 5. In this way, a motion (a radial motion) of the apex seal 3 is smoothened. On the other hand, as the rollers 5 and the recessed grooves 7 which contain these rollers 5, are contained in a corner seal 6 which is attached onto both sides of the top of a rotor, for being covered with this corner seal 6, a route for combustion gas (or compressed gas) from the bottom of the seal groove 8 of the apex seal 3, is intercepted, and consequently, leakage of gas is reduced, and good airtightness can be got.

Description

【発明の詳細な説明】 本発明は、ロータリーエンジンの1コ一ター頂点のアペ
ックスシール部の改良に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an improvement of an apex seal portion at the apex of one rotary engine.

特に、ローター頂点のシール溝側壁とアペックスシール
との間にローラーを組み込み、アペックスシールの肋さ
く半径方向の)を軽くし、ローターハウジングのすべり
而とアペックスシールとの気密を向上ざUるようにした
ロータリーエンジンの改良に係る。
In particular, a roller is incorporated between the seal groove side wall at the rotor apex and the apex seal to reduce the weight of the apex seal (in the radial direction) and improve the airtightness between the rotor housing and the apex seal. This relates to improvements to the rotary engine.

ところで、アペックスシールの手刀きを軽くするために
は、出来るだけアペックスシールの全幅に渡ってローラ
ーにより支える方が効果的で、ローラーをロータ全幅(
軸方向に沿った)を貫き通しを入れるとよい。
By the way, in order to make the apex seal easier to handle, it is more effective to support the entire width of the apex seal with a roller as much as possible.
It is best to make a through hole (along the axial direction).

しかし、ローラーをローター全幅に員いて入れると、こ
れらローラーに沿ってまた、ローラーを収める凹溝がガ
ス通路のとなり、アペックスシールのシール溝に導入し
た燃焼ガス(又は、圧縮ガス)がローター側面に漏れ出
て、隣り合う両作業7間の見方を悪くするのである。
However, when the rollers are inserted across the entire width of the rotor, the concave grooves that accommodate the rollers become gas passages, and the combustion gas (or compressed gas) introduced into the seal groove of the apex seal flows onto the side of the rotor. This leaks out and makes it difficult to see between the two adjacent operations 7.

そこで、本発明は、アペックスシールの動きを軽くして
ローターハウジングのすべり面への追従をよくし、この
すべり而との気密を向上を図るともに、ローターの軸方
向両端からのガス漏れを少くしたロータリーエンジンを
提供するにある。
Therefore, the present invention aims to lighten the movement of the apex seal to better follow the sliding surface of the rotor housing, improve airtightness with this sliding surface, and reduce gas leakage from both ends of the rotor in the axial direction. Located in providing rotary engine.

以下、本発明の実施例を図面により説明する。Embodiments of the present invention will be described below with reference to the drawings.

1はローターハウジングのすべり面、2はローク−頂点
部、3はアペックスシール、4はシール;1η側壁、5
はローラー、6はコーナシール、11はアペックスシー
ルスプリングである。
1 is the sliding surface of the rotor housing, 2 is the rake apex, 3 is the apex seal, 4 is the seal; 1η side wall, 5
is a roller, 6 is a corner seal, and 11 is an apex seal spring.

第1図及び第2図に示されるように、シール溝側壁4に
、軸方向両端に渡って頁通さゼた凹溝7を形成し、この
凹溝1に細良いローラー5を複数個収め、これらローラ
ー5にJ:リアペックスシール3とシール溝側壁4とを
転がり接触させる。
As shown in FIGS. 1 and 2, a concave groove 7 is formed in the seal groove side wall 4 across both ends in the axial direction, and a plurality of thin rollers 5 are housed in the concave groove 1. J: The rear pex seal 3 and the seal groove side wall 4 are brought into rolling contact with these rollers 5.

一方、軸方向の両端部側には、シール溝8のサイドハイ
ジング9に突き合すコーナーシール6及び6が組み込ま
れ、上記ローター5は、これらコーナーシール6及び6
間に収められ、ローラー側端が、ローター側端に露出さ
せない。
On the other hand, corner seals 6 and 6 that abut against the side housings 9 of the seal groove 8 are incorporated at both ends in the axial direction, and the rotor 5
The roller side edge is not exposed to the rotor side edge.

両側のコーナーシール6及び6は、普通に全体形状が円
筒ビン状であるが、第3図に示すように、円筒の一部を
カットし、ローラー収め部10を形成し、L形状としで
ある。
The corner seals 6 and 6 on both sides usually have a cylindrical bottle shape as a whole, but as shown in FIG. 3, a part of the cylinder is cut to form a roller accommodating part 10, making it L-shaped. .

このような形状のコーナーシール6及び6を組み込んだ
状態、ローラー5の収納の凹溝7及びローラー5の両端
をコーナーシール6の収め部10に収め、ローター外喘
に露出さぜイCいよ・うにしである。
With the corner seals 6 and 6 having such shapes installed, store the concave groove 7 for storing the roller 5 and both ends of the roller 5 in the housing part 10 of the corner seal 6, and expose them to the rotor outer shell. It's sea urchin.

上記のようになる本発明によると、 アペックスシール3は略々全幅近くに渡ってローラー5
及び5により転がり支持されて、1FJJさく半径方向
)が軽くなっていると共に、一方、このアペックスシー
ル3を支えるローラー5及び5、また、これらローラー
5及び5を収める凹溝7がローター頂点の両側に組イ→
(Jたコープ−シール6及び6の内方に収められ、これ
らローラーシール6及び6により被覆されるため、アペ
ックスシール3のシール溝8の底よりの燃焼ガス(又、
圧゛粗ガス)通路が遮断される結果、これらガス漏れが
少なく、良好な気密がiffられるのである。
According to the present invention as described above, the apex seal 3 extends almost over the entire width of the roller 5.
The rollers 5 and 5 that support this apex seal 3 and the concave groove 7 that accommodates these rollers 5 and 5 are formed on both sides of the rotor apex. ni group i →
(The combustion gas from the bottom of the seal groove 8 of the apex seal 3 (also
As a result of the (crude gas) passage being blocked, there is less leakage of these gases and good airtightness is achieved.

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

第1図の要部の側面図、第2図は要部の横断面1・・・
ローターハウジングのすべり面、2・・・ローター頂点
部、3・・・アペックスシール、・1・・・シール溝側
壁、5・・・ローラー、6・・・コーナーシール、7・
・・凹溝、8・・・シール溝、9・・・コーナーシール
のローラー収め部、 第1蘭 二1 第2@ 準5m
Figure 1 is a side view of the main part, Figure 2 is a cross section of the main part 1...
Sliding surface of rotor housing, 2... Rotor apex, 3... Apex seal, 1... Seal groove side wall, 5... Roller, 6... Corner seal, 7...
... Concave groove, 8... Seal groove, 9... Corner seal roller housing, 1st Run 21 2nd @ Semi-5m

Claims (1)

【特許請求の範囲】[Claims] ローター頂点のシール溝側壁とアペックスシールとの間
にローターを挿入し、シール溝側壁とアペックスシール
とを転り接触させるようにしたロータリーエンジンにお
いて、上記ローラは、上記シール溝側壁に形成させた凹
溝に収められ、この凹溝及びローラの両側端面が、ロー
ター両側に組み込んだ両コーナーシールの内方に収めら
れ、ローターの両端面に露出させないようにしたロータ
リーエンジン。
In a rotary engine in which a rotor is inserted between a seal groove side wall at the apex of the rotor and an apex seal, and the seal groove side wall and the apex seal are brought into rolling contact, the roller is moved through a recess formed in the seal groove side wall. A rotary engine in which the concave groove and both side end faces of the roller are housed inside both corner seals built into both sides of the rotor so that they are not exposed to both end faces of the rotor.
JP18254686A 1985-11-19 1986-08-02 Rotary engine Pending JPS6338601A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
JP18254686A JPS6338601A (en) 1986-08-02 1986-08-02 Rotary engine
US07/240,434 US4822262A (en) 1985-11-19 1988-09-01 Rotary engine having rollers for the apex seal

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP18254686A JPS6338601A (en) 1986-08-02 1986-08-02 Rotary engine

Publications (1)

Publication Number Publication Date
JPS6338601A true JPS6338601A (en) 1988-02-19

Family

ID=16120176

Family Applications (1)

Application Number Title Priority Date Filing Date
JP18254686A Pending JPS6338601A (en) 1985-11-19 1986-08-02 Rotary engine

Country Status (1)

Country Link
JP (1) JPS6338601A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5039288A (en) * 1988-06-08 1991-08-13 Bando Kiko Co., Limited Rotary engine having an apex seal member
US7303380B1 (en) * 2006-02-14 2007-12-04 Dave Atkins Rotary engine with improved seal assembly

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5039288A (en) * 1988-06-08 1991-08-13 Bando Kiko Co., Limited Rotary engine having an apex seal member
US7303380B1 (en) * 2006-02-14 2007-12-04 Dave Atkins Rotary engine with improved seal assembly

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