JPH03901A - Rotary engine - Google Patents

Rotary engine

Info

Publication number
JPH03901A
JPH03901A JP13695989A JP13695989A JPH03901A JP H03901 A JPH03901 A JP H03901A JP 13695989 A JP13695989 A JP 13695989A JP 13695989 A JP13695989 A JP 13695989A JP H03901 A JPH03901 A JP H03901A
Authority
JP
Japan
Prior art keywords
rotor
sides
housing
hole
rotary 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.)
Pending
Application number
JP13695989A
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 JP13695989A priority Critical patent/JPH03901A/en
Priority to US07/448,100 priority patent/US5121721A/en
Priority to CA002006457A priority patent/CA2006457A1/en
Priority to EP89313501A priority patent/EP0376642A1/en
Publication of JPH03901A publication Critical patent/JPH03901A/en
Priority to US07/814,615 priority patent/US5181489A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To eliminate the pressure difference between the space between both sides so as to improve performance by providing a through hole open to both sides of a rotor for communicating the space between both the sides encircled by a side seal in both the sides of the rotor with each other. CONSTITUTION:A rotor 1 is stored in a rotor housing 2, a side housing 3 and an intermediate housing 4, whereas a through hole 6 open to both sides of it is provided near the top of a rotor 1. Through the through hole 6, the space between both the sides 7, 8 formed inside a side seal in both the sides of the rotor 1 are communicated with each other to eliminate the pressure difference between these. This prevents the rotor 1 from being positioned to one side and makes the side seal slide on both sides in proper conditions along the opposing side housing 3. It is thus possible to prevent high pressure gas from blowing toward the side seals and entering the rotor 1.

Description

【発明の詳細な説明】 (1)産業上の利用分野 本発明は、トロコイド状ローターハウジングと、このハ
ウジング内に収められ、偏心軸上に偏心取付けられたロ
ーターとを有するロータリーエンジンの改良に関する。
DETAILED DESCRIPTION OF THE INVENTION (1) Industrial Application Field The present invention relates to an improvement in a rotary engine having a trochoidal rotor housing and a rotor housed within the housing and eccentrically mounted on an eccentric shaft.

特に本発明は、ローターを挾んで両側のサイドハウジン
グ、インターナデエイトハウジングとの問、ローター側
面空間(サイドシール内方の)同士のガス圧均衡を図っ
たものである。
In particular, the present invention attempts to balance the gas pressure between the side housings and internal housings on both sides of the rotor, and between the rotor side spaces (inside the side seals).

即ち、ローターを片寄せさせるローター両側の側面空間
同士のガス圧差を解浦したものである。
That is, the gas pressure difference between the side spaces on both sides of the rotor, which causes the rotor to shift to one side, is eliminated.

ローターを挾んだこれら側面空間のガス圧力着は、次の
様なことで生じている。
Gas pressure build-up in the side spaces surrounding the rotor occurs due to the following reasons.

即ち、ローター側面のサイドシールはそれぞれ巨視的に
見れば、各々寸法、形状及びシール溝とのスベリ具合の
相異等によってローター表面の高温高圧燃焼ガスの侵入
程度がローター両側の側面空間で相異する。また、 (2)従来の技術 従来のインゼクターによる電子制御燃料噴射方式のロー
タリーエンジンは、インゼクター装置側の吸気ボートは
、他方サイドハウジング側に配置した吸気ボートに比べ
小径となり、このため両者の吸気ボートは配置がずれて
設けられている。
In other words, when looking at the side seals on the side surfaces of the rotor macroscopically, the degree of intrusion of high-temperature, high-pressure combustion gas on the rotor surface differs between the side spaces on both sides of the rotor due to differences in size, shape, and degree of sliding with the seal groove. do. In addition, (2) Prior Art In the conventional electronically controlled fuel injection type rotary engine using an injector, the intake boat on the injector device side has a smaller diameter than the intake boat located on the side housing side. The intake boats are provided at different locations.

従って、吸気ボートの開口出発部は互にずれて位置して
いる。
Therefore, the opening starting parts of the intake boats are located offset from each other.

(3)発明が解決しようとする問題点 ところで、従来の上記のようローターを挾んで両側に配
置した吸気ボートの位置(特に開口出発部のそれぞれ)
が、上記のように大幅にずれていると、ローターの回転
に従い、ローター両側における空間が、吸気ボートと繋
る時間に差が生じている。
(3) Problems to be solved by the invention By the way, the positions of the intake boats (especially at the opening starting parts), which are placed on both sides of the rotor as described above, are conventional.
However, if there is a large deviation as described above, there will be a difference in the time that the spaces on both sides of the rotor connect with the intake boat as the rotor rotates.

すると、ローター側面、特にサイドシールより内方に漏
れ、侵入した高圧ガスはローターの一方の側面空間、つ
まり吸気ボートと早く繋る側面空間の高圧ガスは早く抜
けて圧力が低下し、他方、吸気ボートとまだ繋っていな
い他方の側面空間は高圧ガスが存在し、この高圧ガスの
圧力でローターが片寄せされる。このローターの片寄せ
現象によってローター両側面の一方は、サイドハウジン
グに強く押し付けられ、他方はサイドシールがサイドハ
ウジング摺動から瞬間的に離れる。
Then, the high-pressure gas leaks inward from the side of the rotor, especially the side seal, and the high-pressure gas that enters into the space on one side of the rotor, that is, the side space that connects quickly to the intake boat, quickly escapes and the pressure decreases, while the other side High-pressure gas exists in the other side space that is not yet connected to the boat, and the rotor is pushed to one side by the pressure of this high-pressure gas. Due to this rotor shifting phenomenon, one of the two side surfaces of the rotor is strongly pressed against the side housing, and the other side seal is momentarily separated from the sliding movement of the side housing.

このため、ローターの一方の側面はサイドハウジングと
摩擦抵抗を生じさせていると共に、他方の側面空間(サ
イドシールの内方)がわは高圧ガスのサイドシール上の
吹き扱けで内方にガス漏れし、カス漏れ現↑とエンジン
高温過熱を引き起こしてるのである。
For this reason, one side of the rotor creates frictional resistance with the side housing, and the other side space (inside the side seal) is filled with high-pressure gas blowing on the side seal, causing gas to flow inward. It is leaking, causing scum leakage and high temperature overheating of the engine.

従って出力ロス、エンジン高温過熱化となっている。This results in output loss and engine overheating.

(4)問題点を解決する手段 そこで本発明者は、ローター両側の側面空間同士のガス
圧力を均衡ずべく、ローター側部のサイドシール内方の
部位でローターを負り貫通孔を設け、この貫通孔により
サイドシール部内方の両側面空間部を連通させたロータ
リーエンジンを提供しようとしたのである。
(4) Means for solving the problem Therefore, in order to balance the gas pressure in the side spaces on both sides of the rotor, the inventor of the present invention provided a through hole in the rotor at a portion inside the side seal on the side of the rotor. The objective was to provide a rotary engine in which the spaces on both side surfaces inside the side seal portion were communicated through a through hole.

以下、本発明の一実施例を図面により説明する。An embodiment of the present invention will be described below with reference to the drawings.

本実施例ロータリーエンジンは、乗用車に搭載する20
−ター構成のロータリーエンジンのフロントまたは、リ
ア側の一方のハウジングで説明する。
The rotary engine of this example is installed in a passenger car.
This will be explained using either the front or rear housing of a rotary engine with a rotary engine configuration.

第1図は本発明ロータリーエンジンの軸方向に沿った断
面図、第2図はローターの側面が示しである。
FIG. 1 is a sectional view taken along the axial direction of the rotary engine of the present invention, and FIG. 2 is a side view of the rotor.

1はローター、2はローターハウジング、3はサイドハ
ウジング、4はインターナデエイトハウジング、5はサ
イドシールである。
1 is a rotor, 2 is a rotor housing, 3 is a side housing, 4 is an internal housing, and 5 is a side seal.

さて、本発明は、ローター1にその両側面に至る貫通孔
6を設けである。
Now, in the present invention, the rotor 1 is provided with through holes 6 extending to both sides thereof.

貫通孔6は、ローター1の重量バランスを考慮し、各頂
点部に近い部分に配分配置し、通常3個位い設けである
Considering the weight balance of the rotor 1, the through-holes 6 are distributed and arranged near each vertex, and there are usually about three through-holes.

もちろん、その配設位置は第2図に示すようにサイドシ
ール5.5の内方である。
Of course, its location is inside the side seal 5.5 as shown in FIG.

また、上記貫通孔6の断面径は、ガスの通気量を考慮し
て決めるが、φ5〜81が実験値からよい。
Further, the cross-sectional diameter of the through hole 6 is determined in consideration of the amount of gas permeation, but it is preferably φ5 to 81 based on experimental values.

(5発明の効果 ローター1とサイドハウジング3及びインターの・圧力
差が解消され、均衡する。
(5) Effects of the invention - The pressure difference between the rotor 1, side housing 3, and inter is eliminated and balanced.

このため、ローター1の両側にガス圧差が発生せず、ロ
ーター1が片寄りされることなく、両側のサイドシール
11及び11は、対面するサイドハウジング面16上を
同じ状態を保って摺動する。
Therefore, no gas pressure difference occurs on both sides of the rotor 1, the rotor 1 is not biased, and the side seals 11 and 11 on both sides slide in the same state on the opposing side housing surfaces 16. .

従って、高圧ガスのサイドシール11上を吹扱けてのロ
ーター1の内方への侵入がなく、ガス漏れ、エンジンの
am化が生じない。
Therefore, high-pressure gas is not blown onto the side seal 11 and intrudes into the rotor 1, so that gas leakage and am-change of the engine do not occur.

特に、ローター1の内方へのガス侵入が良好に阻止され
るため、エンジンの高温化を抑えることができるため、
従来困難とされたローターを多重に組込んだ30−ター
エンジン、40−ターエンジンに好都合である。
In particular, since gas intrusion into the rotor 1 is effectively prevented, the engine temperature can be suppressed.
This is convenient for 30-tar engines and 40-tar engines that incorporate multiple rotors, which has been considered difficult in the past.

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

第1図は本発明ロータリーエンジンの軸方向断面図、第
2図はローターの側面図である。
FIG. 1 is an axial sectional view of the rotary engine of the present invention, and FIG. 2 is a side view of the rotor.

Claims (1)

【特許請求の範囲】[Claims] ローターを挟んで、左右のサイドハウジング、インター
ナデエイトハウジングのそれぞれ開口した吸気ポイント
を備えた両サイド吸気のロータリーエンジンにおいて、
ローター側部のサイドシール内方の部位で、このロータ
ーを貫く貫通孔を設け、この貫通孔によりローター両側
面のサイドシールで囲まれた両側面空間部を互いに連通
させたロータリーエンジン。
In a rotary engine with intakes on both sides, the left and right side housings and the internal housing have intake points that open on both sides of the rotor.
A rotary engine in which a through hole is provided through the rotor at a portion inside the side seal on the side of the rotor, and this through hole allows the spaces on both sides of the rotor surrounded by the side seals on both sides of the rotor to communicate with each other.
JP13695989A 1988-12-24 1989-05-29 Rotary engine Pending JPH03901A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP13695989A JPH03901A (en) 1989-05-29 1989-05-29 Rotary engine
US07/448,100 US5121721A (en) 1988-12-24 1989-12-13 Rotary engine
CA002006457A CA2006457A1 (en) 1988-12-24 1989-12-21 Rotary engine
EP89313501A EP0376642A1 (en) 1988-12-24 1989-12-22 Rotary engine
US07/814,615 US5181489A (en) 1988-12-24 1991-12-30 Rotary engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13695989A JPH03901A (en) 1989-05-29 1989-05-29 Rotary engine

Publications (1)

Publication Number Publication Date
JPH03901A true JPH03901A (en) 1991-01-07

Family

ID=15187500

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13695989A Pending JPH03901A (en) 1988-12-24 1989-05-29 Rotary engine

Country Status (1)

Country Link
JP (1) JPH03901A (en)

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