JPH0395034U - - Google Patents

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Publication number
JPH0395034U
JPH0395034U JP248690U JP248690U JPH0395034U JP H0395034 U JPH0395034 U JP H0395034U JP 248690 U JP248690 U JP 248690U JP 248690 U JP248690 U JP 248690U JP H0395034 U JPH0395034 U JP H0395034U
Authority
JP
Japan
Prior art keywords
exhaust
expansion
air supply
housing
passage
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
JP248690U
Other languages
Japanese (ja)
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 filed Critical
Priority to JP248690U priority Critical patent/JPH0395034U/ja
Publication of JPH0395034U publication Critical patent/JPH0395034U/ja
Pending legal-status Critical Current

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Description

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

第1図Aは、本考案にかかわる好適な実施例の
基本構造を示す分解斜視図、第1図Bは、その要
部断面図、第2図Aは、本考案にかかわる好適な
実施例の吸気行程を説明するために第1図Bの
−線に沿つて示した断面図、第2図Bは、同じ
く送気行程を説明するために第1図Bの−線
に沿つて示した断面図、第3図Aは、本考案にか
かわる好適な実施例の膨脹排気行程を説明するた
めに第1図Bの−線に沿つて示した断面図、
第3図Bは、同じく膨脹排気および掃気行程を説
明するために第1図Bの−線に沿つて示した
断面図、第3図Cは、同じく膨脹排気および圧縮
行程を説明するために第1図Bの−線に沿つ
て示した断面図である。 1……吸送気ハウジング、2……気密圧縮ハウ
ジング、3……膨排気ハウジング、4……圧縮室
、5……主軸、6……点火手段、10……吸送気
本体、12……吸送気ロータ、14……外プレー
ト、16……ベアリング、30……膨排気本体、
32……膨排気ロータ、34……外プレート、3
6……ベアリング、4−1……送出通路、4−2
……送気通路、4−3……送入通路、4−4……
送気凹部、100……中空部、102……吸気孔
、104……吸送気室、106……送気区、10
7……吸気区、120……ロータ本体、122…
…ベーン、123……ベーン、200……中空部
、300……中空部、302……排気孔、304
……膨排気室、306……膨脹区、307……排
気区、320……ロータ本体、322……ベーン
、323……ベーン、A……吸気開始点、B……
圧縮開始点、C……最高圧縮点、D……圧縮終了
点、E……膨脹開始点、F……膨脹終了点、H…
…排気終了点、D……圧縮終了点、K……吸送気
ロータのベーン位置。
FIG. 1A is an exploded perspective view showing the basic structure of a preferred embodiment of the present invention, FIG. 1B is a sectional view of the main part thereof, and FIG. 2A is a diagram of the preferred embodiment of the present invention. 1B is a sectional view taken along the - line in FIG. 1B to explain the intake stroke, and FIG. 2B is a sectional view taken along the - line in FIG. 1B to also explain the air supply stroke. Figure 3A is a sectional view taken along the - line in Figure 1B to explain the expansion and exhaust stroke of a preferred embodiment of the present invention;
FIG. 3B is a sectional view taken along the - line in FIG. 1B to similarly explain the expansion exhaust and scavenging strokes, and FIG. FIG. 1 is a sectional view taken along the - line in FIG. 1B. DESCRIPTION OF SYMBOLS 1... Suction air housing, 2... Airtight compression housing, 3... Expansion and exhaust housing, 4... Compression chamber, 5... Main shaft, 6... Ignition means, 10... Suction air main body, 12... Suction air rotor, 14...outer plate, 16...bearing, 30...expansion/exhaust main body,
32... Expansion and exhaust rotor, 34... Outer plate, 3
6... Bearing, 4-1... Delivery passage, 4-2
...Air supply passage, 4-3...Intake passage, 4-4...
Air supply recess, 100... Hollow part, 102... Intake hole, 104... Air intake chamber, 106... Air supply section, 10
7...Intake section, 120...Rotor body, 122...
... Vane, 123 ... Vane, 200 ... Hollow part, 300 ... Hollow part, 302 ... Exhaust hole, 304
...Expansion and exhaust chamber, 306...Expansion section, 307...Exhaust section, 320...Rotor body, 322...Vane, 323...Vane, A...Intake start point, B...
Compression start point, C... Maximum compression point, D... Compression end point, E... Expansion start point, F... Expansion end point, H...
...Exhaust end point, D...Compression end point, K...Vane position of the suction air rotor.

Claims (1)

【実用新案登録請求の範囲】 (1) ベーンを有する吸送気ロータを中空内部へ
回転自在に軸装するとともに、吸送気室および液
体燃料と空気等との混合ガスを吸入する吸気孔お
よび混合ガスを送出する送出通路を備える吸送気
ハウジングと、 ベーンならびに送気凹部を有する膨排気ロータ
を中空内部へ回転自在に軸装するとともに、膨排
気室および混合ガスを導入する送入通路および燃
焼ずみの排気ガスの排気孔を備える膨排気ハウジ
ングと、 前記吸送気ハウジングと膨排気ハウジングとの
間に固設されて、吸送気ハウジングの前記送出通
路および膨排気ハウジングの前記送入通路を連通
する送気通路のみを開口した気密圧縮ハウジング
と、 前記送出通路、送気通路、送入通路および送気
凹部を備える圧縮室と、 前記気密圧縮ハウジングを気密に貫通し、前記
吸送気ハウジングおよび膨排気ハウジングによつ
て軸支されるとともに、前記吸送気ロータおよび
膨排気ロータを一体回転するように所定位置にお
いて固着した主軸と、 前記圧縮室の送気凹部に対して設けた点火手段
とから構成される内燃機関であつて、 前記吸送気ハウジングが、2枚1組みのベーン
を吸送気ロータの一直径に沿つて外方向へ突出す
るように弾装するとともに、前記吸送気室が前記
吸気孔から送入通路までの範囲を拡径して形成さ
れ、その他は吸送気ロータの直径にほぼ等しい内
径を有しており、 前記膨排気ハウジングが、2枚1組のベーンを
膨排気ロータの一直径に沿つて外方向へ突出する
ように弾装するとともに、前記膨排気室が前記点
火手段近くに設けられた膨脹開始点から前記排気
孔までの範囲を拡径して形成され、その他は膨排
気ロータの直径にほぼ等しい内径を有しているも
のにおいて、 前記吸送気ロータの一ベーンが最高圧縮点に到
達した直後、前記圧縮室の送気凹部が送入通路か
ら隔絶されると同時に、前記膨排気ロータの一ベ
ーンが前記膨脹開始点に到達し、かつ点火手段に
より前記送気凹部にある圧縮された混合ガスに対
して着火が行われるように構成したロータリーエ
ンジンの基本構造。 (2) 上記送気凹部が、膨排気ロータの2ベーン
間の2円周面において、各円周面に沿つて適当な
長さの断面形状を備えて、各送気凹部の前端が上
記送入通路にさしかかつた時に送気凹部の後端が
排気孔にとどまり、圧縮された混合ガスで送気凹
部に残留した排気ガスを掃気するように形成した
請求項1記載のロータリーエンジンの基本構造。 (3) 上記送入通路が、排気孔寄りに掃気用切欠
きを形成した請求項2記載のロータリーエンジン
の基本構造。 (4) 上記圧縮室が、上記送出通路、送気通路、
送入通路および送気凹部の総容積を調整して好適
な圧縮比を設定することを特徴とする請求項1記
載のロータリーエンジンの基本構造。
[Scope of Claim for Utility Model Registration] (1) A suction air rotor having vanes is rotatably mounted in a hollow interior, and a suction air chamber and an intake hole for sucking a mixed gas of liquid fuel, air, etc. An intake air housing including a delivery passage for sending out a mixed gas; an expansion/exhaust rotor having vanes and an air supply recess rotatably mounted in the hollow interior; an intake passage for introducing an expansion/exhaust chamber and the mixed gas; an expansion/exhaust housing having an exhaust hole for combusted exhaust gas; and an expansion/exhaust housing fixedly installed between the intake air housing and the expansion/exhaust housing, the delivery passage of the intake air housing and the inlet passage of the expansion/exhaust housing. an airtight compression housing in which only an air supply passage communicating with the intake air is opened; a compression chamber including the delivery passage, an air supply passage, an intake passage, and an air supply recess; a main shaft that is pivotally supported by a housing and an expansion/exhaust housing and is fixed at a predetermined position so as to integrally rotate the intake air rotor and the expansion/exhaust rotor; and an ignition provided for the air supply recess of the compression chamber. an internal combustion engine comprising means, the intake air housing elastically mounting a set of two vanes so as to protrude outward along one diameter of the intake air rotor; The air supply chamber is formed by expanding the diameter of the range from the intake hole to the intake passage, and the rest has an inner diameter approximately equal to the diameter of the intake air rotor, and the expansion and exhaust housing is a set of two pieces. The vanes of the expansion/exhaust rotor are mounted so as to protrude outward along one diameter of the expansion/exhaust rotor, and the expansion/exhaust chamber is expanded in diameter from an expansion start point provided near the ignition means to the exhaust hole. Immediately after one vane of the intake air rotor reaches the maximum compression point, the air supply recess of the compression chamber is The vane of the expansion and exhaust rotor reaches the expansion start point at the same time as being isolated from the inlet passage, and the ignition means ignites the compressed mixed gas in the air supply recess. The basic structure of a rotary engine. (2) The air supply recess has a cross-sectional shape of an appropriate length along each circumferential surface on the two circumferential surfaces between the two vanes of the expansion/exhaust rotor, and the front end of each air supply recess is The basics of the rotary engine according to claim 1, wherein the rear end of the air supply recess remains in the exhaust hole when the engine approaches the entrance passage, and the exhaust gas remaining in the air supply recess is scavenged with the compressed mixed gas. structure. (3) The basic structure of a rotary engine according to claim 2, wherein the inlet passage has a scavenging notch near the exhaust hole. (4) The compression chamber includes the delivery passage, the air supply passage,
2. The basic structure of a rotary engine according to claim 1, wherein a suitable compression ratio is set by adjusting the total volume of the inlet passage and the air inlet recess.
JP248690U 1990-01-16 1990-01-16 Pending JPH0395034U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP248690U JPH0395034U (en) 1990-01-16 1990-01-16

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP248690U JPH0395034U (en) 1990-01-16 1990-01-16

Publications (1)

Publication Number Publication Date
JPH0395034U true JPH0395034U (en) 1991-09-27

Family

ID=31506359

Family Applications (1)

Application Number Title Priority Date Filing Date
JP248690U Pending JPH0395034U (en) 1990-01-16 1990-01-16

Country Status (1)

Country Link
JP (1) JPH0395034U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008077032A1 (en) * 2006-12-19 2008-06-26 Gerber Engineering Incorporated Rotary engine with cylinders of different design and volume

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2008077032A1 (en) * 2006-12-19 2008-06-26 Gerber Engineering Incorporated Rotary engine with cylinders of different design and volume

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