JPH039290B2 - - Google Patents

Info

Publication number
JPH039290B2
JPH039290B2 JP57149556A JP14955682A JPH039290B2 JP H039290 B2 JPH039290 B2 JP H039290B2 JP 57149556 A JP57149556 A JP 57149556A JP 14955682 A JP14955682 A JP 14955682A JP H039290 B2 JPH039290 B2 JP H039290B2
Authority
JP
Japan
Prior art keywords
main body
scavenging
engine
air
fixed
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
JP57149556A
Other languages
Japanese (ja)
Other versions
JPS5939932A (en
Inventor
Hiroyasu Tanigawa
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to JP14955682A priority Critical patent/JPS5939932A/en
Publication of JPS5939932A publication Critical patent/JPS5939932A/en
Publication of JPH039290B2 publication Critical patent/JPH039290B2/ja
Granted legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B57/00Internal-combustion aspects of rotary engines in which the combusted gases displace one or more reciprocating pistons

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Description

【発明の詳細な説明】 「産業上の利用分野」 この発明は、回転往復するピストンにより機関
の本体を回転させる、2サイクル燃料噴射内燃機
関の改良に関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] This invention relates to an improvement in a two-stroke fuel injection internal combustion engine in which a main body of the engine is rotated by a piston that rotates and reciprocates.

「従来の技術」 この発明の発明者である出願人は、前記のよう
な2サイクル燃料噴射内燃機関として、「回転往
復ピストンを具備する燃料噴射内燃機関」(特願
昭57−2059)、及び「機関本体が回転する航空用
燃料噴射内燃機関」(特願昭57−4404)を既に開
示している。
``Prior Art'' The applicant, the inventor of this invention, has proposed a ``Fuel Injection Internal Combustion Engine Equipped with a Rotating Reciprocating Piston'' (Japanese Patent Application No. 57-2059) as a two-stroke fuel injection internal combustion engine as described above; ``Fuel injection internal combustion engine for aviation with a rotating engine body'' (Japanese Patent Application No. 57-4404) has already been disclosed.

両発明に共通する特徴は、高速回転する機関の
本体の空気を高速回転させるとともに、本体の回
転軸に対して内側から外側へ燃料を噴射して、燃
料に遠心力を与えて燃料を拡散させ、高速回転す
る空気との混合を著しく高めることにある。この
結果燃料噴霧の粒径を小さくして燃焼効率を向上
させることができる。
The common feature of both inventions is that the air in the main body of the engine rotates at high speed, and the fuel is injected from the inside to the outside of the rotating shaft of the main body, applying centrifugal force to the fuel and diffusing the fuel. , to significantly increase mixing with high-speed rotating air. As a result, the particle size of the fuel spray can be reduced and the combustion efficiency can be improved.

さらに、本体の回転により効果的な空気冷却が
可能である、排気を利用してタービンを構成でき
る、ピストンの回転往復運動を滑らかにできる、
クランク機構を不要とするのでコンパクトに構成
できる、などの特徴を有する。
In addition, the rotation of the main body allows for effective air cooling, the exhaust gas can be used to form a turbine, and the piston's reciprocating rotation can be made smoother.
It has features such as being able to be constructed compactly as it does not require a crank mechanism.

「発明が解決しようとする問題点」 ところで前記両発明では、左給気室へ連通する
左掃気穴と、右給気室へ連通する右掃気穴とをそ
れぞれ燃焼室に開口させる構成をとつていた。そ
して掃気時には、左給気室から左掃気穴を、又右
給気室から右掃気穴をそれぞれ通つて掃気を燃焼
室へ流入させていた。従つて燃焼室へ流入した掃
気は、互いに向き合つた状態になつていた。
"Problems to be Solved by the Invention" In both of the above inventions, the left scavenging hole communicating with the left air supply chamber and the right scavenging hole communicating with the right air supply chamber are each opened into the combustion chamber. was. During scavenging, the scavenging air was flowed into the combustion chamber from the left air supply chamber through the left scavenging hole, and from the right air supply chamber through the right scavenging hole. Therefore, the scavenging air flowing into the combustion chamber was in a state facing each other.

より燃焼効率の高い内燃機関を得るためには、
さらに掃気効率を高める必要があり、前記構成で
はこの要請に十分応えられないうらみがあつた。
In order to obtain an internal combustion engine with higher combustion efficiency,
Furthermore, there is a need to improve the scavenging efficiency, and there was a problem that the above configuration could not sufficiently meet this requirement.

「問題点を解決するための手段」 この発明は前記両発明に於ける掃気手段を改良
して、より掃気効率を高めることを目的とするも
のであつて、以下の構成を要旨とする。
"Means for Solving the Problems" This invention aims to improve the scavenging means in both of the above inventions to further increase the scavenging efficiency, and has the following configuration as a gist.

機関の本体を閉塞する給気室蓋とピストンとの
間にそれぞれ対向して形成される給気室を、掃気
時に連通させる掃気路を本体に設ける。
An air scavenging path is provided in the main body to communicate air supply chambers formed oppositely between an air supply chamber cover and a piston that close the main body of the engine during air scavenging.

又本体に、掃気路に連結して掃気時に燃焼室の
一端部側へ開口する複数の掃気穴を設ける。
The main body is also provided with a plurality of scavenging holes that are connected to the scavenging passage and open toward one end of the combustion chamber during scavenging.

そして各掃気穴を互いに連通させる連絡路を本
体に設ける。
A communication path is provided in the main body to communicate the scavenging holes with each other.

「作用」 掃気に際して、対向する給気室から送られた掃
気は掃気路へ流入する。掃気路へ流入した掃気
は、連絡路から掃気穴へ流入して燃焼室の一端部
側へ流入する。
"Operation" During scavenging, the scavenging air sent from the opposing air supply chambers flows into the scavenging path. The scavenging air that has entered the scavenging passage flows into the scavenging hole from the communication passage and flows into one end of the combustion chamber.

燃焼室内へ流入した掃気は同一方向であつて、
単流掃気を形成し、効率よく燃焼ガスを排気穴か
ら掃気する。
The scavenging air flowing into the combustion chamber is in the same direction,
Forms single flow scavenging air and efficiently scavenges combustion gas from the exhaust hole.

「実施例」 以下図示実施例に基づいて、この発明を詳細に
説明する。
"Embodiments" The present invention will be described in detail below based on illustrated embodiments.

1は固定軸で、第1図に示すように内部には冷
却兼用潤滑油通路2が設けられており、冷却兼用
潤滑油通路2は図外冷却兼用潤滑油ポンプへ接続
されている。又、第2図に示すように固定軸1の
内部には、図示しない燃料噴射ポンプへ接続され
る燃料通路3が設けられている。
Reference numeral 1 denotes a fixed shaft, and as shown in FIG. 1, a cooling and lubricating oil passage 2 is provided inside the shaft, and the cooling and lubricating oil passage 2 is connected to a cooling and lubricating oil pump (not shown). Further, as shown in FIG. 2, a fuel passage 3 is provided inside the fixed shaft 1, which is connected to a fuel injection pump (not shown).

4はこの発明の特徴の一とする燃料噴射弁であ
つて、固定軸1の半径方向へ複数個が配設されて
おり、前記燃料通路3が接続されている。この燃
料噴射弁4は、第3図に詳細に示す如く、固定軸
1に凹設した取付穴1′の底面に、ノズルニード
ル5が固定されている。6はノズルニードル5の
噴射圧調整部である。7は筒状のノズルボデイで
あり、ノズルニードル5に摺動自在に外嵌されて
いる。そして内周面上部の段差は、前記噴射圧調
整部6に当接する。8はノズルボデイ7の下部に
周設された鍔状のばね座8である。9は調整ナツ
トで、取付穴1′の上部に螺着されており、この
調整ナツト9とばね座8との間には、ばね10が
張設されている。従つて調整ナツト9を回転させ
ることにより、ノズルボデイ7を移動させ、噴射
圧調整部6へかかる荷重を調整して、ノズルニー
ドル5の燃料噴射圧を調整できるようになつてい
る。このように燃料噴射弁4を構成したことによ
つて、固定軸1の直径が小さくても複数の燃料噴
射弁4を配設することが可能になるうえ、燃料噴
射圧の微調整も固定軸1の外側から容易に行うこ
とができる。
A plurality of fuel injection valves 4 are arranged in the radial direction of the fixed shaft 1, and are connected to the fuel passage 3. As shown in detail in FIG. 3, this fuel injection valve 4 has a nozzle needle 5 fixed to the bottom surface of a mounting hole 1' formed in the fixed shaft 1. Reference numeral 6 denotes an injection pressure adjustment section of the nozzle needle 5. Reference numeral 7 denotes a cylindrical nozzle body, which is slidably fitted onto the nozzle needle 5. The step at the upper part of the inner circumferential surface comes into contact with the injection pressure adjusting section 6 . Reference numeral 8 denotes a flange-shaped spring seat 8 provided around the lower part of the nozzle body 7. Reference numeral 9 denotes an adjustment nut which is screwed into the upper part of the mounting hole 1', and a spring 10 is stretched between the adjustment nut 9 and the spring seat 8. Therefore, by rotating the adjustment nut 9, the nozzle body 7 is moved, the load applied to the injection pressure adjustment section 6 is adjusted, and the fuel injection pressure of the nozzle needle 5 can be adjusted. By configuring the fuel injection valve 4 in this way, it becomes possible to arrange a plurality of fuel injection valves 4 even if the diameter of the fixed shaft 1 is small, and fine adjustment of the fuel injection pressure is also possible using the fixed shaft. This can be easily done from the outside of 1.

11はピストンであつて、固定軸1に摺動自在
に対向して外嵌されていて、ピストン11間には
燃焼室12が形成される。
Reference numeral 11 denotes a piston, which is fitted onto the fixed shaft 1 so as to be able to slide freely, and a combustion chamber 12 is formed between the pistons 11.

13はピストンピンであり、各ピストン11か
ら半径方向へ2本が突設されている。ピストンピ
ン13には、後述する機関の本体16のピストン
案内穴17に転動自在に嵌めこまれる、本体側転
動輪14、及び曲溝筒25の曲溝26に転動自在
に嵌めこまれる曲溝側転勤輪15がそれぞれ取付
けられている。
Reference numeral 13 denotes piston pins, two of which protrude from each piston 11 in the radial direction. The piston pin 13 includes a body-side rolling ring 14 that is rotatably fitted into a piston guide hole 17 of a main body 16 of the engine, which will be described later, and a curved ring that is rotatably fitted into a curved groove 26 of a curved groove tube 25. A groove side transfer wheel 15 is attached to each.

16は機関の本体であり、それぞれ長軸方向の
ピストン案内穴17が対向して設けられている。
前記のようにこのピストン案内穴17には、ピス
トンピン13の本体側転動輪14が転動自在に嵌
めこまれる。
Reference numeral 16 denotes a main body of the engine, in which piston guide holes 17 in the longitudinal direction are provided facing each other.
As described above, the main body side rolling ring 14 of the piston pin 13 is fitted into the piston guide hole 17 so as to be freely rotatable.

次に、この発明の最も特徴とする掃気路18、
掃気穴19、連絡路20について説明する。
Next, the scavenging passage 18, which is the most characteristic feature of this invention,
The scavenging hole 19 and the communication path 20 will be explained.

18は複数の掃気路であつて、第1図、第4
図、第5図に示すように、ピストン11が掃気す
る位置にあるとき、本体16、対向するピストン
11、後記する給気室蓋30a,30bとの間に
形成される給気室32を互いに連通させるよう、
本体16に設けられている。19は本体16に設
けられた複数の掃気穴で、燃焼室12の一端側
(図面では左側)に開口する。又これら掃気穴1
9を連通させる環状の連絡路20が、本体16に
設けられている。
Reference numeral 18 indicates a plurality of scavenging passages, which are shown in FIGS. 1 and 4.
As shown in FIG. 5, when the piston 11 is in the scavenging position, the air supply chamber 32 formed between the main body 16, the opposing piston 11, and air supply chamber covers 30a and 30b (to be described later) is mutually moved. To communicate,
It is provided in the main body 16. Reference numeral 19 denotes a plurality of scavenging holes provided in the main body 16, which open at one end of the combustion chamber 12 (on the left side in the drawing). Also, these scavenging holes 1
An annular communication path 20 that communicates with the main body 16 is provided in the main body 16.

なお、21は複数の排気穴で、燃焼室12の他
端側(図面では右側)に開口し、本体に設けられ
た排気噴射口22に連通する。23は空気圧縮羽
根で、本体16のほぼ中央外周に放射状に配設さ
れている(第5図参照)。又24は、排気噴射口
22の外周に配設された動翼群である。
Note that 21 is a plurality of exhaust holes, which open at the other end of the combustion chamber 12 (on the right side in the drawing) and communicate with an exhaust injection port 22 provided in the main body. Reference numeral 23 denotes air compression vanes, which are arranged radially around the center of the main body 16 (see FIG. 5). Further, 24 is a group of rotor blades arranged around the outer periphery of the exhaust injection port 22.

25は曲溝筒で、本体16が回転自在に本体1
6に対向して外嵌されていて、内周面にはそれぞ
れ曲溝26が凹設されている。この曲溝26には
前記ピストンピン13の曲溝側転動輪15が嵌め
こまれている。この曲溝26は、ピストン11が
2往復する間に1回転するよう、ほぼサインカー
ブ状に形成されている。27は吸入口であつて、
それぞれ曲溝筒25の外端部に貫設されている。
28は吸入管である。
25 is a curved groove tube, and the main body 16 is rotatably attached to the main body 1.
6, and a curved groove 26 is formed in each inner peripheral surface. The curved groove side rolling ring 15 of the piston pin 13 is fitted into the curved groove 26 . This curved groove 26 is formed in a substantially sine curve shape so that the piston 11 rotates once during two reciprocations. 27 is an inlet port,
Each of them is provided through the outer end of the curved groove tube 25.
28 is a suction pipe.

29は静翼群であり、前記動翼24群の内側で
排気噴射口22の外側に配設されて、排気噴射口
22、静翼29、動翼24によつて、排気タービ
ンが構成される。
Reference numeral 29 denotes a stator blade group, which is disposed inside the rotor blade 24 group and outside the exhaust injection port 22, and an exhaust turbine is constituted by the exhaust injection port 22, the stator blade 29, and the rotor blade 24. .

30a,30bは給気室蓋で、本体16の両外
端部に固定され、かつ固定軸1に回転自在に対向
して外嵌されている。この給気室蓋30a,30
bには、それぞれ曲溝筒25に設けた吸入口27
に連通する給気口31が設けられている。そし
て、固定軸1、ピストン11、本体16、給気室
蓋30a,30bで形成される給気室32へ、給
気口31は開口する。この結果、本体16ととも
に回転する給気室蓋30a,30bの給気口31
と、固定された曲溝筒25の吸入口27とは回転
弁を形成することになる。
Reference numerals 30a and 30b denote air supply chamber covers, which are fixed to both outer ends of the main body 16 and are externally fitted to be rotatably opposed to the fixed shaft 1. These air supply chamber lids 30a, 30
b, an inlet 27 provided in each curved groove tube 25;
An air supply port 31 communicating with is provided. The air supply port 31 opens into an air supply chamber 32 formed by the fixed shaft 1, the piston 11, the main body 16, and the air supply chamber covers 30a and 30b. As a result, the air supply ports 31 of the air supply chamber covers 30a, 30b rotate together with the main body 16.
The intake port 27 of the fixed curved groove tube 25 forms a rotary valve.

なお、一方の給気室蓋30a(図面では左側)
には大歯車33が固定されている。又他方の給気
室蓋30bには動力軸34が設けられていて、動
力軸34には、図示しない始動用歯車を取付けて
おく。
In addition, one air supply chamber cover 30a (left side in the drawing)
A large gear 33 is fixed to. A power shaft 34 is provided on the other air supply chamber cover 30b, and a starting gear (not shown) is attached to the power shaft 34.

35は固定外筒であり、曲溝筒25の外側で曲
溝筒25に固定されている。36は空気案内羽根
で、本体16の空気圧縮羽根23の外側に、固定
外筒35に配設されている。37は排気噴射ノズ
ルである。38は空気濾過器で、回転する空気圧
縮羽根23によりこの空気濾過器38を通つた空
気は、空気圧縮羽根23、空気案内羽根36によ
り圧縮されて、図外過給機を経て又は直接吸入管
28へ送られる。即ち、空気圧縮羽根23、空気
案内羽根36は過給機を構成する。
35 is a fixed outer cylinder, which is fixed to the curved groove cylinder 25 on the outside of the curved groove cylinder 25. Reference numeral 36 denotes an air guide vane, which is disposed on the fixed outer cylinder 35 on the outside of the air compression vane 23 of the main body 16. 37 is an exhaust injection nozzle. 38 is an air filter, and the air passing through this air filter 38 by the rotating air compression vanes 23 is compressed by the air compression vanes 23 and the air guide vanes 36, and is then passed through a turbocharger (not shown) or directly into an intake pipe. Sent to 28. That is, the air compression vanes 23 and the air guide vanes 36 constitute a supercharger.

39は固定軸1と曲溝筒26を連結する固定板
であり、この固定板39には、前記大歯車33と
歯合する小歯車40が枢着されている。そして小
歯車40の歯車軸41は、図示しない燃料噴射ポ
ンプ、冷却兼用潤滑油ポンプなどの補機に連結さ
れている。これら大歯車33と小歯車40の歯車
比を2:1にしておけば、1爆発毎に小歯車40
は1回転する。なお、固定板39に固定外筒35
を固定することも可能である。
A fixed plate 39 connects the fixed shaft 1 and the curved tube 26, and a small gear 40 that meshes with the large gear 33 is pivotally mounted on the fixed plate 39. A gear shaft 41 of the small gear 40 is connected to auxiliary equipment such as a fuel injection pump and a cooling and lubricating oil pump (not shown). If the gear ratio of these large gears 33 and small gears 40 is set to 2:1, the small gears 40
rotates once. Note that the fixed outer cylinder 35 is attached to the fixed plate 39.
It is also possible to fix.

この発明の内燃機関の作動は、通常の2サイク
ル内燃機関と同様である。まず第2図のようにピ
ストン11が上死点付近にきたとき、燃料噴射弁
4を開いて燃料を噴射して爆発させる。ピストン
11が第1図のように下死点付近に近づくと、排
気穴21が開き排気を排気噴射口22から噴射す
る。このとき排気タービンを構成する静翼29
群、動翼24群により本体16の回転が助勢され
る。
The operation of the internal combustion engine of the present invention is similar to a conventional two-stroke internal combustion engine. First, when the piston 11 reaches near the top dead center as shown in FIG. 2, the fuel injection valve 4 is opened to inject fuel and cause an explosion. When the piston 11 approaches the bottom dead center as shown in FIG. 1, the exhaust hole 21 opens and exhaust gas is injected from the exhaust injection port 22. At this time, the stationary blade 29 that constitutes the exhaust turbine
The rotation of the main body 16 is assisted by the group of rotor blades 24.

次いで掃気穴19群が開いて、給気室32から
掃気路18、連絡路20を経て掃気が燃焼室12
へ供給されて圧縮行程へ移る。掃気穴19群から
供給される掃気は、同一方向であるため単流掃気
を形成するため、掃気効率が極めて高い。
Next, the group of scavenging holes 19 opens, and the scavenging air flows from the air supply chamber 32 through the scavenging passage 18 and the communication passage 20 to the combustion chamber 12.
is supplied to the compressor and moves to the compression stroke. Since the scavenging air supplied from the group of scavenging holes 19 flows in the same direction, a single flow of scavenging air is formed, so that the scavenging efficiency is extremely high.

「効果」 対向する給気室から燃焼室の一端部側へ掃気が
供給されて、掃気が単流掃気で行われるため、掃
気効率を高める効果が大きい。加えて掃気路の大
きな回転半径により空気の回転速度を大きくし、
掃気穴群でのその速度をさらに加速して燃焼室内
の空気回転速度を極限まで高めることにより、燃
料油粒に大きな遠心力を加えて理想の燃焼を得る
効果が大である。
"Effect" Scavenging air is supplied from the opposing air supply chambers to one end of the combustion chamber, and scavenging is performed in a single flow, which has a great effect on increasing scavenging efficiency. In addition, the large rotation radius of the scavenging passage increases the rotational speed of the air,
By further accelerating the speed at the scavenging hole group and increasing the air rotation speed within the combustion chamber to the maximum, it is highly effective to apply a large centrifugal force to the fuel oil particles and obtain ideal combustion.

即ち、機関本体を高速回転させ、単流掃気と
し、燃料噴射弁を設けた固定軸を回転中心に設け
ることにより、掃気の際、回転中心にできる排ガ
スの柱を除去した理想の単流掃気を得る効果が大
きく、高速回転する空気流の回転中心より外側へ
燃料を噴射することにより、燃料油粒に遠心力と
いう全く新しい力が加わり、油粒をポンプ圧と貫
通力と遠心力により拡散燃焼させる。この場合、
油粒は小さい程空気回転流に乗りやすく、燃焼し
ながら貫通力と遠心力とにより空気中を突進し、
理想の燃焼を得る効果が大きい。
In other words, by rotating the engine body at high speed, performing single-flow scavenging, and installing a fixed shaft with a fuel injection valve at the rotation center, ideal single-flow scavenging is achieved by eliminating the column of exhaust gas that forms at the rotation center during scavenging. By injecting fuel outward from the center of rotation of a high-speed rotating air stream, a completely new force called centrifugal force is applied to the fuel oil droplets, and the oil droplets are diffused and burned by pump pressure, penetration force, and centrifugal force. let in this case,
The smaller the oil droplets, the easier it is to ride the rotating air flow, and while burning, they rush through the air due to penetrating force and centrifugal force.
Great effect in obtaining ideal combustion.

又、機関本体を回転させ、単流掃気としたこと
により、排気タービンを片側に構成できるので熱
効率を高める効果が大きく、過給機を容易に構成
できる効果も大きい。
Furthermore, by rotating the engine body and using single-flow scavenging, the exhaust turbine can be configured on one side, which has a great effect of increasing thermal efficiency, and also has a great effect of making it possible to easily configure the supercharger.

燃料噴射弁の燃料噴射圧調整を、固定軸の外側
から調整ナツトにより行えるので、噴射圧の調整
を容易にできる効果があり、小径の固定軸に多数
の燃料噴射弁を配設できる効果も大きい。
The fuel injection pressure of the fuel injection valve can be adjusted from the outside of the fixed shaft using an adjustment nut, which has the effect of making it easy to adjust the injection pressure, and also has the great effect of allowing a large number of fuel injection valves to be arranged on a small diameter fixed shaft. .

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

第1図はピストンが下死点付近にある状態の水
平方向断面図、第2図はピストンが上死点付近に
ある状態の垂直方向断面図である。第3図は燃料
噴射弁の取付状態を示す固定軸の縦断面図、第4
図は掃気路、連絡路、掃気穴の連通状態を示す本
体の断面略図、第5図は過給機を形成する空気圧
縮羽根、空気案内羽根の配設状態を示す断面略図
である。 1……固定軸、4……燃料噴射弁、11……ピ
ストン、12……燃焼室、13……ピストンピ
ン、16……本体、18……掃気路、19……掃
気穴、20……連絡路、21……排気穴、22…
…排気噴射口、23……空気圧縮羽根、24……
動翼、25……曲溝筒、26……曲溝、29……
静翼、30a,30b……給気室蓋、32……給
気室、35……固定外筒、36……空気案内羽
根、39……固定板。
FIG. 1 is a horizontal sectional view of the piston in the vicinity of the bottom dead center, and FIG. 2 is a vertical sectional view of the piston in the vicinity of the top dead center. Figure 3 is a longitudinal sectional view of the fixed shaft showing the installation state of the fuel injection valve;
The figure is a schematic cross-sectional view of the main body showing the communication state of the scavenging passage, the communication passage, and the scavenging hole, and FIG. 5 is a schematic cross-sectional view showing the arrangement of the air compression vanes and air guide vanes forming the supercharger. DESCRIPTION OF SYMBOLS 1...Fixed shaft, 4...Fuel injection valve, 11...Piston, 12...Combustion chamber, 13...Piston pin, 16...Main body, 18...Scavenging air passage, 19...Scavenging hole, 20... Connection path, 21...Exhaust hole, 22...
...Exhaust injection port, 23...Air compression vane, 24...
Moving blade, 25...Curved groove cylinder, 26...Curved groove, 29...
Stationary blades, 30a, 30b...Air supply chamber lid, 32...Air supply chamber, 35...Fixed outer cylinder, 36...Air guide vanes, 39...Fixed plate.

Claims (1)

【特許請求の範囲】 1 固定軸に対向して摺動自在に外嵌したピスト
ンを機関の本体内に摺動自在に収容して、ピスト
ン間に燃焼室を形成し、本体が回転自在に本体に
対向して外嵌された曲溝筒の内周面にそれぞれ凹
設した曲溝に、ピストンからそれぞれ突設したピ
ストンピンを、本体に長軸方向に対向して設けた
案内穴を通して摺動自在に嵌め込むとともに、燃
焼室へ燃料を噴射する燃料噴射弁を固定軸に配設
し、本体に本体の回転を助勢させる排気を噴射す
る排気噴射口が配設されている2サイクルの機関
本体が回転する内燃機関に於いて、 本体を閉塞する給気室蓋とピストンとの間にそ
れぞれ対向して形成される給気室を掃気時に連通
させる掃気路と、掃気路に連通して掃気時に燃焼
室の一端部側へ開口する複数の掃気穴と、掃気穴
を互いに連通させる連絡路とを本体に設けたこと
を特徴とする機関本体が回転する内燃機関。 2 燃料噴射弁は、固定軸に凹設された収容穴の
底面に固定されたノズルニードルと、噴射圧調整
部に当接してノズルニードルに摺動自在に外嵌さ
れたノズルボデイと、ノズルボデイに周設された
ばね座と収容穴に螺着された調整ナツトとの間に
張設されたばねとからなる特許請求の範囲第1項
記載の機関本体が回転する内燃機関。 3 固定軸は曲溝筒を固定する固定外筒を有しし
ており、本体は外周に空気圧縮羽根を配設されて
いて、固定外筒には空気圧縮羽根の外側に空気案
内羽根が配設されている特許請求の範囲第1項又
は第2項記載の機関本体が回転する内燃機関。 4 排気噴射口には曲溝筒に固定された静翼と、
静翼の外側には本体に固定された動翼とが配設さ
れている特許請求の範囲第1項ないし第3項記載
の機関本体が回転する内燃機関。 5 給気室蓋には大歯車が固定され、固定軸と固
定外筒とを連結する固定板には大歯車と歯合する
小歯車が枢着されている特許請求の範囲第1項な
いし第4項記載の機関本体が回転する内燃機関。 6 曲溝筒には吸入口が設けられており、給気室
蓋には吸入口と連通し給気室に開口する給気口が
設けられている特許請求の範囲第1項ないし第5
項記載の機関本体が回転する内燃機関。
[Scope of Claims] 1. A piston that is slidably fitted on the outside facing a fixed shaft is slidably housed in the main body of the engine, a combustion chamber is formed between the pistons, and the main body is rotatably inserted into the main body. The piston pins, which protrude from the piston, slide into curved grooves formed on the inner circumferential surface of the curved tube fitted externally facing the piston, through guide holes formed in the main body facing each other in the longitudinal direction. A 2-cycle engine body that can be fitted freely and has a fuel injection valve on a fixed shaft that injects fuel into the combustion chamber, and an exhaust injection port that injects exhaust gas to assist the rotation of the main body. In an internal combustion engine in which the engine rotates, there is a scavenging air passage that connects the air intake chambers formed opposite to each other between the air intake chamber cover that closes the main body and the piston during scavenging, and a scavenging air passage that communicates with the scavenging air passage and connects the air intake chambers that are formed facing each other during scavenging. 1. An internal combustion engine with a rotating engine body, characterized in that the main body is provided with a plurality of scavenging holes that open toward one end of a combustion chamber, and a communication path that communicates the scavenging holes with each other. 2. A fuel injection valve consists of a nozzle needle fixed to the bottom of a housing hole formed in a fixed shaft, a nozzle body that is slidably fitted onto the nozzle needle in contact with an injection pressure adjustment section, and a nozzle body that is fitted around the nozzle body. An internal combustion engine in which an engine main body rotates according to claim 1, comprising a spring tensioned between a spring seat provided therein and an adjustment nut screwed into a housing hole. 3 The fixed shaft has a fixed outer cylinder that fixes the curved groove cylinder, and the main body has air compression vanes arranged on the outer periphery, and the fixed outer cylinder has air guide vanes arranged on the outside of the air compression vanes. An internal combustion engine in which the engine body according to claim 1 or 2 rotates. 4 The exhaust injection port has a stator blade fixed to a curved groove tube,
4. An internal combustion engine in which the engine main body rotates according to claim 1, wherein a moving blade fixed to the main body is disposed outside the stationary blade. 5. Claims 1 to 5, wherein a large gear is fixed to the air supply chamber cover, and a small gear that meshes with the large gear is pivotally mounted to the fixed plate that connects the fixed shaft and the fixed outer cylinder. An internal combustion engine in which the engine body according to item 4 rotates. 6. Claims 1 to 5, wherein the curved groove cylinder is provided with an intake port, and the air supply chamber lid is provided with an air supply port that communicates with the intake port and opens into the air supply chamber.
An internal combustion engine in which the engine body as described in paragraph 2 rotates.
JP14955682A 1982-08-28 1982-08-28 Rotary reciprocal piston type internal-combustion engine Granted JPS5939932A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14955682A JPS5939932A (en) 1982-08-28 1982-08-28 Rotary reciprocal piston type internal-combustion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14955682A JPS5939932A (en) 1982-08-28 1982-08-28 Rotary reciprocal piston type internal-combustion engine

Publications (2)

Publication Number Publication Date
JPS5939932A JPS5939932A (en) 1984-03-05
JPH039290B2 true JPH039290B2 (en) 1991-02-08

Family

ID=15477744

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14955682A Granted JPS5939932A (en) 1982-08-28 1982-08-28 Rotary reciprocal piston type internal-combustion engine

Country Status (1)

Country Link
JP (1) JPS5939932A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH03229901A (en) * 1990-02-02 1991-10-11 Hiroyasu Tanigawa Fuel injection internal combustion engine of which engine main body itself rotates
JPH0693874A (en) * 1991-10-07 1994-04-05 Hiroyasu Tanigawa Three-combustion-chamber engine with main body rotating

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4929964A (en) * 1972-07-19 1974-03-16

Also Published As

Publication number Publication date
JPS5939932A (en) 1984-03-05

Similar Documents

Publication Publication Date Title
US9719469B1 (en) Turbo-piston engine
CN1908389B (en) Small four-stroke internal combustion engine
US6223775B1 (en) Accumulator
JP3016485B2 (en) Reciprocating 2-cycle internal combustion engine without crank
KR20040031074A (en) Reciprocating piston engine comprising a rotative cylinder
US4362132A (en) Two-cycle engine
US3945348A (en) Two-chamber, two-stroke rocking piston internal combustion engine
US4060060A (en) Valving system for compressors, engines and the like
CN108350795B (en) Supercharged internal combustion engine
US5365892A (en) Rotary internal combustion engine
US4974556A (en) Internal combustion engine
JP5478741B2 (en) Low fuel consumption, low emission 2-stroke engine
CN1063921A (en) The improvement of reciprocating internal combustion engines of two-stroke type
US4136646A (en) Two cycle rotary internal combustion engine
JPS598648B2 (en) Taikou Piston Gatadoriyokukikan
US6021746A (en) arc-piston engine
US5794573A (en) Internal combustion engine
US7398759B2 (en) Four-stroke engine
US3590791A (en) Internal combustion engine and fuel injection system therefor
US4834032A (en) Two-stroke cycle engine and pump having three-stroke cycle effect
US3550568A (en) Opposing piston engine
US6095783A (en) Fluid mover
US3450121A (en) Internal-combustion engine and fuel injection system therefor
CN2413031Y (en) Energy-soving compound diesel and gasoline internal combustion engine
GB2288637A (en) Two-stroke engine piston containing a valve