JP2003269189A - Prime mover - Google Patents

Prime mover

Info

Publication number
JP2003269189A
JP2003269189A JP2002064804A JP2002064804A JP2003269189A JP 2003269189 A JP2003269189 A JP 2003269189A JP 2002064804 A JP2002064804 A JP 2002064804A JP 2002064804 A JP2002064804 A JP 2002064804A JP 2003269189 A JP2003269189 A JP 2003269189A
Authority
JP
Japan
Prior art keywords
hollow
air
combustion chamber
rotary shaft
fuel
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.)
Granted
Application number
JP2002064804A
Other languages
Japanese (ja)
Other versions
JP3837601B2 (en
Inventor
Ichiro Yoshinaga
一郎 吉永
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 JP2002064804A priority Critical patent/JP3837601B2/en
Publication of JP2003269189A publication Critical patent/JP2003269189A/en
Application granted granted Critical
Publication of JP3837601B2 publication Critical patent/JP3837601B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Pre-Mixing And Non-Premixing Gas Burner (AREA)

Abstract

<P>PROBLEM TO BE SOLVED: To provide a prime mover having a simple structure, and capable of efficiently and surely obtaining large rotational motive power. <P>SOLUTION: This prime mover 10 comprises a hollow rotary shaft 12 for rotatably journaling both sides, a hollow cylindrical body 16 penetratingly fixed to the hollow rotary shaft 12, and having inside a combustion chamber 14 for communicating with a hollow part of the hollow rotary shaft 12, a blowout nozzle 18 arranged by turning a blowout port 48 in the rotational circumferential tangent direction of the hollow cylindrical body 16, an air-fuel supply means 20 for supplying fuel and air in the combustion chamber 14, and an ignition means 22 for arranging an ignition point 44 in the combustion chamber 14. The fuel and the air are supplied to the combustion chamber 14 via the hollow part 36 of the hollow rotary shaft 12. The fuel is ignited in the combustion chamber 14 of the hollow cylindrical body 16. The rotational motive power is obtained by rotating the hollow cylindrical body 16 by blowout reaction from the blowout nozzle 18 of the combustion expanding air T. <P>COPYRIGHT: (C)2003,JPO

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【発明の属する技術分野】本発明は、燃焼膨張空気を回
転の接線方向に噴出させてその噴出反力で回転動力を得
る原動装置に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a prime mover for injecting combustion-expanded air in a tangential direction of rotation to obtain rotational power by the ejection reaction force.

【0002】[0002]

【従来の技術】従来、例えば、ガソリン機関、ディーゼ
ル機関、ガスタービンまたはジェット機関等を含む原動
機が広く利用されている。例えば、円周方向に燃焼ガス
等を噴射させることによって回転動力を得る原動機に関
しても様々な発明がなされており、例えば、特開昭61
−241402号公報や特開昭50−100448号公
報に開示されている。
2. Description of the Related Art Conventionally, a prime mover including, for example, a gasoline engine, a diesel engine, a gas turbine or a jet engine has been widely used. For example, various inventions have been made with respect to a prime mover that obtains rotary power by injecting combustion gas or the like in the circumferential direction.
No. 241402 and Japanese Unexamined Patent Publication No. 50-100448.

【0003】[0003]

【発明が解決しようとする課題】特開昭61−2414
02号公報では、図5に示すように、燃焼ガスGをロー
ター100の回転中心部の回転パイプ102から流入
し、ローター100に取付けられた噴射口104を円周
方向に向けたノズル106から燃焼ガスを円周方向に噴
射して回転動力を得る噴射式原動機が開示されている。
しかしながら、この原動機では、別の場所で発生させた
燃焼ガスGが回転パイプ102を通り、ローター内部の
配管108を通ってノズル106へと単に通りぬけてい
くだけに過ぎず、原動機内でエネルギー発生がないので
大きな回転動力を得ることができなかった。また、燃焼
ガスを発生させるための燃焼室を別途に設けなければな
らないので、装置が大きなものとなり製造コストも高い
という問題があった。
Problems to be Solved by the Invention JP-A-61-2414
In JP-A-02 No. 02, as shown in FIG. 5, combustion gas G flows from a rotary pipe 102 at the center of rotation of a rotor 100, and an injection port 104 attached to the rotor 100 burns from a nozzle 106 oriented in the circumferential direction. An injection type prime mover for injecting gas in a circumferential direction to obtain rotational power is disclosed.
However, in this prime mover, the combustion gas G generated at another place simply passes through the rotary pipe 102, the pipe 108 inside the rotor and the nozzle 106, and energy is generated inside the prime mover. I couldn't get a lot of rotation power because there wasn't one. Further, since a combustion chamber for generating combustion gas has to be separately provided, there is a problem that the device becomes large and the manufacturing cost is high.

【0004】また、図6は、特開昭50−100448
号公報の蒸気タービン併用噴射式ロータリー原動機を示
している。図6(a)、図6(b)に示すように、この
原動機の噴射式ロータリー原動機部分200は、回転主
軸202から略十字放射状に4つの棹204が設けられ
ており、その棹204の回転外側先端の各々に燃焼室2
08が固定され、さらに棹204内部の燃料補給路20
6a及び空気補給路206bを介して燃焼室に燃料及び
空気を圧送する構成であり、燃焼ガスを側壁209に向
けて噴射して燃焼室208を周回転させて主軸202か
ら回転動力を得るものである。しかしながら、この噴射
式ロータリー原動機200では、放射状の棹204の中
空内部に燃料補給路206aと空気補給路206bを設
けるために各々の棹内部を2つに仕切って形成されてい
るので構造が複雑なものであった。さらに、燃料に着火
させるために4つの燃焼室208の空気混合燃料の噴射
口外側に点火プラグ211が設置されているので、構造
が複雑であるとともに製造コストが高いものであった。
また、点火プラグ211は、燃焼室208の噴射口付近
の外側部分に取付けられているので、実際には、燃焼室
外部で燃料が燃焼することとなり、燃焼ガスの膨張エネ
ルギーは燃焼室を周回転させる力として利用できないも
のであった。よって、棹内部を圧送されてくる燃焼する
前の燃料及び空気が燃焼室から噴射する際の噴射反力に
よる小さな回転動力しか得ることができないので、噴射
式ロータリー原動機単独では非常に効率が悪く実用性が
ないものであった。したがって、図6(b)に示すよう
に、有効な回転動力を取り出すために燃焼熱を利用した
蒸気タービン210等を補助的に設けなければならず、
羽根体212や蒸気ボイラー214、高圧蒸気パイプ2
16等の設備のために構造がより複雑となり装置全体も
大きくなって製造コストが高いものであった。
Further, FIG. 6 is a diagram of Japanese Patent Application Laid-Open No. 50-100448.
1 shows a steam turbine combined injection-type rotary prime mover disclosed in Japanese Patent Publication No. JP-A-2003-242242. As shown in FIGS. 6 (a) and 6 (b), the injection type rotary prime mover part 200 of this prime mover is provided with four rods 204 in a substantially cross-radial shape from a rotary main shaft 202, and rotation of the rod 204. Combustion chamber 2 on each of the outer tips
08 is fixed, and the fuel supply path 20 inside the rod 204 is further fixed.
Fuel and air are pressure-fed to the combustion chamber via the 6a and the air supply passage 206b, and the combustion gas is injected toward the side wall 209 to rotate the combustion chamber 208 to obtain rotational power from the main shaft 202. is there. However, in this injection type rotary prime mover 200, since the fuel replenishing passage 206a and the air replenishing passage 206b are provided in the hollow inside of the radial rod 204, the inside of each rod is divided into two, so that the structure is complicated. It was a thing. Further, since the ignition plugs 211 are installed outside the air-mixed fuel injection ports of the four combustion chambers 208 to ignite the fuel, the structure is complicated and the manufacturing cost is high.
Further, since the spark plug 211 is attached to the outer portion of the combustion chamber 208 near the injection port, the fuel actually burns outside the combustion chamber, and the expansion energy of the combustion gas rotates around the combustion chamber. It was something that could not be used as a force to cause it. Therefore, since only small rotational power can be obtained by the injection reaction force when the fuel and air before combustion that are pumped inside the rod are injected from the combustion chamber, the injection-type rotary prime mover alone is very inefficient and practical. There was no nature. Therefore, as shown in FIG. 6B, a steam turbine 210 or the like using combustion heat must be provided as an auxiliary in order to take out effective rotational power,
Impeller 212, steam boiler 214, high-pressure steam pipe 2
Due to the equipment of 16 or the like, the structure was more complicated, the entire apparatus was large, and the manufacturing cost was high.

【0005】本発明は上記課題に鑑みてなされたもので
あり、その目的は、構造が簡単で装置全体がコンパクト
であり、しかも効率良く確実に大きな回転動力を得るこ
とができる原動装置を提供することにある。
The present invention has been made in view of the above problems, and an object thereof is to provide a prime mover which has a simple structure and is compact in size as a whole and which can efficiently and reliably obtain a large rotational power. Especially.

【0006】[0006]

【課題を解決するための手段】上記課題を解決するため
に本発明の原動装置は、両側を回転自在に軸支された内
部が中空の中空回転軸12と、中空回転軸12に貫通状
に固定され中空回転軸12の中空部36に連通する燃焼
室14を内部に有して該中空回転軸12と一体回転する
中空筒体16と、中空筒体16の回転周面Rから突設さ
れ中空筒体16内の燃焼室と連通し回転円周接線方向に
その噴出口48を向けて設けられた噴出ノズル18と、
中空回転軸12の中空部36を含み、中空筒体16内の
燃焼室14内へ燃料及び空気を供給する空気・燃料供給
手段20と、燃焼室14内に点火点44を配置させて燃
焼室14内の燃料に自在に点火させる点火手段22と、
を有し、中空筒体16の燃焼室14内で点火させてその
燃焼膨張空気Tの噴出ノズル18からの噴出反力で中空
筒体16を回転させて回転動力を得ることを特徴とする
原動装置10から構成される。
In order to solve the above-mentioned problems, a prime mover of the present invention has a hollow rotary shaft 12 which is rotatably supported on both sides and has a hollow interior, and a hollow rotary shaft 12 which penetrates the hollow rotary shaft 12. A hollow cylindrical body 16 that has a combustion chamber 14 that is fixed and communicates with a hollow portion 36 of the hollow rotating shaft 12 and that rotates integrally with the hollow rotating shaft 12, and that is provided so as to project from the rotation peripheral surface R of the hollow cylindrical body 16. An ejection nozzle 18 which is in communication with the combustion chamber in the hollow cylindrical body 16 and is provided with its ejection port 48 directed in the tangential direction of the rotational circumference,
An air / fuel supply means 20 for supplying fuel and air into the combustion chamber 14 in the hollow cylindrical body 16 including the hollow portion 36 of the hollow rotary shaft 12 and an ignition point 44 arranged in the combustion chamber 14 to form the combustion chamber. Ignition means 22 for freely igniting the fuel in 14;
A prime mover characterized in that the hollow cylindrical body 16 is ignited in the combustion chamber 14 of the hollow cylindrical body 16 and the hollow cylindrical body 16 is rotated by the ejection reaction force of the combustion expansion air T from the ejection nozzle 18 to obtain rotational power. It is composed of the device 10.

【0007】また、点火手段22の点火点44が燃焼室
14内の中空回転軸16の取り付け位置に近接して配置
されたこととしてもよい。
Further, the ignition point 44 of the ignition means 22 may be arranged close to the mounting position of the hollow rotary shaft 16 in the combustion chamber 14.

【0008】また、空気・燃料供給手段20は、中空回
転軸12の中空内部36を空気供給路として外部から空
気を圧送する空気供給手段50と、中空回転軸12の中
空部36の略中心位置で空気供給手段50による空気と
混合するように燃料を供給する燃料供給手段52と、を
備えたこととしてもよい。
The air / fuel supply means 20 includes an air supply means 50 for pumping air from the outside using the hollow interior 36 of the hollow rotary shaft 12 as an air supply path, and a substantially central position of the hollow portion 36 of the hollow rotary shaft 12. The fuel supply means 52 for supplying the fuel so as to be mixed with the air by the air supply means 50.

【0009】また、燃料供給手段52は、中空筒体16
内部の軸方向の略中心位置にその供給口68が設定され
ていることとしてもよい。
The fuel supply means 52 is a hollow cylinder 16
The supply port 68 may be set at a substantially central position inside in the axial direction.

【0010】また、中空筒体16は中空回転軸12に貫
通された状態で固定され、中空筒体16内となる中空回
転軸12に設けられた複数の連通孔38を介して燃焼室
14と中空回転軸12の中空部36が仕切られた状態で
相互に連通されたこととしてもよい。
The hollow cylindrical body 16 is fixed in a state of penetrating the hollow rotating shaft 12, and is connected to the combustion chamber 14 via a plurality of communication holes 38 provided in the hollow rotating shaft 12 inside the hollow cylindrical body 16. The hollow portions 36 of the hollow rotary shaft 12 may be communicated with each other in a partitioned state.

【0011】また、燃料供給手段52は、中空回転軸1
2の中心部を挿通され同中空回転軸12の長手方向に延
長されて外部の燃料供給源(60)に接続されるニード
ルパイプ状の燃料供給路62を含むこととしてもよい。
Further, the fuel supply means 52 is the hollow rotary shaft 1
It is also possible to include a needle pipe-shaped fuel supply passage 62 that is inserted through the central portion of the second rotary shaft 12 and extends in the longitudinal direction of the hollow rotary shaft 12 and is connected to an external fuel supply source (60).

【0012】また、点火手段22は、点火点44に配置
された放電子74を含む放電装置70からなることとし
てもよい。
Further, the ignition means 22 may be composed of a discharge device 70 including a discharge element 74 arranged at the ignition point 44.

【0013】[0013]

【発明の実施の形態】以下、添付図面を参照しつつ本発
明の実施の形態について説明する。図1ないし図3は、
本発明の原動装置の実施の形態を示しており、本発明の
原動装置は、両側を軸支された中空回転軸に固定された
中空の回転筒体内部で燃焼させて、燃焼膨張空気を回転
筒体の回転周面接線方向に噴出し、その噴出反力で回転
筒体を回転させて回転動力を得る原動装置である。
BEST MODE FOR CARRYING OUT THE INVENTION Embodiments of the present invention will be described below with reference to the accompanying drawings. 1 to 3 are
1 shows an embodiment of a prime mover of the present invention, in which a prime mover of the present invention is burned inside a hollow rotary cylinder fixed to a hollow rotary shaft whose both sides are supported to rotate combustion expanded air. This is a prime mover that ejects in the tangential direction of the rotation peripheral surface of the tubular body and rotates the rotary tubular body by the ejection reaction force to obtain rotational power.

【0014】図1に示すように、この実施形態に係る原
動装置10は、内部が中空の中空回転軸12と、中空内
部を燃焼室14とした中空筒体16と、中空筒体16の
回転周面Rから突設された噴出ノズル18と、燃焼室1
4に空気および燃料を供給する空気・燃料供給手段20
と、燃焼室14内の燃料に点火させる点火手段22と、
を有している。
As shown in FIG. 1, a prime mover 10 according to this embodiment has a hollow rotary shaft 12 having a hollow interior, a hollow cylindrical body 16 having a hollow interior as a combustion chamber 14, and a rotation of the hollow cylindrical body 16. The ejection nozzle 18 protruding from the peripheral surface R and the combustion chamber 1
Air / fuel supply means 20 for supplying air and fuel to 4
And an ignition means 22 for igniting the fuel in the combustion chamber 14,
have.

【0015】図1または図3に示すように、この実施形
態において、原動装置10は、中空回転軸12を回転自
在に軸支する1対の軸受体24、26によって支持され
ている。図1又は図3において、中空回転軸12の左側
の軸受体24側が外部に回転動力を伝える出力側とな
る。図3に示すように、図上、左側すなわち出力側の軸
受体24は、その軸受部25に中空回転軸12を水平に
差し通して中空回転軸12を軸支している。一方、右側
の軸受体26は、左側の軸受体24に対向する側に軸受
ケース27を突設させ、その内部に軸受28が内蔵さ
れ、この軸受28で中空回転軸12の右端側を差し入れ
状に係合させて軸支している。さらに軸受体26の上面
側に開口30が設けられており、軸受体26内部には軸
受28により軸支された中空回転軸12の中空内部とこ
の開口30とをL字状に連通するL字中空部32が設け
られている。
As shown in FIG. 1 or 3, in this embodiment, the prime mover 10 is supported by a pair of bearing bodies 24 and 26 that rotatably support the hollow rotary shaft 12. In FIG. 1 or FIG. 3, the bearing body 24 side on the left side of the hollow rotary shaft 12 is the output side for transmitting the rotational power to the outside. As shown in FIG. 3, the bearing body 24 on the left side, that is, the output side, has the hollow rotary shaft 12 inserted horizontally through the bearing portion 25 to support the hollow rotary shaft 12 in the axial direction. On the other hand, the right side bearing body 26 has a bearing case 27 projecting from the side facing the left side bearing body 24, and a bearing 28 is built in the bearing case 27, and the right end side of the hollow rotary shaft 12 is inserted by the bearing 28. And is pivotally supported. Further, an opening 30 is provided on the upper surface side of the bearing body 26, and the inside of the bearing body 26 has an L-shape that connects the hollow inside of the hollow rotary shaft 12 pivotally supported by a bearing 28 and the opening 30 to each other in an L-shape. A hollow portion 32 is provided.

【0016】図1または図3に示すように、中空回転軸
12は、耐熱性耐圧性の高い金属から形成され、内部を
中空とした中空内部36が形成されている。この実施形
態で用いられる金属は、例えば、耐圧性が高く硬くて加
工しやすい黄銅等を用いるとよい。また、黄銅に限ら
ず、耐熱性や耐圧性のある任意の金属を用いてもよい。
この中空回転軸12の右側は開口34され、その開口3
4が軸受体26のL字中空部32と連通しており、後述
する空気供給手段の空気供給路とされる。この実施形態
において、中空回転軸12は、中空筒体16を貫通した
形態で同中空筒体16に固定されており、中空回転軸に
よって中空回転軸12の中空内部36と中空筒体16の
燃焼室14とが仕切られている。中空回転軸12の中空
内部左端側となる位置でメクラ穴状に閉鎖する閉鎖壁4
0が設けられている。この閉鎖壁40は、三角錐状にそ
の頂点を中空内部36側に向けて突出して設けられてい
る。また、中空筒体16内部分の中空回転軸12の周壁
には小径の貫通孔38が複数個穿孔されており、この貫
通孔38によって中空回転軸12の中空内部36と燃焼
室14とが連通されている。これにより、中空回転軸内
に開口30側から空気が圧送されると貫通孔38を通っ
て燃焼室14内へ流入させる。
As shown in FIG. 1 or 3, the hollow rotary shaft 12 is made of a metal having a high heat resistance and a high pressure resistance, and a hollow interior 36 having a hollow interior is formed. As the metal used in this embodiment, for example, brass having high pressure resistance, hard, and easy to process may be used. Further, not limited to brass, any metal having heat resistance and pressure resistance may be used.
The right side of the hollow rotary shaft 12 has an opening 34, and the opening 3
4 communicates with the L-shaped hollow portion 32 of the bearing body 26, and serves as an air supply passage of an air supply unit described later. In this embodiment, the hollow rotating shaft 12 is fixed to the hollow cylindrical body 16 so as to penetrate through the hollow cylindrical body 16, and the hollow inside 36 of the hollow rotating shaft 12 and the hollow cylindrical body 16 are burned by the hollow rotating shaft. The room 14 is partitioned. A closing wall 4 that closes like a blind hole at a position that is on the left end side inside the hollow rotating shaft 12.
0 is provided. The closing wall 40 is provided in a triangular pyramid shape with its apex protruding toward the hollow interior 36 side. A plurality of small-diameter through holes 38 are bored in the peripheral wall of the hollow rotary shaft 12 inside the hollow cylindrical body 16, and the hollow interior 36 of the hollow rotary shaft 12 and the combustion chamber 14 communicate with each other through the through holes 38. Has been done. As a result, when air is pumped into the hollow rotary shaft from the opening 30 side, the air is made to flow into the combustion chamber 14 through the through hole 38.

【0017】図1ないし図3に示すように、中空筒体1
6は、この実施形態において、例えば、中空回転軸と同
様の耐熱性及び耐圧性の高い金属で形成されており、円
筒形状に形成されている。中空筒体16の円筒の両端面
は円形板体42で覆蓋されて略密閉状に設けられてい
る。中空筒体16は、円形板体42の中心を中空回転軸
12が垂直に貫通した状態で固定されており、円筒周面
が回転周面Rとなる。中空筒体16内部の燃焼室14
は、空気・燃料供給手段20により供給される燃料を燃
焼させて燃焼膨張空気Tを発生させる空間であり、中空
筒体16と同心の円筒形状の空間である。図2または図
3に示すように、燃焼室14内には、点火手段22の点
火点44が配置されており、燃焼室14内の燃料に自在
に点火される。また、中空筒体16の円形板体42に
は、複数の冷却部材45が外部側に向けて突出して設け
られている。冷却部材45には、円形板体42との間に
空隙45aを有しており、円形板体42の表面積を広く
して燃焼室で発生する熱を良好に放熱させる。なお、冷
却部材45は、例えば、フィンを突設させたものでもよ
く、その他の任意の形状でもよい。実施形態において、
中空筒体16の回転周面Rには、90度おきに噴出ノズ
ル18が一体的に設けられている。さらに中空筒体16
には、噴出ノズル18の取付位置に対応しこの噴出ノズ
ル18に向けて燃焼膨張空気Tを導入排出させる燃焼室
14と外部とを連通させる排気孔46が設けらていれ
る。
As shown in FIGS. 1 to 3, the hollow cylindrical body 1
In this embodiment, 6 is formed of, for example, a metal having high heat resistance and pressure resistance similar to that of the hollow rotating shaft, and has a cylindrical shape. Both end surfaces of the cylinder of the hollow cylindrical body 16 are covered with a circular plate body 42 and are provided in a substantially hermetically sealed manner. The hollow cylindrical body 16 is fixed in a state where the hollow rotary shaft 12 vertically penetrates the center of the circular plate body 42, and the cylindrical peripheral surface becomes the rotary peripheral surface R. Combustion chamber 14 inside hollow cylinder 16
Is a space for burning the fuel supplied by the air / fuel supply means 20 to generate combustion expanded air T, which is a cylindrical space concentric with the hollow cylindrical body 16. As shown in FIG. 2 or FIG. 3, the ignition point 44 of the ignition means 22 is arranged in the combustion chamber 14, and the fuel in the combustion chamber 14 is freely ignited. A plurality of cooling members 45 are provided on the circular plate body 42 of the hollow cylindrical body 16 so as to project toward the outside. The cooling member 45 has a gap 45a between the cooling member 45 and the circular plate body 42, and widens the surface area of the circular plate body 42 to satisfactorily radiate the heat generated in the combustion chamber. The cooling member 45 may be, for example, a fin provided in a protruding manner, or may have any other shape. In an embodiment,
On the rotating peripheral surface R of the hollow cylindrical body 16, jet nozzles 18 are integrally provided at every 90 degrees. Further hollow cylinder 16
An exhaust hole 46 is provided corresponding to the mounting position of the jet nozzle 18 to connect the combustion chamber 14 for introducing and discharging the combustion expansion air T toward the jet nozzle 18 and the outside.

【0018】図2において、噴出ノズル18は、燃焼室
14で発生させた燃焼膨張空気Tを噴出口48から外部
に噴出させて中空筒体を回転させるための空気噴出ノズ
ルである。この実施形態において、噴出ノズル18は、
略L字管状に形成されており、その内部を排気孔46を
介して燃焼室14と連通させつつ中空筒体16の回転周
面R上に固定され、さらに噴出口48を回転円周接線方
向に向くように設けられている。すなわち、図2におい
て、中空筒体16の回転方向を左回りとすると、その回
転中心から噴出ノズル18の接続端側(中空筒体16の
排気孔46)を見た時に右曲がり90度方向に噴出口4
8が向くように設けられている。なお、中空筒体の大き
さや燃焼室の容積、あるいは噴出口48の径の大きさ等
は必要とする回転出力の大きさに応じて任意に設定され
る。
In FIG. 2, the ejection nozzle 18 is an air ejection nozzle for ejecting the combustion expansion air T generated in the combustion chamber 14 from the ejection port 48 to rotate the hollow cylindrical body. In this embodiment, the jet nozzle 18 is
It is formed in a substantially L-shaped tubular shape, and is fixed on the rotating peripheral surface R of the hollow cylindrical body 16 while communicating the inside thereof with the combustion chamber 14 through the exhaust hole 46, and the jet outlet 48 is further tangential to the rotating circumferential direction. It is provided to face. That is, in FIG. 2, assuming that the rotation direction of the hollow cylindrical body 16 is counterclockwise, when looking at the connection end side of the ejection nozzle 18 (exhaust hole 46 of the hollow cylindrical body 16) from the center of rotation, a right turn is made in a 90-degree direction. Spout 4
8 is provided so as to face. The size of the hollow cylindrical body, the volume of the combustion chamber, the size of the diameter of the ejection port 48, and the like are arbitrarily set according to the required rotation output.

【0019】図1または図3に示すように、空気・燃料
供給手段20は、この実施形態において、空気供給手段
50と、燃料供給手段52と、を備えており、中空回転
軸12の中空部36を介して中空筒体16内の燃焼室1
4内に空気と燃料を供給する。
As shown in FIG. 1 or 3, the air / fuel supply means 20 in this embodiment is provided with an air supply means 50 and a fuel supply means 52, and the hollow portion of the hollow rotary shaft 12 is provided. Combustion chamber 1 in hollow cylindrical body 16 via 36
4. Supply air and fuel into 4.

【0020】この実施形態において、空気供給手段50
は、図3に示すように、空気圧縮圧送用の空気ポンプ5
4と、中空回転軸12の中空部36と軸受体26のL字
中空部32とからなる空気供給路と、を有している。空
気ポンプ54は、例えば、コンプレッサ等からなり、空
気を圧縮して中空回転軸12の中空内部36及び燃焼室
14に圧送する装置である。空気ポンプ54は、空気調
整バルブ56を有する空気供給パイプ58を介して軸受
体26の上面側開口30に接続されている。空気ポンプ
54によって圧縮された空気は、空気供給パイプ58を
通って、軸受体26のL字中空部32内を通過して中空
回転軸12の中空内部36を圧送されて燃焼室14側に
供給される。中空回転軸の中空内部を空気供給路とした
構成とすることにより、構造を複雑にすることなく空気
を燃焼室側に確実にかつ効率良く送ることができる。
In this embodiment, the air supply means 50
Is, as shown in FIG. 3, an air pump 5 for compressed air feeding.
4 and an air supply path formed by the hollow portion 36 of the hollow rotary shaft 12 and the L-shaped hollow portion 32 of the bearing body 26. The air pump 54 is, for example, a compressor, and is a device that compresses air and sends the compressed air to the hollow interior 36 of the hollow rotary shaft 12 and the combustion chamber 14. The air pump 54 is connected to the upper surface side opening 30 of the bearing body 26 via an air supply pipe 58 having an air adjusting valve 56. The air compressed by the air pump 54 passes through the air supply pipe 58, passes through the L-shaped hollow portion 32 of the bearing body 26, is pressure-fed through the hollow inside 36 of the hollow rotary shaft 12, and is supplied to the combustion chamber 14 side. To be done. By configuring the inside of the hollow rotating shaft as the air supply path, the air can be reliably and efficiently sent to the combustion chamber side without complicating the structure.

【0021】この実施形態において、図3に示すよう
に、燃料供給手段52は、燃料供給源である燃料ポンプ
60と、燃料供給路62と、からなる。燃料は、例え
ば、ガソリン、灯油、軽油、重油等の液体燃料又はプロ
パンガス等の気体燃料を任意に選択して適用してよい。
燃料ポンプ60は、燃料を燃料供給路62に圧送して燃
焼室側に供給する装置である。
In this embodiment, as shown in FIG. 3, the fuel supply means 52 comprises a fuel pump 60 as a fuel supply source and a fuel supply passage 62. As the fuel, for example, a liquid fuel such as gasoline, kerosene, light oil, heavy oil or a gaseous fuel such as propane gas may be arbitrarily selected and applied.
The fuel pump 60 is a device that pumps fuel to the fuel supply passage 62 and supplies it to the combustion chamber side.

【0022】燃料供給路62は、この実施形態におい
て、吐出部がテーパー状に形成されたニードルパイプ状
の燃料パイプ64から形成されており、中空回転軸12
の中心部及び軸受体26のL字中空部32を水平方向に
挿通され、軸受体26の左側壁を貫通して直線状に配置
されて固定支持されている。燃料パイプ64は、軸受体
26に対する固定位置から外部に向けて長手方向に延長
されており、途中に燃料調整バルブ66が設けられて外
部の燃料ポンプ60に接続される。燃料パイプ64の吐
出部の先端が燃料供給口68であり、この燃料供給口6
8を中空回転軸12の中空筒体16内の軸方向の略中心
位置に配置させている。すなわち、燃料供給口68が配
置されている中空回転軸12の中空内であって貫通孔3
8が設けられた部分に対応する空間部が混合空間Mとな
り、混合空間Mで燃料供給口68から噴射された燃料と
空気供給手段50によって圧送された空気とが混合され
る。この混合気体は圧送空気によって貫通孔38を通過
して燃焼室14に均一に供給される。
In this embodiment, the fuel supply passage 62 is formed of a needle pipe-shaped fuel pipe 64 having a tapered discharge portion, and the hollow rotary shaft 12
Is horizontally inserted through the central portion of the bearing body 26 and the L-shaped hollow portion 32 of the bearing body 26, penetrates the left side wall of the bearing body 26, and is linearly arranged and fixedly supported. The fuel pipe 64 extends in the longitudinal direction from the fixed position with respect to the bearing body 26 toward the outside, and a fuel adjusting valve 66 is provided on the way to be connected to the external fuel pump 60. The tip of the discharge portion of the fuel pipe 64 is a fuel supply port 68.
8 is disposed in the hollow cylindrical body 16 of the hollow rotary shaft 12 at a substantially central position in the axial direction. That is, in the hollow of the hollow rotary shaft 12 in which the fuel supply port 68 is arranged, the through hole 3
The space corresponding to the portion where 8 is provided becomes the mixing space M, and the fuel injected from the fuel supply port 68 and the air pumped by the air supply means 50 are mixed in the mixing space M. This mixed gas is uniformly supplied to the combustion chamber 14 through the through hole 38 by the pressure-fed air.

【0023】この実施形態において、点火手段22は、
図3に示すように、点火装置70と、点火装置用回路7
2と、を有した放電装置からなる。点火装置70は、例
えば、点火プラグからなり、一端に放電子74が配置さ
れた点火点44が設けられおり、他端側を入力端子76
として点火装置用回路72に接続される。また、点火装
置70の外部側面は絶縁体で覆われている。図2にも示
すように、点火装置70は、その点火点44が燃焼室1
4内の中空回転軸12に近接するように配置され、中空
筒体16の円形板体42の偏心位置を貫通して絶縁体部
分を円形板体42に固定されて支持されている。放電子
74は、わずかな間隙をおいた一対の電極からなり、入
力端子76に高電圧の電流を流すと放電子74の間隙で
火花が発生し燃焼室内の燃料に点火させる。また、図1
または図3に示すように、点火装置70の入力端子76
は、中空回転軸12の外面から外側に張り出し状に固定
された薄肉厚の円環導体板78に接続されている。
In this embodiment, the ignition means 22 is
As shown in FIG. 3, the ignition device 70 and the ignition device circuit 7 are provided.
2 and a discharge device having. The ignition device 70 is formed of, for example, a spark plug, and has an ignition point 44 having a discharge element 74 arranged at one end and an input terminal 76 at the other end.
Is connected to the ignition circuit 72. The outer side surface of the ignition device 70 is covered with an insulator. As shown in FIG. 2, the ignition device 70 has an ignition point 44 in the combustion chamber 1.
It is arranged so as to be close to the hollow rotary shaft 12 in the hollow cylinder 4, and penetrates the eccentric position of the circular plate body 42 of the hollow cylindrical body 16 so that the insulator portion is fixed and supported by the circular plate body 42. The discharge element 74 is composed of a pair of electrodes with a slight gap, and when a high voltage current is applied to the input terminal 76, a spark is generated in the gap of the discharge element 74 to ignite the fuel in the combustion chamber. Also, FIG.
Alternatively, as shown in FIG. 3, the input terminal 76 of the ignition device 70
Are connected to a thin-walled annular conductor plate 78 that is fixed in an outwardly protruding shape from the outer surface of the hollow rotary shaft 12.

【0024】点火装置用回路72は、図示しない電源等
に接続されており、内部回路にて高電圧を発生させて点
火装置70に電流を流して火花を起こさせるものであ
る。図3に示すように、点火装置用回路72はブラシ7
9を介して円環導体板78に接続される。ブラシ79
は、例えば、軸受体26に固定されたブラシ支持体77
に支持され、ブラシ79の一端を中空回転軸とともに回
転する円環導体板78に接触させている。したがって、
点火装置用回路72と点火装置70とは常に電気的接続
状態となり燃料室14の燃料に自在に点火できる。
The igniter circuit 72 is connected to a power source (not shown) or the like, and generates a high voltage in an internal circuit to flow a current to the igniter 70 to cause a spark. As shown in FIG. 3, the ignition device circuit 72 includes a brush 7
It is connected to the annular conductor plate 78 via 9. Brush 79
Is, for example, a brush support 77 fixed to the bearing body 26.
The brush 79 has one end thereof brought into contact with an annular conductor plate 78 which rotates together with the hollow rotating shaft. Therefore,
The ignition device circuit 72 and the ignition device 70 are always in an electrically connected state, and the fuel in the fuel chamber 14 can be freely ignited.

【0025】次に、この実施形態に係る原動装置の作用
について説明する。図3に示すように、燃料ポンプによ
り燃料供給路から圧送された燃料は中空回転軸の中空部
の混合空間で燃料供給口から噴射される。噴射された燃
料は、空気ポンプにより空気供給路を圧送された空気と
混合されて貫通孔を介して燃焼室へ圧送される。それと
同時に、点火装置用回路で発生させた高電圧の電流は、
ブラシを介して円環導体板に通じ点火装置に流れ、放電
子で火花を起こす。そして、中空筒体の燃焼室内の燃料
は放電子の火花によって点火されて燃焼し、高温高圧の
燃焼膨張気体を発生する。図2に示すように、燃焼室内
で発生した燃焼膨張空気は、噴出ノズルから回転円周接
線方向に向けて噴出される。その噴出反力によって、中
空筒体及び中空回転軸体が一体回転し回転動力を得る。
これにより、構造を複雑にすることなく燃料及び空気を
燃焼室へ確実にしかも効率良く燃焼する燃料を供給でき
るとともに燃焼室内で大きな燃焼膨張エネルギーを発生
させて大きな回転動力を確実に出力することができる。
Next, the operation of the prime mover according to this embodiment will be described. As shown in FIG. 3, the fuel pumped from the fuel supply passage by the fuel pump is injected from the fuel supply port in the mixing space in the hollow portion of the hollow rotating shaft. The injected fuel is mixed with the air pressure-fed through the air supply passage by the air pump and pressure-fed to the combustion chamber through the through hole. At the same time, the high-voltage current generated in the ignition circuit is
It flows through the brush to the circular conductor plate, flows to the ignition device, and sparks at the discharge element. Then, the fuel in the combustion chamber of the hollow cylindrical body is ignited by the sparks of the discharge element and burned to generate combustion expanded gas of high temperature and high pressure. As shown in FIG. 2, the combustion expanded air generated in the combustion chamber is ejected from the ejection nozzle in the tangential direction of the rotation circumference. Due to the ejection reaction force, the hollow cylindrical body and the hollow rotating shaft body rotate integrally to obtain rotational power.
As a result, it is possible to reliably and efficiently supply fuel and air that burn fuel and air to the combustion chamber without complicating the structure, and to generate large combustion expansion energy in the combustion chamber to reliably output large rotational power. it can.

【0026】また、図4は、実施形態の原動装置10の
噴出排気ガスを再利用した使用例を示している。原動装
置10から排出された高温高圧の燃焼膨張空気を熱交換
器80や排ガスボイラー82へ引き込み、燃焼膨張空気
の熱エネルギーを、例えば、冷房や暖房等に利用する。
これにより、エネルギーを無駄なく使用できる。
Further, FIG. 4 shows an example of use in which the exhaust gas discharged from the prime mover 10 of the embodiment is reused. The high-temperature high-pressure combustion expanded air discharged from the prime mover 10 is drawn into the heat exchanger 80 and the exhaust gas boiler 82, and the thermal energy of the combustion expanded air is used for, for example, cooling and heating.
This allows energy to be used without waste.

【0027】本発明の原動装置は上記した実施の形態に
限定されるものではなく特許請求の範囲に記載した発明
の本質を逸脱しない範囲において任意の改変を加えても
良い。例えば、噴出ノズルの個数は、4個に限らず、2
個又は3個、或は5個以上設けてもよい。また、中空筒
体16の形状は、三角筒状、四角筒状、またはそれ以上
の多角形筒状に設けても良い。
The prime mover of the present invention is not limited to the above-mentioned embodiments, and any modification may be added within the scope not departing from the essence of the invention described in the claims. For example, the number of ejection nozzles is not limited to four, but 2
One or three pieces, or five or more pieces may be provided. Further, the hollow tubular body 16 may be provided in a triangular tubular shape, a quadrangular tubular shape, or a polygonal tubular shape having more than that.

【0028】[0028]

【発明の効果】上記したように本発明の原動装置によれ
ば、両側を回転自在に軸支された内部が中空の中空回転
軸と、中空回転軸に貫通状に固定され中空回転軸の中空
部に連通する燃焼室を内部に有して該中空回転軸と一体
回転する中空筒体と、中空筒体の回転周面から突設され
中空筒体内の燃焼室と連通し回転円周接線方向にその噴
出口を向けて設けられた噴出ノズルと、中空回転軸の中
空部を含み、中空筒体内の燃焼室内へ燃料及び空気を供
給する空気・燃料供給手段と、燃焼室内に点火点を配置
させて燃焼室内の燃料に自在に点火させる点火手段と、
を有し、中空筒体の燃焼室内で点火させてその燃焼膨張
空気の噴出ノズルからの噴出反力で中空筒体を回転させ
て回転動力を得る構成であるから、中空筒体内の燃焼室
で燃焼させて噴出ノズルから噴出させる結果、この燃焼
室内で大きな燃焼膨張空気による燃焼膨張エネルギーを
発生させ、確実に大きな回転動力を得ることができる。
さらに、中空回転軸の中空部を介して燃料及び空気を供
給するので、燃焼室に空気及び燃料を効率良く供給でき
るとともに装置を複雑にすることなく装置全体がコンパ
クトに製造でき、製造コストも低廉にすることできる。
As described above, according to the prime mover of the present invention, a hollow rotary shaft whose inside is hollow and rotatably supported on both sides, and a hollow rotary shaft which is fixed to the hollow rotary shaft so as to penetrate therethrough. A hollow cylindrical body that has a combustion chamber communicating with the hollow section and that rotates integrally with the hollow rotating shaft; and a hollow circumferential cylinder projecting from the peripheral surface of the hollow cylindrical body and communicating with the combustion chamber inside the hollow cylindrical body An injection nozzle provided with its ejection port facing to the inside, an air / fuel supply means including a hollow portion of a hollow rotating shaft for supplying fuel and air into the combustion chamber in the hollow cylinder, and an ignition point arranged in the combustion chamber Ignition means for freely igniting the fuel in the combustion chamber,
In the combustion chamber of the hollow cylinder, the hollow cylinder has a structure in which the rotary cylinder is rotated by an ejection reaction force from the ejection nozzle of the combustion expansion air to ignite in the combustion chamber of the hollow cylinder to obtain rotational power. As a result of burning and jetting from the jet nozzle, a large amount of combustion expansion energy is generated in the combustion chamber by the combustion expansion air, and a large rotational power can be reliably obtained.
Further, since the fuel and the air are supplied through the hollow portion of the hollow rotary shaft, the air and the fuel can be efficiently supplied to the combustion chamber, and the entire device can be manufactured compactly without complicating the device, and the manufacturing cost is low. Can be

【0029】また、点火手段の点火点が燃焼室内の中空
回転軸の取り付け位置に近接して配置された構成とする
ことにより、1個の点火装置だけで燃焼室内の燃料に効
率良く点火させることができる。また、構造が簡単で、
製造コストも低廉にすることができる。
Further, since the ignition point of the ignition means is arranged close to the mounting position of the hollow rotary shaft in the combustion chamber, the fuel in the combustion chamber can be efficiently ignited by only one ignition device. You can Also, the structure is simple,
Manufacturing costs can also be reduced.

【0030】また、空気・燃料供給手段は、中空回転軸
の中空内部を空気供給路として外部から空気を圧送する
空気供給手段と、中空回転軸の中空部の略中心位置で空
気供給手段による空気と混合するように燃料を供給する
燃料供給手段と、を備えた構成とすることにより、中空
回転軸内部を空気供給路として利用するので構造を複雑
にすることなく燃焼に必要な空気を確実に大量に供給す
ることができる。また、大量の空気を圧送できるととも
に中空回転軸の中空部の中心位置で空気と燃料を混合さ
せるので、ムラなく混ざって着火しやすい燃料を燃焼室
に供給でき燃焼効率を良くして稼動効率を良くすること
ができる。
The air / fuel supply means includes an air supply means for pumping air from the outside using the hollow inside of the hollow rotary shaft as an air supply passage, and an air supplied by the air supply means at a substantially central position of the hollow portion of the hollow rotary shaft. By providing the fuel supply means for supplying fuel so as to mix with the air, the inside of the hollow rotary shaft is used as an air supply path, so that the air necessary for combustion can be reliably provided without complicating the structure. Can be supplied in large quantities. Also, since a large amount of air can be pumped and the air and fuel are mixed at the central position of the hollow part of the hollow rotary shaft, fuel that is easily mixed and ignited can be supplied to the combustion chamber to improve combustion efficiency and improve operating efficiency. You can get better.

【0031】また、燃料供給手段は、中空筒体内部の軸
方向の略中心位置にその供給口が設定されている構成と
することにより、供給口から噴射される燃料と空気圧送
手段によって圧送された空気とをムラなく混合させるこ
とができ、燃料に点火させやすく燃焼室内での良好な燃
焼が行われて、原動装置を効率良く稼動できる。
Further, the fuel supply means is configured such that the supply port is set at a substantially central position in the axial direction inside the hollow cylindrical body, so that the fuel injected from the supply port and the air pressure supply means are pressure-fed. The air can be evenly mixed, and the fuel can be easily ignited, good combustion is performed in the combustion chamber, and the prime mover can be efficiently operated.

【0032】また、中空筒体は中空回転軸に貫通された
状態で固定され、中空筒体内となる中空回転軸に設けら
れた複数の連通孔を介して燃焼室と中空回転軸の中空部
が仕切られた状態で相互に連通された構成とすることに
より、中空回転軸内部から空気及び燃料を燃焼室内に供
給するとともに燃焼室と中空回転軸の中空部とを仕切る
ことによって燃焼室の燃焼によって中空回転軸内の燃料
に引火するのを防止して、装置の安全性及び耐久度を高
めることができる。
Further, the hollow cylindrical body is fixed in a state of penetrating the hollow rotary shaft, and the combustion chamber and the hollow portion of the hollow rotary shaft are connected to each other through a plurality of communication holes provided in the hollow rotary shaft which is the hollow cylindrical body. With the structure in which they are communicated with each other in a partitioned state, by supplying air and fuel from the inside of the hollow rotating shaft into the combustion chamber and partitioning the combustion chamber and the hollow portion of the hollow rotating shaft, combustion of the combustion chamber is achieved. It is possible to prevent the fuel in the hollow rotary shaft from being ignited and improve the safety and durability of the device.

【0033】また、燃料供給手段は、中空回転軸の中心
部を挿通され同中空回転軸の長手方向に延長されて外部
の燃料供給源に接続されるニードルパイプ状の燃料供給
路を含む構成とすることにより、燃料供給路が回転軸内
に配置されるので、構造を複雑にすることなくかつ空気
の圧送を妨害しないで燃料を供給することができ、かつ
低コストで効率のよい原動装置を製造できる。また、供
給口から噴射される燃料と空気圧送手段によって圧送さ
れた空気とがムラなく混合するので、燃料に点火しやす
くなり、効率よく稼動できる。
Further, the fuel supply means includes a needle pipe-shaped fuel supply passage which is inserted through the central portion of the hollow rotary shaft and extends in the longitudinal direction of the hollow rotary shaft to be connected to an external fuel supply source. By doing so, the fuel supply path is arranged in the rotating shaft, so that the fuel can be supplied without complicating the structure and without disturbing the pressure feeding of air, and a low-cost and efficient prime mover can be provided. Can be manufactured. Further, since the fuel injected from the supply port and the air pressure-fed by the air pressure-feeding means are uniformly mixed, the fuel is easily ignited and the fuel cell can be efficiently operated.

【0034】また、点火手段は、点火点に配置された放
電子を含む放電装置からなる構成とすることにより、燃
焼室内の燃料に確実に点火することができる。また、コ
ンパクトに製造できるとともに構造も簡単にすることが
できる。
Further, the igniting means can surely ignite the fuel in the combustion chamber by comprising the discharge device including the discharge element arranged at the ignition point. Further, it can be manufactured compactly and the structure can be simplified.

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

【図1】本発明の原動装置の実施形態の斜視図である。FIG. 1 is a perspective view of an embodiment of a prime mover of the present invention.

【図2】図1の一部切欠きアーア矢視図である。FIG. 2 is a partially cutaway arrow view of FIG.

【図3】図2のA―A断面図である。3 is a cross-sectional view taken along the line AA of FIG.

【図4】原動装置の噴出空気を再利用する使用例を示し
た図である。
FIG. 4 is a diagram showing an example of use in which jet air of a prime mover is reused.

【図5】(a)は、従来の原動機の側面図、(b)は、
(a)の一部切り欠き正面図である。
FIG. 5A is a side view of a conventional prime mover, and FIG.
It is a partially notched front view of (a).

【図6】(a)は、従来の蒸気タービン併用噴射式ロー
タリー原動機の一部平面図、(b)は、側断面図であ
る。
FIG. 6 (a) is a partial plan view of a conventional steam turbine combined injection type rotary prime mover, and FIG. 6 (b) is a side sectional view.

【符号の説明】[Explanation of symbols]

10 原動装置 12 中空回転軸 14 燃焼室 16 中空筒体 18 噴出ノズル 20 空気・燃料供給手段 22 点火手段 44 点火点 48 噴出口 50 空気供給手段 52 燃料供給手段 62 燃料供給路 68 燃料供給口 T 燃焼膨張空気 10 prime mover 12 hollow rotating shaft 14 Combustion chamber 16 hollow cylinder 18 jet nozzle 20 Air / fuel supply means 22 Ignition means 44 ignition point 48 spout 50 Air supply means 52 Fuel Supply Means 62 Fuel supply path 68 Fuel supply port T Combustion expanded air

Claims (7)

【特許請求の範囲】[Claims] 【請求項1】 両側を回転自在に軸支された内部が中空
の中空回転軸と、 中空回転軸に貫通状に固定され中空回転軸の中空部に連
通する燃焼室を内部に有して該中空回転軸と一体回転す
る中空筒体と、 中空筒体の回転周面から突設され中空筒体内の燃焼室と
連通し回転円周接線方向にその噴出口を向けて設けられ
た噴出ノズルと、 中空回転軸の中空部を含み、中空筒体内の燃焼室内へ燃
料及び空気を供給する空気・燃料供給手段と、 燃焼室内に点火点を配置させて燃焼室内の燃料に自在に
点火させる点火手段と、を有し、 中空筒体の燃焼室内で点火させてその燃焼膨張空気の噴
出ノズルからの噴出反力で中空筒体を回転させて回転動
力を得ることを特徴とする原動装置。
1. A hollow rotary shaft having a hollow interior rotatably supported on both sides and a combustion chamber fixed to the hollow rotary shaft in a penetrating manner and communicating with a hollow portion of the hollow rotary shaft. A hollow cylindrical body that rotates integrally with the hollow rotating shaft; and an ejection nozzle that is provided so as to project from the rotational peripheral surface of the hollow cylindrical body and communicate with the combustion chamber in the hollow cylindrical body, with its ejection port facing in the tangential direction of the rotational circumference. , An air / fuel supply means including a hollow portion of a hollow rotary shaft for supplying fuel and air into a combustion chamber in a hollow cylinder, and an ignition means for arranging an ignition point in the combustion chamber to freely ignite the fuel in the combustion chamber A prime mover characterized by including: and igniting in the combustion chamber of the hollow cylinder to rotate the hollow cylinder by the reaction force of the jet of the combustion-expanded air from the jet nozzle to obtain rotational power.
【請求項2】 点火手段の点火点が燃焼室内の中空回転
軸の取り付け位置に近接して配置された請求項1記載の
原動装置。
2. The prime mover according to claim 1, wherein the ignition point of the ignition means is arranged close to the mounting position of the hollow rotary shaft in the combustion chamber.
【請求項3】 空気・燃料供給手段は、中空回転軸の中
空内部を空気供給路として外部から空気を圧送する空気
供給手段と、 中空回転軸の中空部の略中心位置で空気供給手段による
空気と混合するように燃料を供給する燃料供給手段と、
を備えた請求項1または2記載の原動装置。
3. The air / fuel supply means includes an air supply means for pumping air from the outside through an air supply path inside the hollow rotary shaft and an air supplied by the air supply means at a substantially central position of the hollow portion of the hollow rotary shaft. Fuel supply means for supplying fuel to mix with
The prime mover according to claim 1 or 2, further comprising:
【請求項4】 燃料供給手段は、中空筒体内部の軸方向
の略中心位置にその供給口が設定されている請求項3記
載の原動装置。
4. The prime mover according to claim 3, wherein the fuel supply means has a supply port set at a substantially central position in the axial direction inside the hollow cylindrical body.
【請求項5】 中空筒体は中空回転軸に貫通された状態
で固定され、 中空筒体内となる中空回転軸に設けられた複数の連通孔
を介して燃焼室と中空回転軸の中空部が仕切られた状態
で相互に連通された請求項3または4記載の原動装置。
5. The hollow cylindrical body is fixed in a state of penetrating the hollow rotating shaft, and the combustion chamber and the hollow portion of the hollow rotating shaft are connected to each other through a plurality of communication holes provided in the hollow rotating shaft which is the hollow cylindrical body. The prime mover according to claim 3 or 4, which is communicated with each other in a partitioned state.
【請求項6】 燃料供給手段は、中空回転軸の中心部を
挿通され同中空回転軸の長手方向に延長されて外部の燃
料供給源に接続されるニードルパイプ状の燃料供給路を
含む請求項3ないし5のいずれかに記載の原動装置。
6. The fuel supply means includes a needle pipe-shaped fuel supply passage which is inserted through a central portion of the hollow rotary shaft and extends in the longitudinal direction of the hollow rotary shaft and is connected to an external fuel supply source. The prime mover according to any one of 3 to 5.
【請求項7】 点火手段は、点火点に配置された放電子
を含む放電装置からなる請求項1ないし6記載の原動装
置。
7. The prime mover according to claim 1, wherein the ignition means comprises a discharge device including a discharge element arranged at an ignition point.
JP2002064804A 2002-03-11 2002-03-11 Prime mover Expired - Fee Related JP3837601B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2002064804A JP3837601B2 (en) 2002-03-11 2002-03-11 Prime mover

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2002064804A JP3837601B2 (en) 2002-03-11 2002-03-11 Prime mover

Publications (2)

Publication Number Publication Date
JP2003269189A true JP2003269189A (en) 2003-09-25
JP3837601B2 JP3837601B2 (en) 2006-10-25

Family

ID=29197405

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2002064804A Expired - Fee Related JP3837601B2 (en) 2002-03-11 2002-03-11 Prime mover

Country Status (1)

Country Link
JP (1) JP3837601B2 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010107146A1 (en) * 2009-03-18 2010-09-23 Kim Ki-Tae Reaction-type turbine
JP2010533259A (en) * 2007-07-10 2010-10-21 ジーヤッド クアムヒイェー Rotary internal combustion engine
KR101044395B1 (en) 2010-08-31 2011-06-27 주식회사 에이치케이터빈 Steam turbine
WO2013168904A1 (en) * 2012-05-10 2013-11-14 주식회사 에이치케이터빈 Reaction turbine
WO2013177706A1 (en) * 2012-05-28 2013-12-05 Worldiscoveries Mechanism for enhanced energy extraction and cooling pressurized gas
US10495353B2 (en) 2012-05-28 2019-12-03 The University Of Western Ontario Mechanism for enhanced energy extraction and cooling of pressurized gas at low flow rates

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101279722B1 (en) * 2011-12-28 2013-06-27 한국항공우주연구원 Gas torch igniter and burner having the same

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2010533259A (en) * 2007-07-10 2010-10-21 ジーヤッド クアムヒイェー Rotary internal combustion engine
WO2010107146A1 (en) * 2009-03-18 2010-09-23 Kim Ki-Tae Reaction-type turbine
KR101044395B1 (en) 2010-08-31 2011-06-27 주식회사 에이치케이터빈 Steam turbine
WO2013168904A1 (en) * 2012-05-10 2013-11-14 주식회사 에이치케이터빈 Reaction turbine
WO2013177706A1 (en) * 2012-05-28 2013-12-05 Worldiscoveries Mechanism for enhanced energy extraction and cooling pressurized gas
US10495353B2 (en) 2012-05-28 2019-12-03 The University Of Western Ontario Mechanism for enhanced energy extraction and cooling of pressurized gas at low flow rates

Also Published As

Publication number Publication date
JP3837601B2 (en) 2006-10-25

Similar Documents

Publication Publication Date Title
JP6215988B2 (en) Method and combustion engine for introducing microwave energy into the combustion chamber of a combustion engine
JP2007132350A5 (en)
CN109441643B (en) Micro-turbojet engine and ignition device for combustion chamber of gas turbine
JP2013503447A (en) Prechamber spark plug
JPS598652B2 (en) torch igniter
US3373723A (en) Internal combustion engine
JP3837601B2 (en) Prime mover
US5274994A (en) Pressure wave machine with integrated combustion
KR200386084Y1 (en) An air guide apparatus for intake manifold of an internal combustion engine
WO2021157302A1 (en) Combustor
JP2015504999A (en) Rotary piston engine
JP2011517741A (en) Boundary layer gas turbine combined with rotary and mechanical reciprocating sliding metal vane air pump and pulse gas turbine engine system
JP6280943B2 (en) Internal combustion engine
JP2002004873A (en) Internal combustion engine
US11486336B2 (en) Propulsion device for liquid propellant rocket engine
KR101153801B1 (en) Plasma buner including radial shape fuel pipe
JP5670886B2 (en) Spark plug assembly
KR100446335B1 (en) Heater for wind tunnel
KR102611920B1 (en) Burner, water heating apparatus and control method of same
RU217752U1 (en) Device for ignition of the combustion chamber of a gas turbine engine
RU2823078C1 (en) Device for inlet of fuel and air into combustion chamber of rotary vane internal combustion engine
CA2027843A1 (en) Rotary engine
JP2000337615A (en) Burner for flame-regardant material
KR100558981B1 (en) Gas producing apparatus for actuating turbo pump of liquid rocket
KR101930077B1 (en) A device of plasma assisted spray combustion and Gas burning Apparatus using the Same

Legal Events

Date Code Title Description
A977 Report on retrieval

Effective date: 20040722

Free format text: JAPANESE INTERMEDIATE CODE: A971007

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20051018

A521 Written amendment

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20051116

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20060627

A61 First payment of annual fees (during grant procedure)

Effective date: 20060713

Free format text: JAPANESE INTERMEDIATE CODE: A61

R150 Certificate of patent (=grant) or registration of utility model

Free format text: JAPANESE INTERMEDIATE CODE: R150

LAPS Cancellation because of no payment of annual fees