JP2001107840A - Device for converting centrifugal force into propulsive force - Google Patents
Device for converting centrifugal force into propulsive forceInfo
- Publication number
- JP2001107840A JP2001107840A JP32731799A JP32731799A JP2001107840A JP 2001107840 A JP2001107840 A JP 2001107840A JP 32731799 A JP32731799 A JP 32731799A JP 32731799 A JP32731799 A JP 32731799A JP 2001107840 A JP2001107840 A JP 2001107840A
- Authority
- JP
- Japan
- Prior art keywords
- centrifugal force
- force
- mass
- generated
- orbit
- 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
Links
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- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
Description
【0001】本発明は、下記の構造である。同一中心の
内輪と外輪を複数のシリンダーレールで連結する。シリ
ンダーレールには、シリンダーレールに沿って、半径方
向に摺動する物体(質量)を設ける。それらを、中心を
軸にして回転させる。回転する回転体のシリンダーレー
ルに沿って摺動する物体(質量)を、周回軌道の半径が
小さい小さな円軌道、内輪から外輪へ移行する直線軌
道、周回軌道の半径が大きい大きな円軌道、外輪から内
輪へ移行する直線軌道。この周回軌道を物体(質量)が
周回運動するよう軌道制御を行わせる軌道環を設ける。
軌道環は、小さな円軌道の円の中心と、大きな円軌道の
円の中心が、回転体の中心軸の中心と同じになるよう設
け、回転しないよう軸に固定し、なおかつ、固定された
軸を中心に角度調整が行えるように設ける。The present invention has the following structure. Connect the inner and outer rings of the same center with multiple cylinder rails. The cylinder rail is provided with an object (mass) that slides in the radial direction along the cylinder rail. They are rotated about a center. An object (mass) that slides along the cylinder rail of a rotating rotating body can be transferred from a small circular orbit with a small orbital radius, a straight orbital transition from the inner ring to the outer ring, a large circular orbit with a large orbital radius, and an outer ring. A straight track that moves to the inner ring. An orbital ring is provided to control the orbit so that an object (mass) orbits around the orbit.
The orbital ring is provided so that the center of the circle of the small circular orbit and the center of the circle of the large circular orbit are the same as the center of the center axis of the rotating body, and is fixed to the shaft so that it does not rotate. Is provided so that the angle can be adjusted around the center.
【0002】本発明は、下記の動作を行う。物体(質
量)の軌道を周回する回転数(角速度)は、シリンダー
レールの回転に従う為、一定である。物体(質量)の回
転半径は、軌道環に制御されるため、小さな円軌道で小
さく、大きな円軌道で大きくなる。このとき、同じ回転
数(角速度)で半径が変わるため、回転数(角速度)の
変化を伴わない、物体(質量)の運動速度の変化を得る
ことができる。遠心力は、質量×回転半径×角速度の2
乗で求められ、一つの周回軌道で回転半径が変化するこ
とによって、大きな円軌道で大きな遠心力が発生し、小
さな円軌道で小さな遠心力が発生する。[0002] The present invention performs the following operations. The number of revolutions (angular velocity) of the orbit of the object (mass) follows the rotation of the cylinder rail, and thus is constant. Since the radius of gyration of the object (mass) is controlled by the orbital ring, it is small for a small circular orbit and large for a large circular orbit. At this time, since the radius changes at the same rotation speed (angular speed), a change in the motion speed of the object (mass) without changing the rotation speed (angular speed) can be obtained. Centrifugal force is 2 times of mass x radius of gyration x angular velocity.
When the radius of gyration changes in one orbit, a large centrifugal force is generated in a large circular orbit, and a small centrifugal force is generated in a small circular orbit.
【0003】本発明は、下記の効果を発揮する。軌道環
は回転の軸に固定されているため、大きな円軌道、小さ
な円軌道の位置は変化しない。そのため、大きな遠心
力、小さな遠心力は、固定された方向にのみ発生し、大
きな遠心力と、小さな遠心力の量の差が推進力となっ
て、装置を大きな遠心力が向く方向に引っ張る。また、
小さな円軌道から大きな円軌道へ、または、大きな円軌
道から小さな円軌道へ移行する際、軌道の変化に伴い発
生する慣性力は、お互いの対角線上にあるため相殺さ
れ、発生する推進力の大きさには影響しない。また、軸
に固定された軌道環を、軸に対して角度調整すること
で、推進力の発生する向きを自在に変化させることがで
きる。[0003] The present invention has the following effects. Since the orbital ring is fixed to the axis of rotation, the positions of the large and small circular orbits do not change. Therefore, a large centrifugal force and a small centrifugal force are generated only in a fixed direction, and a difference between the large centrifugal force and the small centrifugal force becomes a driving force, and pulls the device in a direction toward the large centrifugal force. Also,
When transitioning from a small circular orbit to a large circular orbit, or from a large circular orbit to a small circular orbit, the inertial forces generated due to changes in the orbit are offset on each other's diagonal lines, and the amount of thrust generated is large. Does not affect Further, by adjusting the angle of the race ring fixed to the shaft with respect to the shaft, the direction in which the propulsion force is generated can be freely changed.
【発明の属する技術分野】本発明は、航空機、宇宙船、
などを推進させる、反動を伴わない推進機関に関する発
明である。TECHNICAL FIELD The present invention relates to an aircraft, a spacecraft,
It is an invention related to a propulsion engine that does not involve a recoil that promotes the above.
【従来の技術】従来の推進機関は、外部の媒体(空気や
水)をプロペラや爆発によって、押すことで得られる反
動、もしくは、内蔵するエネルギーを噴射、消費するこ
とで得られる反動を利用していた。また、推進力は一方
向にのみ発生し、推進させる方向の制御は、外部の媒
体、別個の装置、別個の推進力などで行っていた。2. Description of the Related Art A conventional propulsion engine utilizes a recoil obtained by pushing an external medium (air or water) by a propeller or an explosion, or a reaction obtained by injecting and consuming internal energy. I was Further, the propulsion force is generated only in one direction, and the control of the propulsion direction is performed by an external medium, a separate device, a separate propulsion force, or the like.
【発明が解決しようとしている課題】従来の技術では、
外部の媒体が存在しない場所(宇宙空間など)では、反
動を得るための内蔵できるエネルギーに限度があり、推
進力を得られる期間が限られていた。また、推進力の発
生する方向が一方向に限られ、推進する方向を変化させ
るために、外部の媒体、別個の装置、別個の推進力を必
要とした。In the prior art,
In places where there is no external medium (such as outer space), there is a limit to the amount of energy that can be built in to obtain recoil, and the period during which propulsion can be obtained is limited. Further, the direction in which the propulsion force is generated is limited to one direction, and an external medium, a separate device, and a separate propulsion force are required to change the propulsion direction.
【課題を解決するための手段】回転体が回転すると、周
回軌道を周回運動する対角線上の質量が同じであれば、
対角線上で反対の向き、同じ大きさの遠心力が発生する
が、周回運動している物体の対角線上での質量や回転の
中心からの距離が異なれば回転体は質量や半径の差によ
る遠心力量の差によって振動する。この回転体を振動さ
せる遠心力量の差に指向性を与えれば、遠心力は、回転
体を指向方向に推進させる力として利用できる。回転軸
に固定された回転の一部分で、対角線上で反対の向き、
大きさの異なる遠心力を発生させると、回転体は、大き
な遠心力の発生する方向に引かれてゆく。遠心力の大き
さを回転の一部分で変化させるためには、固定された一
部分の対角線上で回転の半径を変化させ、このとき、角
速度を変えなければ、質量×回転半径×角速度の2乗で
得られる遠心力量は回転半径の違いから大きさに差を生
じさせることができる。本発明は、周回軌道を周回運動
する物体(質量)の周回軌道半径を変化させるために軌
道環を設け、周回軌道を周回運動する物体(質量)の角
速度を変化させないために、物体(質量)が半径方向に
摺動できるシリンダーレールを設け、物体(質量)はシ
リンダーレールを設けた輪の回転によって周回運動を行
うようにした。これによって、発生する遠心力量に差を
生じさせ、軌道環を軸の中心に対して角度調整できるよ
う固定することで推進力に指向性と自在性を設けた。対
角線上で発生する大きさの違う遠心力は、密閉された装
置の内側から発生する推進力であり、外部の媒体に作用
する反動ではなく。内蔵するエネルギーの質量変化を伴
う噴射によって得られる反動でもない。When the rotating body rotates, if the masses on the diagonal lines that orbit around the orbit are the same,
A centrifugal force of the same magnitude is generated in the opposite direction on the diagonal line, but if the orbiting object has a different diagonal mass or distance from the center of rotation, the rotating body will be centrifugal due to the difference in mass and radius. Vibrates due to the difference in power. If directivity is given to the difference in the amount of centrifugal force that vibrates the rotating body, the centrifugal force can be used as a force to propel the rotating body in the directional direction. A part of the rotation fixed to the axis of rotation, diagonally opposite direction,
When centrifugal forces of different magnitudes are generated, the rotating body is pulled in a direction in which a large centrifugal force is generated. In order to change the magnitude of the centrifugal force in a part of the rotation, the radius of rotation is changed on the diagonal line of the fixed part. At this time, if the angular velocity is not changed, the square of mass × radius of rotation × angular velocity The amount of centrifugal force obtained can cause a difference in magnitude due to a difference in radius of rotation. The present invention provides an orbital ring for changing the orbital radius of an object (mass) orbiting on an orbit, and an object (mass) for preventing the angular velocity of the object (mass) orbiting on the orbital from changing. Is provided with a cylinder rail that can slide in the radial direction, and the object (mass) performs a revolving motion by rotation of a wheel provided with the cylinder rail. As a result, a difference is generated in the amount of generated centrifugal force, and the orbital ring is fixed so that the angle can be adjusted with respect to the center of the shaft, thereby providing directivity and flexibility in propulsion. The centrifugal forces of different magnitudes generated diagonally are propulsive forces generated from inside the sealed device, not recoil acting on the external medium. It is not a recoil obtained by the injection of the built-in energy accompanied by a mass change.
【発明を解決するための手段】周回軌道を周回運動する
物体(質量)を角速度の変化を伴わない、周回回転半径
の変化、および、周回軌道半径が変化する部位の調整で
きる固定によって、遠心力量に差を生じさせ、また、向
きを調整できる指向性を生じさせたが、遠心力量の差の
合計量を大きくするために、軌道環の大きな円軌道と、
小さな円軌道を周回している物体(質量)の数量を、大
きな円軌道に多く設け、小さな円軌道に少なく設けられ
るような形状を軌道環に設けた。また、物体(質量)の
運動方向の変化が緩やかに行えるよう、直線軌道から円
軌道、円軌道から直線軌道に移行する部位には曲線軌道
を設け、軌道が移行する際に発生する慣性力を対角線上
で互いに打ち消す形状も併せて軌道環に設けた。また、
回転する内輪、外輪、シリンダーレールの回転トルクを
打ち消すために同じ装置を同じ軸を中心に2重反転させ
た。また、そのことによって、発生する推進力をさらに
大きくした。The centrifugal force of an object (mass) that orbits in an orbital orbit is controlled by a change in orbital radius of rotation without a change in angular velocity and an adjustable fixing of a portion where the orbital radius changes. And a directivity that can adjust the direction, but in order to increase the total amount of the difference in the amount of centrifugal force, a large circular orbit of the orbital ring,
A large number of objects (mass) orbiting a small circular orbit are provided in a large circular orbit, and a shape is provided in the orbital ring such that the number of objects (mass) is small in a small circular orbit. In order to change the direction of motion of the object (mass) gently, a curved trajectory is provided at the part that transitions from a linear trajectory to a circular trajectory and from a circular trajectory to a linear trajectory. Shapes that cancel each other on the diagonal are also provided on the orbital ring. Also,
The same device was inverted twice around the same axis to cancel the rotating torque of the rotating inner ring, outer ring, and cylinder rail. In addition, the generated thrust was further increased.
【実施例】図1及び図2に示すよう、上下に、反転する
2つの内輪、外輪、シリンダーレールで構成される回転
体を設け、シリンダーレールには半径方向に摺動する物
体(質量)を設け、上下2つの回転体の間に、回転体が
互いに反転しても、周回運動する物体(質量)は、向き
が反対の同じ周回軌道を通るよう、対象形状をした1つ
の軌道環を設け、軌道環は外枠に沿って角度が調整でき
るよう設け、外枠の構成物に原動機を配置した。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS As shown in FIGS. 1 and 2, a rotating body composed of two reversing inner rings, an outer ring and a cylinder rail is provided up and down, and an object (mass) sliding in the radial direction is provided on the cylinder rail. A single orbital ring having a target shape is provided between the upper and lower two rotating bodies so that even if the rotating bodies are inverted, the object (mass) orbiting along the same orbit in the opposite direction is provided. The orbital ring was provided so that the angle could be adjusted along the outer frame, and the prime mover was arranged on the component of the outer frame.
【発明の効果】遠心力は回転数の2乗に比例して大きく
なるため、回転数によって制御できる推進力量を得られ
る。また、回転数をあげることで大きな推進力が得られ
る。外部に媒体の存在しない場所での推進力として利用
できる。物体(質量)を周回運動させるための原動機
は、回転力が得られるものであれば制約がない。推進力
の向きは、内側から調整でき。推進力は密閉された装置
内で発生する。The centrifugal force increases in proportion to the square of the rotation speed, so that a propulsive force that can be controlled by the rotation speed can be obtained. In addition, a large propulsion force can be obtained by increasing the rotation speed. It can be used as a driving force in places where there is no external media. The prime mover for making the orbital movement of the object (mass) has no limitation as long as a rotational force can be obtained. The direction of the propulsion can be adjusted from the inside. Propulsion occurs in enclosed equipment.
【図1】装置の全体構成を示す正面から見た3層断面図
である。FIG. 1 is a three-layer cross-sectional view showing the entire configuration of a device as viewed from the front.
【図2】装置の全体構成を示す横から見た断面図であ
る。FIG. 2 is a cross-sectional view showing the entire configuration of the apparatus as viewed from the side.
【図3】シリンダーレール、外輪、物体(質量)、軌道
環を表す断面図である。FIG. 3 is a cross-sectional view illustrating a cylinder rail, an outer ring, an object (mass), and a track ring.
【図4】装置の回転体の構成を示す正面図である。物体
(質量)がシリンダーレールに固定されてなく、半径方
向に摺動することを示している。FIG. 4 is a front view showing a configuration of a rotating body of the apparatus. This indicates that the object (mass) is not fixed to the cylinder rail but slides in the radial direction.
【図5】軌道環の形状を示す正面図である。FIG. 5 is a front view showing the shape of a track ring.
【図6】周回運動をしている物体(質量)が発生させて
いる遠心力、慣性力、及び角速度を矢印で示す図であるFIG. 6 is a diagram showing, with arrows, a centrifugal force, an inertial force, and an angular velocity generated by an orbiting object (mass).
1 内輪 2 外輪 3 シリンダーレール 4 物体(質量) 5 軌道環 6 原動機 7 小さな円軌道を周回運動する物体(質量)が発生さ
せる遠心力 8 大きな円軌道を周回運動する物体(質量)が発生さ
せる遠心力 9 物体(質量)の運動方向の変化に伴い発生する慣性
力 10 角速度DESCRIPTION OF SYMBOLS 1 Inner ring 2 Outer ring 3 Cylinder rail 4 Object (mass) 5 Track ring 6 Motor 7 Centrifugal force generated by object (mass) orbiting on a small circular orbit 8 Centrifugal force generated by object (mass) orbiting on a large circular orbit Force 9 Inertial force generated due to change in the direction of movement of the object (mass) 10 Angular velocity
Claims (2)
に復数個設けた、摺動する物体(質量)を周回運動させ
る回転体。周回運動する物体(質量)の周回軌道を、半
径方向に摺動させながら、大きな円軌道と小さな円軌道
を周回運動するよう制御するための、回転体の軸に固定
された、回転体の軸を中心に角度を調整できる軌道環。
上記2つの装備によって、角速度を変化させずに、周回
運動する物体(質量)の回転半径と運動速度を変化さ
せ、対角線上で、発生する遠心力の大きさに差を生じさ
せ、差の生じた遠心力に指向性をもたせる装置。1. A rotating body having a plurality of radially slidable objects (mass) provided on a circumference thereof, wherein the slidable objects (mass) circulate around. The axis of the rotating body fixed to the axis of the rotating body for controlling the orbit of the orbiting object (mass) to orbit around the large and small circular orbits while sliding in the radial direction. Orbital ring whose angle can be adjusted around the center.
The above two devices change the radius of gyration and the speed of movement of the orbiting object (mass) without changing the angular velocity, thereby causing a difference in the magnitude of the generated centrifugal force on the diagonal line, and causing a difference. A device that gives directivity to the centrifugal force.
よって、差の生じた遠心力の向きを自在に変化させ、推
進力の発生する方向を水平方向に制御する装置。2. An apparatus for horizontally changing the direction of the generated propulsion force by freely changing the direction of the generated centrifugal force by means of an orbital ring whose angle can be adjusted about the rotation axis.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP32731799A JP2001107840A (en) | 1999-10-12 | 1999-10-12 | Device for converting centrifugal force into propulsive force |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP32731799A JP2001107840A (en) | 1999-10-12 | 1999-10-12 | Device for converting centrifugal force into propulsive force |
Publications (1)
Publication Number | Publication Date |
---|---|
JP2001107840A true JP2001107840A (en) | 2001-04-17 |
Family
ID=18197800
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP32731799A Pending JP2001107840A (en) | 1999-10-12 | 1999-10-12 | Device for converting centrifugal force into propulsive force |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2001107840A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2003087573A1 (en) * | 2002-04-11 | 2003-10-23 | Btt Co., Ltd. | A method generating coriolis force of noninertial force and inner propulsion method of the closed system using the coriolis force |
-
1999
- 1999-10-12 JP JP32731799A patent/JP2001107840A/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2003087573A1 (en) * | 2002-04-11 | 2003-10-23 | Btt Co., Ltd. | A method generating coriolis force of noninertial force and inner propulsion method of the closed system using the coriolis force |
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