JP2015145675A - Ufo flight device based on flight principle of ufo - Google Patents

Ufo flight device based on flight principle of ufo Download PDF

Info

Publication number
JP2015145675A
JP2015145675A JP2015065193A JP2015065193A JP2015145675A JP 2015145675 A JP2015145675 A JP 2015145675A JP 2015065193 A JP2015065193 A JP 2015065193A JP 2015065193 A JP2015065193 A JP 2015065193A JP 2015145675 A JP2015145675 A JP 2015145675A
Authority
JP
Japan
Prior art keywords
ufo
magnet
flight
force
electrodes
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP2015065193A
Other languages
Japanese (ja)
Other versions
JP2015145675A5 (en
Inventor
瑞穗 新谷
Mitsuo Shintani
瑞穗 新谷
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 JP2015065193A priority Critical patent/JP2015145675A/en
Publication of JP2015145675A publication Critical patent/JP2015145675A/en
Publication of JP2015145675A5 publication Critical patent/JP2015145675A5/ja
Pending legal-status Critical Current

Links

Images

Abstract

PROBLEM TO BE SOLVED: To provide a device that solves disadvantages or defects usually found in rockets for traveling to a universe space, acceleration applied to a human body is high and a space trip for ordinary people is difficult, airplanes have a principal defect that the airplane crashes unless the airplane flies at a speed more than a certain speed, and automobiles have no choice but to run on a road, when traffic density exceeding path capacity occurs, traffic jams may occur.SOLUTION: Means for solving the problem is based on a flight principle of a UFO discovered by the inventor. A structure in which a magnet and a pair of electrodes are fixed is studied. When a discharge is produced between the electrodes in a magnetic field of the magnet, a symmetric property in respect to transmission of force is decayed and a force that is not zero is transmitted to the structure. With this force, the structure performs an acceleration motion. This is a flight principle of a UFO and the structure becomes a flight body to which a UFO flight device based on the flight principle of a UFO is fixed.

Description

この発明は、フレミングの左手の法則から導かれるUFOの飛行原理に基づくUFO飛行装置に関するものである。The present invention relates to a UFO flying device based on the UFO flight principle derived from Fleming's left-hand rule.

UFOの飛行原理は未発見であったので、従来UFO飛行装置は存在しなかった。Since the UFO flight principle was undiscovered, there was no UFO flight device in the past.

UFOについて、科学的若しくは技術的観点から論じられた先行文献はない。There is no prior literature discussing UFO from a scientific or technical point of view.

▲1▼ 従来、宇宙空間に行くためにはロッケットを使っていたが、身体にかかる加速度が大きく、一般人の宇宙旅行は困難であると言う欠点があった。
▲2▼ 飛行機は、ある程度以上の速さで飛行していなければ墜落してしまうと言う原理的な欠陥があった。
▲3▼ 自動車は道路上を走行せざるを得ないので、道路容量を超える交通量が発生した時には渋滞が生じると言う欠点があった。
本発明は、これらの欠点・欠陥を解決する為になされたものである。
(1) Conventionally, a rocket was used to go to outer space, but there was a drawback that it was difficult for ordinary people to travel in space due to the large acceleration applied to the body.
(2) The plane had a fundamental defect that it would crash if it did not fly at a certain speed.
(3) Since automobiles must drive on the road, there is a drawback that a traffic jam occurs when the traffic volume exceeds the road capacity.
The present invention has been made to solve these drawbacks and defects.

課題を解決するための手段は、発明者が見出したUFOの飛行原理に基づくものである。
まず、その原理を紹介する為に、発明者が著した論文を全文引用する。
因みに、この論文は未発表である。
The means for solving the problem is based on the UFO flight principle found by the inventors.
First, in order to introduce the principle, I quoted the full paper of the paper authored by the inventor.
Incidentally, this paper has not been published.

(論文全文掲載)

Figure 2015145675
(以下本文)
UFOの飛行原理
1.はじめに
UFOと言うのは、未確認飛行物体の事であるから、その飛行原理を論じると言う事は、論理的には如何なものかと言う観は否めない。寧ろ、「空飛ぶ円盤等の新しい飛行物体に係る飛行原理」とでも表現すべきであるが、耳目に入り易いと言う事で、敢て、標記の通りの表現とした。
さて、UFOについての話題は、マスコミにも時々取り上げられ、UFOを見たと言う人の情報も掲載されている。
それによると、その飛行の様子は、急発進・急停止・急角度ターン等々だそうである。
しかし、肝心の飛行原理については詳しく紹介されたと言う事は寡聞にして知らない。
未確認飛行物体であるから、それは当然の事と言えば当然の事である。
かねてより人類が想像してきた空飛ぶ円盤と言う未来の新しい乗り物を作り出すためには、この原理を解明する必要がある。
又、それは、人類の一つの夢でもあると思う。
幸運にも、筆者はこの原理を見出した。それを、以下に示す。
2.相異なる二つの条件下に於けるフレミングの左手の法則の適用
Figure 2015145675
磁石J(磁石の形状は問わない。)と導
Figure 2015145675
とならないような位置関係で、図1のように構造体
ABCD‐EFGHの(構造体の役割は、磁石と導線との相対的な位置関係を固定する事であるから、形状は問わない。また、構造体は磁石や導線等に対して電磁気的な影響を与える事がないように配慮されているものとする。)点P,Q,U,Vの位置で固定するものとする。ここでは、磁石を棒状の磁石であると仮定している。また、点U及び点Vは、UV間に電流を流す事が出来るように、電源に繋がっているものとする。
Figure 2015145675
2−1.導線に電流を流した場合
棒状の磁石JのN極・S極がそれぞれ点P・点Qに位置している場合、UからVに向け
Figure 2015145675
磁石及び導線は、構造体ABCD‐EFGHに固定されているので、磁石及び導線に作用する力は、それぞれを固定している点P,Q及び点U,Vを介して構造体に伝達される。
Figure 2015145675
は加速度運動をしない。
2−2.導線Lを設置せずに、電極U,V間で放電を起こした場合
図2に於いて、電気を電極Uから電極Vに向けて放電させた場合、電子はVからUに向って空中を飛ぶ。電子は、磁石Jの影響を受けて磁石に近付く向きに曲げられて飛ぶから、首尾よく放電を起こさせるために、電極U及び電極Vは電子の軌道の曲がりを考慮して、位置や大きさを決める必要がある。
電子の流れが磁石から受ける力は、フレミングの左手の法則
Figure 2015145675
この電子の流れが作る磁界が磁石Jに及
Figure 2015145675
Figure 2015145675
磁石Jは点P,Qで固定されているので、
Figure 2015145675
点P,Qを介して構造体ABCD‐EFGHに伝達される。
一方、放電を起こすVU間を移動する
Figure 2015145675
事は出来ない。
何故なら、UV間を繋ぐ物体(導線)は存在せず、電子は空中を飛んでいるからである。
Figure 2015145675
みが伝達される。
それ故、図2に示すように、構造体ABCD‐EFGHに磁石J及び電極U,Vを固定し、電
Figure 2015145675
3.UFOの飛行原理とUFO飛行装置
Figure 2015145675
電極間で放電を起こすものとする。(磁石が棒状の磁石であるならば、例えば図2に示すようになる。)
放電により空間を飛ぶ電子は、磁石が作る磁界から力を受け、曲線運動を行なう。しかし、電子が受けている力は、電子が空間を飛んでいるが故に構造体には伝達されない。
然るに、磁石も運動する電子が作る磁界から力を受けるが、この力は、磁石を固定している点を介して構造体に伝達される。
電極間が導線で繋がれておれば、磁石が受ける力と導線の中を走る電子が受ける力(導線が受ける力)とは、それぞれが共に構造体に伝達されるが、導線を設置せずに放電と言う方法を用いた場合、空間を飛ぶ電子が受ける力の方は構造体には伝達されない。
以上を要約する。
Figure 2015145675
考える。その構造体の磁界の中に於いて電極間で放電を起こすと、力の伝達に係る対称性が崩れ、構造体には零でない力が伝達される。」
この力により、構造体は加速度運動を行なう。
これが、UFOの飛行原理である。
そして、この構造体が、UFOの飛行原理に基づくUFO飛行装置である。
4.UFOの作成
飛行させたい物体に(形状は問わない。)UFO飛行装置取り付ければ、UFOの基本的な部分は完成である。
因みに、UFO本体の構造、電力供給の問題、飛行制御の方法等、工学上のテーマについては、稿を改めて考察すべき事柄である。
さて、UFO全体の質量をMとする。
Figure 2015145675
磁石を電磁石とするならば、
Figure 2015145675
ここに、k:比例定数。
Figure 2015145675
Figure 2015145675
この時、UFOは、地球の重力に打ち勝って、g以上の加速度で上昇する事が出来る。
尚、この飛行装置は、水密性を確保しておけば、海中・水中でも使用可能である。
5.おわりに
地球と月の間の距離は約380000kmである。
地球から月までを、ここで提案したUFOで行くものとする。中間地点まではgで加速し、それ以降はgで減速し、月には速度0で着陸するものとする。
中間地点までに要する時間tは、
Figure 2015145675
よって、往復に要する時間は、約7時間であり、月旅行は日帰りが可能となる。
尚、加減速がgであるから、身体的負担はないものと思われる。
(引用終わり)(Full paper published)
Figure 2015145675
(The text below)
UFO flight principle Introduction UFO is an unidentified flying object, so we can not deny that it is logical to discuss the flight principle. On the contrary, it should be expressed as “flight principle relating to a new flying object such as a flying saucer”, but because it is easy to get into the ears, it was intentionally expressed as shown.
Now, topics about UFO are sometimes taken up by the media, and information about people who have seen UFO is also posted.
According to it, the state of the flight seems to be sudden start, sudden stop, steep angle turn, and so on.
However, I don't know that it was introduced in detail about the essential flight principle.
Since it is an unidentified flying object, it is natural that it is natural.
It is necessary to clarify this principle in order to create a new vehicle of the future called the flying saucer that human beings have long imagined.
I think that is also a human dream.
Fortunately, the author found this principle. This is shown below.
2. Application of Fleming's left-hand rule under two different conditions
Figure 2015145675
Magnet J (magnet shape does not matter) and lead
Figure 2015145675
As shown in FIG. 1, the structure ABCD-EFGH (the role of the structure is to fix the relative positional relationship between the magnet and the conducting wire, and the shape is not limited. The structure shall be considered so as not to have an electromagnetic influence on the magnet, the conducting wire, etc.) It shall be fixed at the positions of points P, Q, U and V. Here, it is assumed that the magnet is a rod-shaped magnet. Further, it is assumed that the points U and V are connected to a power source so that a current can flow between the UVs.
Figure 2015145675
2-1. When a current is passed through the conductor When the north and south poles of the rod-shaped magnet J are located at points P and Q, respectively, from U to V
Figure 2015145675
Since the magnet and the conducting wire are fixed to the structure ABCD-EFGH, the forces acting on the magnet and the conducting wire are transmitted to the structure via the points P and Q and the points U and V that fix the magnet and the conducting wire, respectively. .
Figure 2015145675
Does not accelerate.
2-2. When a discharge is caused between the electrodes U and V without installing the lead wire L In FIG. 2, when electricity is discharged from the electrode U to the electrode V, the electrons move from V to U in the air. jump. Electrons are bent and fly in the direction approaching the magnet under the influence of the magnet J, so that the electrode U and the electrode V are positioned and sized in consideration of the bending of the electron trajectory in order to cause a successful discharge. It is necessary to decide.
The force that the electron flow receives from the magnet is the Fleming's left-hand rule
Figure 2015145675
The magnetic field created by this electron flow reaches magnet J.
Figure 2015145675
Figure 2015145675
Since magnet J is fixed at points P and Q,
Figure 2015145675
It is transmitted to the structure ABCD-EFGH via points P and Q.
On the other hand, it moves between VUs that cause discharge
Figure 2015145675
I can't do that.
This is because there is no object (conductive wire) connecting the UVs, and electrons are flying in the air.
Figure 2015145675
Is transmitted.
Therefore, as shown in FIG. 2, the magnet J and the electrodes U and V are fixed to the structure ABCD-EFGH.
Figure 2015145675
3. UFO flight principle and UFO flight equipment
Figure 2015145675
It shall cause discharge between the electrodes. (If the magnet is a rod-shaped magnet, for example, as shown in FIG. 2)
Electrons flying in the space by electric discharge receive a force from the magnetic field generated by the magnet and perform a curved motion. However, the force received by the electrons is not transmitted to the structure because the electrons fly through the space.
However, the magnet also receives a force from the magnetic field created by the moving electrons, but this force is transmitted to the structure via the point fixing the magnet.
If the electrodes are connected by a conducting wire, the force received by the magnet and the force received by the electrons running inside the conducting wire (the force received by the conducting wire) are both transmitted to the structure, but the conducting wire is not installed. When the method of discharging is used, the force received by the electrons flying in the space is not transmitted to the structure.
The above is summarized.
Figure 2015145675
Think. When a discharge occurs between the electrodes in the magnetic field of the structure, the symmetry relating to the force transmission is lost, and a non-zero force is transmitted to the structure. "
With this force, the structure performs an acceleration motion.
This is the UFO flight principle.
This structure is a UFO flying device based on the UFO flight principle.
4). Creation of UFO The basic part of UFO is completed when the UFO flying device is attached to the object to be flying (regardless of the shape).
Incidentally, engineering themes such as the structure of the UFO body, power supply problems, flight control methods, etc. are matters that should be considered again.
Now, let M be the mass of the entire UFO.
Figure 2015145675
If the magnet is an electromagnet,
Figure 2015145675
Where k is a proportionality constant.
Figure 2015145675
Figure 2015145675
At this time, the UFO can overcome the gravity of the earth and rise with an acceleration of g or more.
This flying device can be used underwater or underwater as long as water tightness is ensured.
5. Conclusion The distance between the earth and the moon is about 380000 km.
Let's go from the earth to the moon with the proposed UFO. It is assumed that the vehicle will accelerate at g to the middle point, decelerate at g after that, and land at zero speed on the moon.
The time t required to reach the intermediate point is
Figure 2015145675
Therefore, the time required for the round trip is about 7 hours, and the monthly trip can be a day trip.
In addition, since acceleration / deceleration is g, it seems that there is no physical burden.
(End of quotation)

以下に、引用論文の一部を再掲する。

Figure 2015145675
て考える。その構造体の磁界の中に於いて電極間で放電を起こすと、力の伝達に係る対称性が崩れ、構造体には零でない力が伝達される。」
この力により、構造体は加速度運動を行なう。
これが、UFOの飛行原理である。
そして、この構造体が、UFOの飛行原理に基づくUFO飛行装置である。Below are some of the cited papers.
Figure 2015145675
Think. When a discharge occurs between the electrodes in the magnetic field of the structure, the symmetry relating to the force transmission is lost, and a non-zero force is transmitted to the structure. "
With this force, the structure performs an acceleration motion.
This is the UFO flight principle.
This structure is a UFO flying device based on the UFO flight principle.

Figure 2015145675
の電極とが固定された構造体(構造体の役割は、磁石と電極との相対的な位置関係を固定する事であるから、形状は問わない。また、構造体は磁石や電極に対して電磁気的な影響を与える事がないように配慮されているものとする。)であって、これらの電極間で放電を起こす事が出来るように作成された構造体は、UFOの飛行原理に基づくUFO飛行装置である。
Figure 2015145675
Figure 2015145675
(The role of the structure is to fix the relative positional relationship between the magnet and the electrode, so the shape does not matter. It is assumed that there is no electromagnetic influence.) The structure created so that discharge can occur between these electrodes is based on the flight principle of UFO. UFO flight device.
Figure 2015145675

UFO飛行装置を、飛行させようとする飛行体に取り付ける事により課題が解決する。
何故なら、この飛行体は適当な大きさの電流を供給すれば、地球の重力に打ち勝って加速度運動をする事が出来るからである。
本発明は、以上の構成よりなるUFO飛行装置である。
The problem is solved by attaching the UFO flying device to the flying object to be caused to fly.
This is because the aircraft can overcome the gravity of the earth and perform acceleration motion if it supplies a current of an appropriate magnitude.
The present invention is a UFO flying device configured as described above.

本発明によるUFO飛行装置を、円盤に取り付ければ、所謂UFOが実現する。If the UFO flying device according to the present invention is attached to a disk, a so-called UFO is realized.

このUFOは、引用論文にあるように、適当な大きさの電流を供給すれば、地球の重力に打ち勝ってg以上の加速度で上昇する事が出来る。加減速の加速度を身体的に負担がないと考えられるgとしても、日帰りの月旅行が可能となる。As described in the cited paper, this UFO can rise at an acceleration of g or more by overcoming the gravity of the earth if an appropriate current is supplied. Even if the acceleration of acceleration / deceleration is assumed to have no physical burden, a day trip to the moon is possible.

UFOの実現により、飛行機の失速による墜落と言う悲劇は避ける事が出来るようになる。The realization of UFO makes it possible to avoid the tragedy of crashes caused by airplane stalls.

気象観測衛星等の人工衛星は、ロケットで打ち上げるのではなく、宇宙空間の必要な場所にUFOで置きに行く事となる。Artificial satellites such as meteorological observation satellites will not be launched by rockets, but will be placed by UFO at necessary places in outer space.

自動車用の車体にUFO飛行装置を取り付ければ、空飛ぶ自動車が実現する。これの通路としては、従来のような道路ではなく空間に通行帯を設定するだけでよく、その容量は幾らでも大きく設定する事が出来るから、交通渋滞は発生しない。
又、超高速移動(gで加減速すれば1000km離れた地点に約5分で行く事が出来る。)が可能となるから、大都市への過度の集中の必然性はなくなる。
If a UFO flying device is attached to the body of an automobile, a flying car can be realized. As a passage for this, it is only necessary to set a traffic zone in a space rather than a conventional road, and the capacity can be set as large as possible, so traffic congestion does not occur.
In addition, since it is possible to move at a very high speed (accelerating and decelerating with g, it is possible to go to a point 1000 km away in about 5 minutes), so there is no need for excessive concentration in a big city.

棒状の磁石を用いた場合の本発明の一例としての斜視図である。 棒状の磁石を用いた場合の本発明の一例としての平面図である。 棒状の磁石を用いた場合の本発明の一例としての正面図である。 棒状の磁石を用いた場合の本発明の一例としての側面図である。尚、磁石の形状は問わないから、磁石は必ずしも棒状である必要はない。 It is a perspective view as an example of this invention at the time of using a rod-shaped magnet. It is a top view as an example of this invention at the time of using a rod-shaped magnet. It is a front view as an example of this invention at the time of using a rod-shaped magnet. It is a side view as an example of this invention at the time of using a rod-shaped magnet. In addition, since the shape of a magnet is not ask | required, a magnet does not necessarily need to be rod-shaped.

以下、本発明を実施するための形態について説明する。

Figure 2015145675
の役割は、磁石と電極との相対的な位置関係を固定する事であるから、形状は問わない。また、構造体は磁石や電極に対して電磁気的な影響を与える事がないように配慮されているものとする。)固定する。
Figure 2015145675
▲2▼ 構造体に固定された電極は、電極間で放電を起こす事が出来るように電源に接続する。電極間での放電は構造体に固定された磁石による磁界の中で起こるから、この構造体はUFOの飛行原理を満足する。
従って、この構造体は、UFO飛行装置である。
▲3▼ 別の表現をすると、「UFOの飛行原理に基づくUFO飛行装置を作成するには、磁
Figure 2015145675
(ii)電極間で放電を起こす事が出来る、構造体を作成すればよい。」と言う事である。
▲4▼ 尚、放電現象が生じる電極間が真空であるか否かは、UFOの飛行原理にとっては本質的な問題ではない。
本発明は、以上の構成からなるUFOの飛行原理に基づくUFO飛行装置である。Hereinafter, modes for carrying out the present invention will be described.
Figure 2015145675
Since the role of is to fix the relative positional relationship between the magnet and the electrode, the shape is not limited. In addition, the structure is considered so as not to have an electromagnetic influence on the magnet and the electrode. ) Fix.
Figure 2015145675
{Circle around (2)} The electrodes fixed to the structure are connected to a power source so that discharge can occur between the electrodes. Since the discharge between the electrodes occurs in a magnetic field generated by a magnet fixed to the structure, this structure satisfies the UFO flight principle.
Therefore, this structure is a UFO flying device.
(3) In other words, “To create a UFO flying device based on the UFO flight principle,
Figure 2015145675
(Ii) What is necessary is just to produce the structure which can cause discharge between electrodes. Is to say.
(4) It should be noted that whether or not the space between the electrodes where the discharge phenomenon occurs is a vacuum is not an essential problem for the UFO flight principle.
The present invention is a UFO flying device based on the UFO flight principle having the above-described configuration.

1 構造体に固定されている磁石。
磁石の形状は問わないので、磁石は必ずしも棒状である必要はない。
2 磁石を固定する構造体上の点。磁石に働く力はこの点を介して構造体に伝わる。
棒状の磁石の場合は、この点の位置で例えば磁石のN極を固定する。
3 磁石を固定する構造体上の点。磁石に働く力はこの点を介して構造体に伝わる。
棒状の磁石の場合は、この点の位置で例えば磁石のS極を固定する。

Figure 2015145675
れが固定されておればよく、しかも磁石の形状は問わないから、磁石のN極・S極は構造体上の点2・点3の位置に必ずしも存在する必要はない。
4 構造体に固定されている電極。
5 構造体に固定されている電極。
6 構造体。
ここでは、構造体を便宜上蓋と底の無い六面体(六面体状)として表現しているが、構造体の役割は磁石と電極との相対的な位置関係を固定する事であるから、その形状は問わない。従って、構造体は六面体状である必要はない。
7 電源と構造体に固定されている電極とを繋ぐ電線。
8 電源と構造体に固定されている電極とを繋ぐ電線。
9 電極間に於いて放電を起こさせる事が出来る能力を有する電源。1 Magnet fixed to the structure.
Since the shape of the magnet does not matter, the magnet does not necessarily have a rod shape.
2 A point on the structure that fixes the magnet. The force acting on the magnet is transmitted to the structure through this point.
In the case of a rod-shaped magnet, for example, the N pole of the magnet is fixed at this point.
3 Points on the structure to fix the magnet. The force acting on the magnet is transmitted to the structure through this point.
In the case of a rod-shaped magnet, for example, the S pole of the magnet is fixed at this point.
Figure 2015145675
Since it is only necessary to fix this, and the shape of the magnet does not matter, the N and S poles of the magnet do not necessarily exist at the positions of points 2 and 3 on the structure.
4 Electrode fixed to the structure.
5 Electrode fixed to the structure.
6 Structure.
Here, the structure is expressed as a hexahedron without a lid and bottom for convenience (hexahedral shape), but since the role of the structure is to fix the relative positional relationship between the magnet and the electrode, the shape is It doesn't matter. Therefore, the structure does not need to be hexahedral.
7 Electric wires that connect the power supply and the electrodes fixed to the structure.
8 Electric wires that connect the power source and the electrodes fixed to the structure.
9 A power supply capable of causing discharge between electrodes.

Claims (1)

磁石及び対をなす電極が取り付けられた物体であって、それらの電極間で放電が可能なもの。An object to which a magnet and a pair of electrodes are attached, and discharge is possible between these electrodes.
JP2015065193A 2015-03-10 2015-03-10 Ufo flight device based on flight principle of ufo Pending JP2015145675A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2015065193A JP2015145675A (en) 2015-03-10 2015-03-10 Ufo flight device based on flight principle of ufo

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2015065193A JP2015145675A (en) 2015-03-10 2015-03-10 Ufo flight device based on flight principle of ufo

Publications (2)

Publication Number Publication Date
JP2015145675A true JP2015145675A (en) 2015-08-13
JP2015145675A5 JP2015145675A5 (en) 2018-03-22

Family

ID=53890006

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015065193A Pending JP2015145675A (en) 2015-03-10 2015-03-10 Ufo flight device based on flight principle of ufo

Country Status (1)

Country Link
JP (1) JP2015145675A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2018096361A (en) * 2016-12-08 2018-06-21 素明 依田 Ufo floating method engine

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0874731A (en) * 1994-09-07 1996-03-19 Ishikawajima Harima Heavy Ind Co Ltd Propulsion device for space craft
JP2003139044A (en) * 2001-11-01 2003-05-14 Mitsubishi Electric Corp Ion thrustor
JP2005036717A (en) * 2003-07-14 2005-02-10 National Aerospace Laboratory Of Japan Ion engine having thrust direction control mechanism
JP2007506016A (en) * 2003-09-15 2007-03-15 カサル テクノロジエントビックルング ゲゼルシャフト ミット ベシュレンクテル ハフトゥング Method and apparatus for generating Alfven waves
JP2009085206A (en) * 2007-09-13 2009-04-23 Tokyo Metropolitan Univ Charged particle emission device and ion engine
US20120137652A1 (en) * 2005-10-07 2012-06-07 Asprey Margaret W Electromagnetic Thrust System
JP2014194220A (en) * 2014-06-12 2014-10-09 Elwing Llc Thruster and thrust-generating process

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0874731A (en) * 1994-09-07 1996-03-19 Ishikawajima Harima Heavy Ind Co Ltd Propulsion device for space craft
JP2003139044A (en) * 2001-11-01 2003-05-14 Mitsubishi Electric Corp Ion thrustor
JP2005036717A (en) * 2003-07-14 2005-02-10 National Aerospace Laboratory Of Japan Ion engine having thrust direction control mechanism
JP2007506016A (en) * 2003-09-15 2007-03-15 カサル テクノロジエントビックルング ゲゼルシャフト ミット ベシュレンクテル ハフトゥング Method and apparatus for generating Alfven waves
US20120137652A1 (en) * 2005-10-07 2012-06-07 Asprey Margaret W Electromagnetic Thrust System
JP2009085206A (en) * 2007-09-13 2009-04-23 Tokyo Metropolitan Univ Charged particle emission device and ion engine
JP2014194220A (en) * 2014-06-12 2014-10-09 Elwing Llc Thruster and thrust-generating process

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2018096361A (en) * 2016-12-08 2018-06-21 素明 依田 Ufo floating method engine

Similar Documents

Publication Publication Date Title
ES2709423T3 (en) Thrust motor of charged particles
US7413149B2 (en) Wing enhancement through ion entrainment of media
Eckman The Competence-Performance Issue in Second-Language Acquisition Theory: A Debate: ISSUE
KR20150089898A (en) Amphibious flying car
JP2015145675A (en) Ufo flight device based on flight principle of ufo
Büchner et al. The separatrix tentacle effect of ion acceleration to the plasma sheet boundary
Kosyakov Radiation in electrodynamics and in Yang–Mills theory
RU2646711C1 (en) Space vehicle
CN109941461A (en) A kind of magnetic control angle of divergence electric propulsion device
De Keyser et al. Auroral and sub-auroral phenomena: an electrostatic picture
Katsurayama et al. DSMC Simulation of Electrodynamic Aerobraking on a Reentry Capsule in a Hypersonic Rarefied Regime
JP6693967B2 (en) Hall effect thruster
Fujii et al. A proposed bare-tether experiment on board a sounding rocket
Vasyliunas Large-scale morphology of the magnetosphere
Goertz The role of planetary satellites in magnetospheric processes
JP2021126908A (en) Space debris removal apparatus
RU2333385C2 (en) Method of creating jet thrust
Fontanes Molina et al. Experimental study of the charge saturation levels of an aircraft with an active electrostatic charge control system
Mahajan Hyperlop Transportation System
GB2588415A (en) An apparatus for generating a force
Triger et al. A method and system for braking of flying objects
KR20160080735A (en) Aerodynamic Noise Reduction Structure at High Reynolds Number Zone
Voitcu et al. Electron and ion velocity distribution functions across one-dimensional tangential discontinuities: particle-in-cell simulations
Matsoukas et al. Experimental Investigation of Asymmetrical Capacitors for Electric Propulsion
Treumann et al. Downward auroral currents from the reconnection Hall-region

Legal Events

Date Code Title Description
A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20180115

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20180211

A871 Explanation of circumstances concerning accelerated examination

Free format text: JAPANESE INTERMEDIATE CODE: A871

Effective date: 20180226

A975 Report on accelerated examination

Free format text: JAPANESE INTERMEDIATE CODE: A971005

Effective date: 20180330

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20180410

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20180527

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20180807

A02 Decision of refusal

Free format text: JAPANESE INTERMEDIATE CODE: A02

Effective date: 20181120