WO2014061759A2 - System for space propulsion and staying in space (staying in above-stratosphere air) - Google Patents
System for space propulsion and staying in space (staying in above-stratosphere air) Download PDFInfo
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- WO2014061759A2 WO2014061759A2 PCT/JP2013/078241 JP2013078241W WO2014061759A2 WO 2014061759 A2 WO2014061759 A2 WO 2014061759A2 JP 2013078241 W JP2013078241 W JP 2013078241W WO 2014061759 A2 WO2014061759 A2 WO 2014061759A2
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- 239000005437 stratosphere Substances 0.000 title claims 2
- 239000003380 propellant Substances 0.000 claims abstract description 15
- 238000000034 method Methods 0.000 claims description 9
- 230000001141 propulsive effect Effects 0.000 claims description 4
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
- F03G7/00—Mechanical-power-producing mechanisms, not otherwise provided for or using energy sources not otherwise provided for
- F03G7/10—Alleged perpetua mobilia
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/40—Arrangements or adaptations of propulsion systems
- B64G1/409—Unconventional spacecraft propulsion systems
Abstract
[Problem] To universally realize a space structure (such as a space elevator) to which particular spacecraft, having significantly better propulsion efficiency than solar sail boats and not using rocket fuel (that is disposable and expensive), and the power units (continuous-perpetual airflow circulation) of such models have been applied. [Solution] Firstly, as shown, for example, in figure 1 and figure 2, in particular, propulsion bodies (two bodies having different shapes) are prepared, the propulsion bodies having applied thereto the pressure difference and wind pressure acting on both ends, and being moved by the wind pressure from a ducted fan. Sequentially, the two bodies (applying dynamic lift or the like acting on the vicinity of a hollow part of the inside the machine), without action and reaction forces canceling each other out, and moreover, and with the propellant (simply air gas) blown from one among the bodies being accepted (in-taken), without any spare, by another receiving body, move close together (closest together) overall, and are moved in parallel...etc.
Description
本発明は、概して、宇宙関連機器類の推進技術云々に関するものである。
The present invention generally relates to a propulsion technique for space-related equipment.
前述の宇宙航空機体（宇宙航空部品）の製法（技法）分野に準じる。
According to the manufacturing method (technique) field of the above-mentioned spacecraft body (aerospace parts).
尚、本推進剤を見当している主要な（圧縮）空気類の準用に関しては、無論、既存のロケット燃料の威力よりも劣る推力云々故、従前より、既定の様々な宇宙推進システムにかけて、ほとんど皆無ながら、とりわけ、当該船体（結合体）自体、その空気力（同体の静止上の慣性力よりも大きい風力）を持続的にも大いに利用する（ダクテッド）ファン類等の推進力を応用した技法云々を相可能な限り、採用する。
Of course, with regard to the application of the major (compressed) airs that have found this propellant, of course, the thrust is inferior to the power of existing rocket fuel. A technique that applies propulsive force such as ducted fans that utilize the hull (combined body) itself and its aerodynamic force (wind power larger than the static inertial force of the same body) in a sustained manner. Adopt as much as possible.
注：（請求項３等の局所的にも閉じた系に関し）従前より、「外力が加わらない限り、質点は、その運動（静止）状態を維持し、運動量は保存される」という運動の第一法則・運動量保存則等に則って、観照上、当の物体（質点）を動かすには、ぜがひでも、さしたる外力（推力）とならん、推進剤（空気ガス等）を外部（宇宙船外）の方へ噴出させなければならない・・などという既成概念的な考え方のもと、目下、以下の通りの（準）閉鎖系の中空式物体内に於いて、当の推進剤を外部に放出しない内圧（風圧）差云々を応用した推進システムなど、ほとんど無いのが実状であるが、関連事件の国際調査機関の見解により指摘された、ほんの数件の類似システムを下記の先行技術文献の項目に補足的に記載するものの、如何せん、それ等の特異な方法をもってしても、依然として、主要な向心力に相対した遠心力等がかかってしまい、それほど、実用性のある推進効果が生じるものではないと言っても過言ではない・・・云々。
Note: (Regarding a locally closed system such as claim 3) From the past, as long as no external force is applied, the mass will maintain its motion (stationary state) and the momentum will be preserved. In order to move the object (mass point) for observing according to the law of conservation of momentum and the law of momentum, the propellant (air gas, etc.) is applied to the outside (spacecraft) in addition to the external force (thrust), even if it is a crack. Based on the existing conceptual idea that it must be ejected to the outside), the propellant is currently placed outside in the (quasi) closed hollow body as shown below. There are almost no propulsion systems that apply internal pressure (wind pressure) differences that do not release, but there are only a few similar systems that have been pointed out by the opinion of international search organizations in related cases. Although it is described in the item as supplementary, Even with a peculiar way, still, it takes a centrifugal force or the like relative to the major centripetal force, so, practical use of a propulsion effect is not what occurs to say it is not too much to ... so and so.
専ら、（使い捨てで高価な）ロケット燃料を要さず、太陽帆船等よりも数段、推進効率のよい（剰え、繰り返し使え、尚安価な推進剤を利用した）宇宙船類及びその（気流循環式）動力部等を複合的にも応用した関連上等の宇宙構造物云々を普く実現化させる。
Spacecraft and its (air circulation) that do not require rocket fuel (disposable and expensive), are more efficient than solar sailing ships, etc., have better propulsion efficiency (use surplus, reusable, and cheaper propellant) Formula) Commonly realized space structures such as related parts that apply power parts etc. in a complex manner.
先ず、本推進剤用の主なる（圧縮）空気類を外部（宇宙船外）の方へ噴出させる、通気（排気）孔等付の中空式物体にして、概ね、図１に相対しては、図２等の様に、形状云々の違うものを２体系（A体系とB体系）、個別に準備し、順次、一方の A体系のものに関しては、少なくとも、湾曲状の（エア）チューブ壁面にかかる、気流上の反作用力（反推進力）が分散される所以から、所定のファン類のブレードから吹き出される空気力（推進力）が尚勝り、且つ又、所定の偏向板類を効果的に付することにより、当該船体自体、少なからず、推進方向への移動を確実なものと為し、且つ又、もう一方の B体系のものについては、特段、対をなす各ファン類（符号C3とC4及びC5とC6）同士が、ちょうど、同出力にて、力のつり合いを保ち続けつつ、メイン（中央部付近）のダクテッドファン類の推進力が効果的に作用し、更に、特殊回転体による角運動保存則により、それほど、後進力が掛からないことなどから、さほど、推進可能な両体（A体とB体）を（同速度にて）適度に連動させつつ、必要なら、宇宙飛行上の位置センサー等を調整しながら、各体を（最）接近させれば、B体の射出部から吹き出される（圧縮）空気ガスの受け皿として、A体系の受容体自体、さしたる気体を受け止めながら、気流循環させつつ、尚のこと、A体とB体等が、いみじくも作用反作用云々で打ち消し合うことなく、両体とも移動し得るようになり、以て、なお端的に言えば、本推進体同士を同期（同調）的にも（準）結合化させながら、（各ファン類の風量等の調整機器類や機体付属の姿勢制御装置等を駆使しつつ、必要に応じて、空気を吸込む吸引口付き等の回収エアタンク類等を補完的にも併設して付け足しながら）適程に平行移動させればよい・・・云々。
First of all, the main (compressed) air for this propellant is blown out to the outside (outside the spacecraft) and is made into a hollow object with ventilation (exhaust) holes, etc. As shown in Fig. 2 and so on, two systems (A system and B system) with different shapes are prepared separately, and one of the A systems has at least a curved (air) tube wall surface. Since the reaction force (anti-propulsive force) on the airflow is dispersed, the aerodynamic force (propulsive force) blown from the blades of the predetermined fans is still superior, and the predetermined deflecting plates are effective. In particular, the hull itself is sure to move in the propulsion direction, and for the other B system, each pair of fans (symbols) C3 and C4 and C5 and C6) keep the balance of power at the same output. Both main body (near the center) ducted fans act effectively, and due to the conservation of angular motion by a special rotating body, the reverse force is not applied so much. (A body and B body) are linked appropriately (at the same speed), and if necessary, adjusting each position sensor on the space flight, etc. As a receiving tray for (compressed) air gas blown out from the part, the A system receptor itself, receiving the gas of interest, circulating the air flow, while the A body and B body, etc., cancel each other with an action and reaction. Both bodies can move without matching, so to put it simply, while this propulsion body is coupled (synchronously) with each other (synchronously), Adjustment devices and attitude control devices attached to the aircraft Use and while, if necessary, while afterthought on site to air sucked suction port with such complementary collected air tank, etc.) of or ... so and so that is moved parallel to the extent applicable.
尚、A体等の動力上の形態云々を補足して言えば、一種、スラストリバーサ（逆推力装置）風の機器類の性能のごとく、さほど、後進力（反推進力）がかかり、当該機種自ら、それ相応に減速したとしても、少なからず、前進し得る為、上述の通り、さしたるA体等（及びそれ等の合体物）とも、宇宙航行に於いては、なお有効的に推進可能である。
In addition, to supplement the form of power, such as the A body, the reverse model (reverse thrust device) wind, like the performance of equipment, the reverse force (anti-propulsive force) is applied, the model concerned Even if you decelerate accordingly, you can move forward a little, so as described above, you can still effectively propel the A body (and their union) as well as in space navigation. is there.
更に注釈して言えば、閉じた系に関し、肝要的にも、本宇宙推進システムに於ける力学上の注目物体を本船体（金属体）と気体（空気）の合体物（図１１の様な一物体）とみなして、所定の推進ファン等にかかる空気力等を内力とした場合、その内力の性質（作用反作用の関係）上、とりわけ、同上ファンと空気間で働く内力の合力が０とならなければならない。
In addition, for the closed system, the important object of dynamics in this space propulsion system is the combined body of the hull (metal body) and gas (air) (as shown in FIG. 11). If the aerodynamic force applied to a given propulsion fan is an internal force, the internal force acting between the fan and the air is 0 in particular due to the nature of the internal force (relationship between action and reaction). Must be.
しかしながら、一応、そう断定してしまえば、実質的にも、ファン稼働による気体の流れ（空気の圧力）が、尚も、その物質（空気粒子）ある限り、船内のエアタンクや空気配管等へと通じる空気の通り道のあらゆる内面に作用し得る（し続ける）にも関わらず、さして、内力自体、０、即ち、消えてなくなる力と断固、既定している以上、当の物質（空気粒子）自ら、あろうことか、幽霊化しつつ、何ら、（他の）あらゆる面に、作用を及ぼし得ない・・・などという不条理（不合理）な結果と相成ってしまうとも考えられる。
However, once determined, the flow of air (air pressure) due to the operation of the fan will continue to the air tank and air piping in the ship as long as the substance (air particles) is still present. Despite being able to act on (and continue to) any inner surface of the air passage that leads to it, the internal force itself, zero, that is, the force that disappears, is determined. It may be ghostly, but it is combined with an absurd (irrational) result that it cannot act on any other aspect.
従ってそれ故、たとえ、さしたる（圧縮）空気が、さほど、閉鎖系の物体の内部（閉曲面に囲まれた中空部）にあろうとも、船体（固体）と気体は、もともと、別個（別状）の物体の為、その一方の物体（物質）による空気力を内力とせず、運動方程式（第一法則）上等の外力とみなすべきである。
Therefore, the hull (solid) and the gas are originally separate (separate), even if the (compressed) air is so much inside the closed system body (hollow part surrounded by the closed curved surface). Therefore, the aerodynamic force of one object (material) should not be regarded as an internal force, but should be regarded as an external force on the equation of motion (first law).
要するに、本宇宙推進システムの場合、当該物体（宇宙船体）を動かす推進剤（圧縮空気）が、たとえ、船内にあろうとも、それは、注目・着目すべき同上物体（金属体）から見れば、外力に相当し、その結果、運動方程式により、同体にかかる静止上の慣性力よりも大きい力（風力）を与えれば、無論、同物体自ら、適度に移動しなければならず、ましてや、所定の宇宙船内を非圧縮性の水などでなく、圧縮性のある（付属の空気圧縮機により、気圧を変えられる）空気類で賄う限り、殊の外、パスカルの原理等々に悪影響しないことなどを念のため、補足的に追記しておく
In short, in the case of this space propulsion system, even if the propellant (compressed air) that moves the object (space hull) is in the ship, It corresponds to an external force, and as a result, if a force (wind force) greater than the stationary inertial force applied to the same body is given by the equation of motion, the same object itself must move moderately. As long as the spacecraft is covered not only with incompressible water but with air that is compressible (the air pressure can be changed by the attached air compressor), it should be noted that it will not adversely affect the Pascal principle. For this reason, add a supplementary note
再追記として、観照上、当の合体版では、さして閉鎖系につき、運動エネルギーが熱エネルギーに変換され、それほど、推進力が生じないのでは？・・という既定の高察があるものの、如何せん、物理法則上、ある系に外部から力が加わらない限り、その系の運動量の総和は不変という運動量保存則のもとでは、そもそも、外部からの力が働かない事例として、物体の衝突問題が挙げられ、専ら、その一例の完全弾性衝突以外、物体の運動エネルギーは保存されない、と既定されており、以て、本案件の衝突の対象物（本物体と気体・空気）など、いみじくも完全弾性衝突でない為、さしたる保存則が効かず、従ってそれ故、当の内圧差を利用した推進システムにかけては、それ相応に有効と見定めてもよい・・・云々（必要があれば、追って、手続補正する）。
As a re-added note, for the sake of sight, in this combined version, the kinetic energy is converted into thermal energy for the closed system, and so much propulsion is not generated?・ ・ Although there is a pre-existing high-level observation, under the law of physics, unless a force is externally applied to a certain system, the sum of the momentum of that system is essentially unchanged under the momentum conservation law. As an example where force does not work, there is a problem of collision of an object, and it is exclusively set that the kinetic energy of the object is not preserved except for one example of perfect elastic collision. Since this object and gas / air are not completely elastic collisions, the conservation law is not effective. Therefore, it can be considered that the propulsion system using the internal pressure difference is correspondingly effective.・ Noun (If necessary, we will correct the procedure later).
さほど、従来のような高価なロケット燃料などを要さないことなどから、当該宇宙船類などを尚も安価で製造及び実施し得るようになり、しかも、ただ同然の推進剤を繰り返し使用すれば、加速度的にも高速（果ては光速）で増えていく為、よもや、燃料を補充することなく、（数光年先の）恒星間移動をも容易く相可能となると言っても過言ではない（かもしれない）・・・等々。
Now, because it does not require expensive rocket fuel like the conventional one, it becomes possible to manufacture and implement the spacecraft etc. at a low price, and if only the same propellant is repeatedly used. It is not an exaggeration to say that it is possible to easily move between stars (several light years ahead) without replenishing fuel because it increases at a high speed (and eventually the speed of light). I can't) ... etc.
＊尚（実験機に於ける）各図の寸法表記は、一応、ラジコンパーツのダクテッドファンのサイズをもとにしているものの、実際の宇宙船類の（推進部の）開発にあたっては、大体、これに比例した大きさ（規格サイズ）となり得る所存である。
＊図１０以降は、追って、手続補正にて表記する。 * Although the dimensional notation in each figure (on the experimental aircraft) is based on the size of the ducted fan of the radio control parts, this is mostly for the development of the actual spacecraft (propulsion unit). The size can be proportional to (standard size).
* Figures on and after FIG.
＊図１０以降は、追って、手続補正にて表記する。 * Although the dimensional notation in each figure (on the experimental aircraft) is based on the size of the ducted fan of the radio control parts, this is mostly for the development of the actual spacecraft (propulsion unit). The size can be proportional to (standard size).
* Figures on and after FIG.
追って、手続補正にて表記する。
Later, it will be described in the procedure amendment.
追って、手続補正にて表記する。
Later, it will be described in the procedure amendment.
追って、手続補正にて表記する。
Later, it will be described in the procedure amendment.
a ダクテッドファン類
b 偏向板類
c インペラー類
d エアータンク類
e エアーチューブ類
f エアーノズル類（ロングタイプ）
g 推進補助ファン類（ロングダクト版） a Ducted fans
b Deflectors
c Impellers
d Air tanks
e Air tubes
f Air nozzles (long type)
g Propulsion auxiliary fans (long duct version)
b 偏向板類
c インペラー類
d エアータンク類
e エアーチューブ類
f エアーノズル類（ロングタイプ）
g 推進補助ファン類（ロングダクト版） a Ducted fans
b Deflectors
c Impellers
d Air tanks
e Air tubes
f Air nozzles (long type)
g Propulsion auxiliary fans (long duct version)
Claims (10)
- 先ず、図１等の通り、宇宙船体（A体）の推進部に於ける中央上部あたりに、概ね、ダクテッドファン類或いは、エアコンプレッサー類を配置した上で、その向かいの二股（或いは、それ以上の筒類・曲がり管が四方八方）に分かれたR形状の気筒などを有し、尚且つ、各々の曲がり管類の通気孔（排気口）の端部辺りに、（A体推進向上用の特種形状の）偏向板類を付したA体系の中空式物体と図２等の様に、A体の両吐出口の偏向板類より、強く押し出された空気を別段、B体内の所定の位置にて、極力、一点上に重心軸を置いた特種回転体・（主にプロペラ状のものでなく、ペルトン水車風等含む）ゴム羽根式等のインペラーのブレード類で余す所なく受け止めては、（局部的に、B体と固定していない分離上等の）同回転体を（必要なら、補助的に電動機等による自動式で）自ずと回転し続けることにより、所謂、角運動量保存則（角運動量と歳差運動の角運動量の合成）が成立することを利用して、B体にかかる反推進力を削減（相殺）させ、尚且つ、同回転体自ら、連係上のユー字形のエアチューブ管類を通して、当該ファン類の前方部へ、途切れることなく十二分に空気供給し続けるエアポンプの役目・機能も果たし得ることなどから、予め、偏向板類によって、推進力を補強したA体とそれ相応に、推進力を増強させたB体（周囲の特種コーティングカバー付きチューブ管類等の形状云々が、図２とは違うものなど含む）の推進可能な両体を各物体の静止上の慣性力よりも大きい力（推進ファン類の出力）をもって、必要なら、各体内に付属の的確な速度センサーや位置センサー、平行移動用（補助）バランス調整機器類や風量調節機器類等を駆使しながら、程よく同速度にて連動させつつ、概して、図３等の通り、最接近（準合体化）させ、追々、B体系の射出部から吹き出される（圧縮）空気ガスの受け皿として、隣接したA体系の受容体自ら、吹き出し中の空気ガスを必要なら、同受容体等の周囲に、別枠・分離上等の吸引口付トーラス・ドーナツ型エアチューブ・エアバッグ（図１５参照）類等を覆って、余すところ、気体漏れを生じさせることなく受け止めつつ、尚且つ、そのエアバッグ類の皮膜を高効率の放熱膜として使用し、専ら、推進上の運動エネルギーが熱エネルギーに変換されてしまうことをある程度、阻止或いは軽減しつつ、さほど、持続的にも自動移動可能なA体とB体等が、作用反作用で打ち消し合うことなく、ちょうど、両体（各中空体）を通して気流循環させながら、適程に平行移動させるようにした複式（多重）構造からなる、連係的な特殊宇宙船類（並びに人工衛星等）及び関連機器類一式。 First, as shown in FIG. 1 and the like, a ducted fan or air compressor is generally arranged around the central upper part of the propulsion unit of the spacecraft (A body), and then a bifurcated (or more) It has an R-shaped cylinder, etc., divided into cylinders and bent pipes in all directions, and around the end of the vent hole (exhaust port) of each bent pipe (special for improving A body propulsion) A type hollow object with deflecting plates (shaped) and deflecting plates strongly pushed by the deflecting plates at both outlets of body A, as shown in Fig. 2, etc. As much as possible, the special rotating body with the center of gravity axis on one point and the impeller blades such as rubber blades (not mainly propeller-like ones, including Pelton turbine wind) Locally, the same rotating body (such as separation not fixed to B body) (if necessary, auxiliary) By using the fact that the so-called angular momentum conservation law (combination of angular momentum and precession angular momentum) is established by continuing to rotate itself (automatically by an electric motor, etc.) The function of an air pump that reduces (offsets) the force and continues to supply air sufficiently to the front part of the fans through the U-shaped air tube pipes on the link itself.・ Because it can also fulfill its functions, the A body whose propulsive force has been reinforced with deflecting plates in advance and the B body whose propulsive force has been increased accordingly (the shape of the surrounding tube tubes with special coating covers, etc.) However, if necessary, the exact speed attached to each body can be increased with a force larger than the inertial force of each object (propulsion fan output). Sensor and position sensor While making full use of parallel movement (auxiliary) balance adjustment equipment and air flow adjustment equipment, etc., and interlocking at the same speed moderately, as shown in FIG. As a receiving tray for (compressed) air gas blown out from the injection part of the system, if the adjacent A system receiver itself needs the air gas being blown out, suction around the receiver etc. in a separate frame or separation Covering the torus with a mouth, donut-shaped air tube, airbag (see FIG. 15), etc., and receiving it without causing any gas leakage, while also providing a highly efficient heat dissipation film for the airbag A body and B body, etc. that can automatically move continuously while preventing or reducing to a certain extent that the kinetic energy on propulsion is converted to thermal energy, Counter Without undue effort, the special spacecrafts (and satellites etc.) linked to each other, consisting of a double (multiple) structure that was made to translate appropriately while circulating airflow through both bodies (each hollow body) and A set of related equipment.
- 前項のB体付属の推進ファン類から、A体内（のファンの各ブレード等）へ強風を吹き付ける段階で、多少たりとも、A体自体に後進力が掛かってしまう場合の対処方法として、概ね、図７の通り、A体付属のダクテッドファンの空気吸込口あたりに、B体のファンの風力から被る後進力回避・軽減用インペラー類を数個とその周囲云々に、所々、通気孔の空いた湾曲状等の仕切り金属板類を局部的にも（固定枠等に）組み入れた半ドーム型等の筒類（B体の強風を受け入れる受け皿となるもの）を付加させた特種構造からなる本推進上の後進力回避・軽減システム及び関連機器類一式。 From the propulsion fans attached to body B in the previous section, in the stage where strong wind is blown into body A (each blade of the fan, etc.) As shown in Fig. 7, around the air inlet of the ducted fan attached to the A body, several impellers for avoiding and reducing the backward force from the wind power of the B body fan and the surroundings are curved with vent holes. On the main propulsion consisting of a special structure with a semi-dome-shaped tube (which will be a receiving body for receiving strong B body wind) that incorporates partition metal plates such as shapes locally (in a fixed frame, etc.) Backward force avoidance / reduction system and related equipment set.
- 前々項のB体付属の推進ファン類から、A体内（のファンの各ブレード等）へ強風を吹き付ける段階で、多少たりとも、A体自体に後進力が掛かってしまう場合の対処方法として、概ね、図８の通り、先ず、B体のダクテッドファン類の吹出口辺りに、別途、エアーノズル類（ロングタイプ）を付した上で、所定のエアータンク類から伸びるエアーチューブ類をエアーノズル等に沿って適程に伸ばし、片や、A体内には、先のエアーチューブ類からの気流を受け入れては、それを主なる推進剤とする推進補助ファン（ロング・ダクトタイプで、ファンのブレードはショートタイプでも可）を筒状に沿って配し、ちょうど、請求項１の構図（組図）の様なA体とB体の各ファンが重なり合うことにより、当のA体に、それ相応の後進力が掛かることなく、さほど、両体の各ファン等が確と重複云々せぬよう、なお並列的に配置させた特殊構造からなる本推進上の後進力回避・軽減システム及び関連機器類一式。 As a coping method in the case where the forward force is applied to the A body itself to some extent at the stage of blowing strong wind from the propulsion fans attached to the B body in the previous paragraph to the body A (each blade of the fan, etc.) In general, as shown in FIG. 8, first, air nozzles (long type) are separately attached around the outlet of the B-body ducted fans, and air tubes extending from predetermined air tanks are used as air nozzles. Protruding auxiliary fan (long duct type, fan blade is used as the main propellant, accepting the airflow from the previous air tubes into the piece or A body, (Short type is also possible) is arranged along the cylinder shape, and the A body and B body fans as shown in the composition (composition diagram) of claim 1 overlap each other, so that the corresponding A body moves backward. Without force As both bodies each fan or the like is so, not overlapping the probability so and so, even parallel arranged backward force avoid or mitigate system and related equipment set of the present propulsion consisting special structure was.
- 請求項１等の推進体系に於ける関係機器類の（最）先端部云々に、別途、図９等の通り、中央部のエアタンク類（空気圧縮室）の両脇あたりに、左右の湾曲状のエアーチューブ類から、矢印の方向通り、空気注入するエアーコンプレッサー等の空気吸込口を付設し、所定の空気圧縮室内を極力（最大限に）加圧させては、適時、（小さめの）通気孔付の仕切り金属板類（予め、同空気室付属の気圧センサー等により、同室の気圧・高圧の度合い云々に応じて、自動的に開閉し得る特種形状等の蓋付きのものなど含む）を介して、（数気圧か数十気圧か数百気圧以上の）圧縮空気の一部を後方へ吹き出すことにより、同上の空気圧縮室の前方に、多大な圧力（押力）を加えつつ、それ相応に前進させるという本推進上等の推力増強システム及び関連機器類一式。 In addition to the (most) tip part of the related equipment in the propulsion system of claim 1 etc., as shown in FIG. As shown in the direction of the arrow, air inlets such as an air compressor that injects air are attached to the air tubes, and the specified air compression chamber is pressurized as much as possible (maximum) to ensure that (small) Partition metal plates with pores (including those with lids of special shapes that can be automatically opened and closed according to the degree of atmospheric pressure and high pressure in the same chamber by the pressure sensor attached to the same air chamber) By blowing a part of compressed air (several atmospheres, tens of atmospheres or hundreds of atmospheres or more) to the rear, a large pressure (pressing force) is applied to the front of the air compression chamber. This propulsion superior thrust augmentation system to move forward accordingly, and Communication equipment set.
- 請求項１のA体とB体（外部の方へ、推進剤・空気等を吹き出す開放系にして、各体自体、分離状態にあるもの）を程よく合体化・一体化（コンパクト化）させ、所定の反進行方向に強く吹き出すメインファン類（中央部付近）と、それとは垂直方向に風力を起こす、対となった両サイドの（吸引）ファン類などを統合体内に保持したまま、同体を密閉化させ、当の推進剤（空気）が、一旦、各サイドファンの隣接上の空間部から、メインファン前方の空間部（エアタンク室含む）へ移行する際には、ちょうど、反推進方向に力を加えることなく、自動的に気体（準自然風）を循環させるようにした上で、必要なら、メインファン類への送風用の推進剤・空気等を送り込む（溜め込む）気圧室（加圧室）及びその三角（対角）線上の他の各室（図１０の二重丸部）の要所要所にて、気圧等の度合いが変えられる気圧調整装置や（エアタンク等付）空気圧縮機器類、それに、冷却用等の熱交換器類などを搭載し、適時、（圧力センサー等含む）付属装置で、さしたる気圧等々を部分的にも各（与圧）室ごとに制御することにより、所定請求項１のA体とB体（外部の方へ、推進剤・空気等を吹き出す開放系にして、各体自体、分離状態にあるもの）を程よく合体化・一体化（コンパクト化）させ、所定の反進行方向に強く吹き出すメインファン類（中央部付近）と、それとは垂直方向に風力を起こす、対となった両サイドの（吸引）ファン類などを統合体内に保持したまま、同体を密閉化させ、当の推進剤（空気）が、一旦、各サイドファンの隣接上の空間部から、メインファン前方の空間部（エアタンク室含む）へ移行する際には、ちょうど、反推進方向に力を加えることなく、自動的に気体（準自然風）を循環させるようにした上で、必要なら、メインファン類への送風用の推進剤・空気等を送り込む（溜め込む）気圧室（加圧室）及びその三角（対角）線上の他の各室（図１０の二重丸部）の要所要所にて、気圧等の度合いが変えられる気圧調整装置や（エアタンク等付）空気圧縮機器類、それに、冷却用等の熱交換器類などを搭載し、適時、（圧力センサー等含む）付属装置で、さしたる気圧等々を部分的にも各（加圧）室ごとに制御することにより、所定の高気圧部から低気圧部への気体の流れをなおスムーズにした、単式構造からなる（統合型）特殊宇宙船類（図１０参照）及び関連機器類一式。 Combining and integrating (compact) moderately the A body and B body of claim 1 (open system that blows propellant, air, etc. to the outside, and each body itself is in a separated state) The main fans (near the center) that blow out strongly in a predetermined anti-advancing direction and the paired (suction) fans that generate wind force in the vertical direction, etc. When the propellant (air) is sealed and moves from the space above each side fan to the space (including the air tank chamber) in front of the main fan, it is just in the anti-propulsion direction. Gas pressure (semi-natural wind) is automatically circulated without applying force, and if necessary, an air pressure chamber (pressurized) that sends (accumulates) propellant and air to the main fans. Room) and other rooms on the triangle (diagonal) line ( (10 double circles) equipped with air pressure adjustment devices that can change the degree of atmospheric pressure, etc., air compression equipment (with an air tank, etc.), heat exchangers for cooling, etc. Prompt A body and B body (predetermined to the outside) by controlling each atmospheric pressure etc. partially (each under pressure) with attached devices (including pressure sensors) at appropriate times Main fans (near the central part) that blow out strongly in the specified anti-advancing direction by making the system itself open and separate from each agent and air, etc. And while keeping the paired (suction) fans etc. on both sides that generate wind power in the vertical direction in the integrated body, the same body is sealed, and the propellant (air) is temporarily The space in front of the main fan from the space above the side fan When moving to (including the air tank chamber), the gas (quasi-natural wind) is automatically circulated without applying force in the anti-propulsion direction. At the required locations in the pressure chamber (pressurization chamber) for feeding (accumulating) the propellant and air for blowing and the other chambers (double circles in Fig. 10) on the triangle (diagonal) line Equipped with air pressure adjustment devices that can change the degree of pressure, etc., air compression equipment (with an air tank, etc.), and heat exchangers for cooling, etc. Is partly controlled for each (pressurization) chamber, and the flow of gas from the specified high-pressure part to the low-pressure part is still smooth. FIG. 10) and related equipment set.
- 請求項１等の２口或いは３～４口（以上）の推進ファン及び付随の各（吸引）ファン類の各基につき、別途、チップタービン・ファン或いは、単動翼列多段チップタービン駆動ファン類に改め、適時、各ファン類と空気配管でつながれたコアエンジン（主にエアソースエンジン１基）で、同ファン（複数基）の駆動空気をなべて生成させるという、極力、機体総重量を抑制した（重複）構造からなる本推進力（増強）システム及び関連機器類一式。 A chip turbine fan or a single-stage cascaded multi-stage chip turbine drive fan is separately provided for each of the two-port or three-four-port (or more) propulsion fans and the accompanying (suction) fans. The core engine (mainly one air source engine) that is connected to each fan by air piping will be generated in a timely manner to reduce the total weight of the fuselage as much as possible by generating all the drive air for the same fan (multiple units). A complete set of propulsion (enhancement) systems and related equipment consisting of the
- 請求項１等の特殊宇宙船類に於いて、所定の２口（或いは３～４口以上）の噴出口をもつ各々のチューブ類に通じた各ファン類を任意の一方のみ、適度に稼働させたり、両方の内、片方を強く（或いは弱く）稼働させて、なお偏向的に進行方向を変えたり、別途、推進ファン等の排気口辺りに、概ね 図１１の通り、各メインファン類の２基（或いは４基以上）の作用力（合力）を偏向させる、推力偏向可変ノズル類（同図のT）を付したり、或いは、自動回転装置・リアクションホイール等々を適所に付設（付加）して、適時、それ等の操縦機器類を用いながら、全方位・全角度対応の進路変更などを容易にした方向変換（転換）システム及び関連機器類一式。 In the special spacecraft of claim 1, etc., only one of the fans connected to each tube having a predetermined two-port (or three to four or more) spouts is operated appropriately. Or, one of them can be operated strongly (or weakly) and the direction of travel can be changed in a deflected manner, or separately around the exhaust outlet of the propulsion fan, etc., as shown in FIG. Attaching variable thrust nozzles (T in the figure) to deflect the acting force (synthetic force) of the base (or 4 or more), or attaching (adding) an automatic rotating device, reaction wheel, etc. A direction change system that makes it easy to change the course for all directions and angles while using these control devices in a timely manner and a set of related devices.
- 前項等の各宇宙推進システム及び推力偏向システムを（補助的にも）用いた人工衛星等及び関連機器類（姿勢制御装置等含む）一式。 A set of artificial satellites and related equipment (including attitude control device etc.) using each space propulsion system and thrust deflection system (including auxiliary) in the previous paragraph.
- 請求項１等の宇宙推進システム及びその補助的な推力偏向システムなどを搭載した本船体（単体）もしくは、所定の噴出口が２口から４口以上の複数口をもつ当該船体（一体）を尚も、何体も連ね、複合的に構築した複合船体を（自由落下即ち、見かけ上の無重力下にある）静止軌道上、或いは、それより低軌道上等に滞空、否、滞宙的に配置する一方、とりわけ、以下の長大且つ強靭な紐類自体、自重によって切れないよう、炭素繊維等の複合材などを用いた螺旋状等の特種テザー（各素材の紐類の破断長を限度とした長さのものの末端を連ねた所々のつなぎ目には、多重の強力布類で覆たり、強度の粘着・接着性等のあるものなどで繋ぎ合わされたもの）を採用し、任意のカプセル式等の特種ゴンドラ類をもって、随時、地上からの宇宙旅行客や貨物（ペイロード）などをけん引させるという、自動操縦装置による定点飛行可能な本宇宙滞空（滞宙）システムを備えた宇宙（軌道）エレベーターに加え、別段、これを宇宙の入り口付近の成層圏上（高度約25km以上）に定点飛行させる場合には、特段、当該推力偏向システムを準用した姿勢制御装置類等を駆使しつつ、概ね、図１２通り、本体（母体）の要所（随所）に、（特種硬式飛行船類の気嚢式等の）ヘリウムガス気球類などを加えたり、或いは、さしたる気流循環式の浮上システム（特段、主要なダクテッドファンやエアコンプレッサー類・軸流又は遠心式圧縮機等で、より多くの反動質量をもった推進剤・圧縮空気類を高圧的に進行方向側へ噴射させると同時に、その反作用力を極力、抑える反推進力抑制用の各ファン類を適度に稼働させ、尚且つ、有り余る（余剰の）空気類を所定の排出口より当該機外へ噴出させるという３段階式の推力増強システム）を図１９等の様に応用しては、それ相当、浮力を増すように施したり、更に、付随的にも、複数基の宇宙エレベーターにかけて、とりわけ、本塔の垂直線上と両端辺りにかかる斜め上等に作用力を強く及ぼしながら、特殊なロープウエイ方式等にて、各々の任意の２点間等を自動的に渡れるようにしたスペースブリッジ（スペース＜ケーブル＞レール）・システム且つ（地球上の全天周囲に取り巻く）オービタルリング等・システム及び関連機器類一式。 The main hull (single unit) on which the space propulsion system according to claim 1 and the auxiliary thrust deflection system thereof are mounted, or the hull (integral unit) having a plurality of two or more predetermined outlets. However, multiple hulls that are constructed in a row are placed on a stationary orbit (free fall or under apparent weightlessness) or on a lower orbit, etc. On the other hand, in particular, the following long and strong cords themselves, special tethers such as spirals using a composite material such as carbon fiber so as not to be broken by their own weight (limited to the breaking length of the strings of each material) At the joints where the ends of the long ones are connected, they are covered with multiple strong cloths or joined together with strong adhesives / adhesives etc.), and any capsule type etc. Space from the ground with special gondola In addition to the space (orbit) elevator equipped with this space aerial system (aerial space) system that can fly fixed points by automatic control devices that tow passengers and cargo (payload) etc., this is the stratosphere near the entrance of the universe When flying at a fixed point above (altitude of about 25km or more), the main points of the main body (matrix) are almost as shown in Fig. 12, using the attitude control devices that apply the thrust deflection system. Helium gas balloons (such as the air bag type of special type hard airships), or the airflow circulation type levitation system (specially, major ducted fans, air compressors, axial flow, centrifugal compressors, etc.) Each of the fans for suppressing the anti-propulsion force that injects the propellant / compressed air having a larger reaction mass into the traveling direction side at a high pressure and suppresses the reaction force as much as possible. Applying a three-stage thrust augmentation system that allows the engine to operate in a modest manner and that excess air (excess air) is ejected from the specified outlet to the outside of the machine. It can be applied to increase buoyancy, and incidentally, it can be applied to multiple space elevators, especially while acting strongly on the vertical line of the main tower and diagonally upwards around both ends, and has a special ropeway. Space bridge (space <cable> rail) system and orbital ring (around the entire sky on the earth), etc. A set of equipment.
- 前項等の３段式推力システムなどを（部分的にも）採用した特種宇宙船類・（再使用型）宇宙往還機類及び同上システム（の一部）を応用した関連上の推進装置類や姿勢制御装置類を含む人工衛星等並びに関連機器類一式。
＊請求項５以降は、追って、手続補正する。 Special-purpose spacecraft, (reusable) space return aircraft that employs the three-stage thrust system, etc., as described in the previous paragraph, and related propulsion devices that apply (part of) the same system A set of artificial satellites and related equipment including attitude control devices.
* From claim 5 onwards, the procedure will be amended later.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP2012230374A JP2014080938A (en) | 2012-10-17 | 2012-10-17 | Space propulsion and endurance space (stratospheric endurance flight) system |
| JP2012-230374 | 2012-10-17 |
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| PCT/JP2013/078241 WO2014061759A2 (en) | 2012-10-17 | 2013-10-17 | System for space propulsion and staying in space (staying in above-stratosphere air) |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017037528A1 (en) * | 2015-09-04 | 2017-03-09 | Nagel Edmund F | Periphery-independent drive |
| WO2018079754A1 (en) * | 2016-10-27 | 2018-05-03 | 上内金吾 | Pressure (internal pressure) difference propulsion system |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20240010362A1 (en) * | 2022-07-07 | 2024-01-11 | Martin Eugene Nix | Solar space ship yacht |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010208501A (en) * | 2009-03-10 | 2010-09-24 | Mitsubishi Heavy Ind Ltd | Unmanned aircraft and unmanned aircraft system |
| WO2012137366A1 (en) * | 2011-04-06 | 2012-10-11 | グレースマリー・ワールド株式会社 | Space propulsion and space endurance flight system |
-
2012
- 2012-10-17 JP JP2012230374A patent/JP2014080938A/en active Pending
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Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010208501A (en) * | 2009-03-10 | 2010-09-24 | Mitsubishi Heavy Ind Ltd | Unmanned aircraft and unmanned aircraft system |
| WO2012137366A1 (en) * | 2011-04-06 | 2012-10-11 | グレースマリー・ワールド株式会社 | Space propulsion and space endurance flight system |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2017037528A1 (en) * | 2015-09-04 | 2017-03-09 | Nagel Edmund F | Periphery-independent drive |
| WO2018079754A1 (en) * | 2016-10-27 | 2018-05-03 | 上内金吾 | Pressure (internal pressure) difference propulsion system |
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| WO2014061759A3 (en) | 2014-06-26 |
| JP2014080938A (en) | 2014-05-08 |
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