JP2008309054A - Propelling machine - Google Patents
Propelling machine Download PDFInfo
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- JP2008309054A JP2008309054A JP2007157084A JP2007157084A JP2008309054A JP 2008309054 A JP2008309054 A JP 2008309054A JP 2007157084 A JP2007157084 A JP 2007157084A JP 2007157084 A JP2007157084 A JP 2007157084A JP 2008309054 A JP2008309054 A JP 2008309054A
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本発明は昇降機を内臓したフレーム外側に本推進機を組み付けて何段も重ねて上空に伸ばして物体を宇宙などに往復搬送に関するものである。
The present invention relates to a reciprocating conveyance of an object to space or the like by assembling the propulsion device outside a frame having a built-in elevator and stacking several layers and extending it to the sky.
これまでは宇宙へはガス噴出ロケットだけです。 先行特許文献には
従来のロケット推進では宇宙搬送には施設、資金が莫大となる。
本推進器は遠心力、プレセッションを利用して推進力を発生させてフレームに内臓した昇降機、推進機と組み合わせ恒常的に宇宙へ搬送する事が課題である。
In conventional rocket propulsion, facilities and funds are huge for space transportation.
The problem with this propulsion unit is that it generates centrifugal propulsion and propulsion using precession and is transported to space constantly in combination with an elevator and propulsion unit built in the frame.
本発明は上記目的を達成する為、下記の手段、構成で解決させる、
鉄丸棒を円形リングにしたものを水平に置き、円形リングを蝶の羽のようにU状に二つ折れに、曲げて、上が広がったU型にする、U型の内角は120度にする、円形U曲がりリングのU型底両端は留め金11、で大型フライホイル9、の円の淵に取り付け固定する。
In order to achieve the above object, the present invention is solved by the following means and configuration.
Place a round steel ring into a circular ring and place it in a U shape like a butterfly's wing and bend it into a U shape with an open top. The both ends of the U-shaped bottom of the circular U-bending ring are fixed to the circular flange of the large flywheel 9 with clasps 11.
大型フライホイル9、はフレーム7、に取り付け軸先に大型フライホイル9、を嵌入し、大型フライホイル9、のセンターに大型モーター1、を取り付け固定し軸先にには、フランジ駆動ホルダー8、を嵌入する。
The large flywheel 9 is inserted into the frame 7 with a large flywheel 9 at the mounting shaft, and the large motor 1 is mounted and fixed at the center of the large flywheel 9, and the flange drive holder 8 is mounted at the shaft. Insert.
フランジ駆動ホルダー8、には角型棒バー5、の6本をピンで放射状に取り付ける、角型棒バー5、の先端には小型モーター6、を取り付ける。
Six pieces of the
小型モーター6、の軸先には小型フライホイル2、を嵌入する、小型フライホイル2、のカバー先端軸に、角金板12、を嵌め更に長いボールベアリング4も嵌めこみ、角金板12、に二つ目の長いボールベアリング4、を取り付け固定して円形U曲がりリング3、を挟んで取り付ける。
A small flywheel 2 is inserted into the shaft tip of the small motor 6. A square metal plate 12 is fitted into a cover tip shaft of the small flywheel 2, and a longer ball bearing 4 is also fitted into the small flywheel 2. The second long ball bearing 4 is attached and fixed to the circular U-bend ring 3 and attached.
小型フライホイル2、を上段左周りで2000回転で自転させ その小型フライホイル2、が円形U曲がリング3、に沿ってガイドされ200回転で公転させて更に大型フライホイル9、を100回転で全体回転するようにする。
The small flywheel 2 is rotated around the upper left at 2000 rotations, and the small flywheel 2 is guided along the circular U-shaped ring 3 and revolved at 200 rotations, and the large flywheel 9 is rotated at 100 rotations. Make the whole rotation.
小型フライホイル2、が右半円2個と左半円2個での、上60度方向の遠心力の合力で推進力を発生させる、円形U曲がりリング3、のU型曲がりの底部位置で小型フライホイル2、の自転、公転で円周接線の直角方向にプレセッションの力で方向転換する、と同時に大型フライホイル9、の全体回転でも小型フライホイル2、のプレセッションで揚力が発生し下接線方向への力が減殺される、上段下段の回転方向はすべて逆回転とし反作用など相殺してバランスをとらせる、以上の手段を講じた推進機である。
At the bottom of the U-shaped bend of the circular U-bend ring 3, the small flywheel 2 generates propulsive force with the resultant force of centrifugal force in the direction of 60 degrees upward, with two right semicircles and two left semicircles. When the small flywheel 2 rotates and revolves, the direction is changed by the precession force in the direction perpendicular to the circumference tangential line. At the same time, the large flywheel 9 also rotates with the small flywheel 2 precession. The propulsion unit has the above measures in which the force in the lower tangential direction is reduced, and the upper and lower rotation directions are all reverse rotations and counterbalances and balances them.
請求項2の推進機は円形U曲がりリング3、を平鉄にし、そこに電磁石のリニアモーター駆動コイル14、を貼り付け磁石ホルダー13、が円形U曲がりリング3、に沿ってスライドするようにして、公転200回転させる磁石ホルダー13、には小型モーター6、と小型フライホイル2、を取り付ければ、請求項1と同じ効果の推進機である。
The propulsion device according to claim 2 is configured such that the circular U-curved ring 3 is made of flat iron, and an electromagnet linear motor drive coil 14 is attached thereto so that the magnet holder 13 slides along the circular U-curved ring 3. If the small motor 6 and the small flywheel 2 are attached to the magnet holder 13 that rotates 200 revolutions, the propulsion device has the same effect as that of the first aspect.
ロ字型の四角形立法体のフレームにして何段も積み上げ四角形の中にエレベターを組み込み本推進機又は電磁誘導駆動式かギヤーとスピンドルギヤーなどの組み合わせによってエレベーターを昇降させる事が出来る、本推進機を何箇所もフレームの外側に取り付けフレームを常に上方に推進力を働かせてフレームの重力を軽減上空に固定安定させる事が出来て、宇宙にも往復搬送が常時可能となる効果がある、動力は電力で賄う。
又宇宙でのソーラーシステムなどで電力を地上に送電出来る期待ががもてるまた小型フライホイル2、の回転中心点移動が推進機移動距離より遅ければ昇降機やヘリコプターなどに応用できる、効果のある推進機である。
This propulsion unit can be lifted up and down by a combination of a propeller or electromagnetic induction drive type or a combination of gear and spindle gear. A number of places are attached to the outside of the frame, and the frame is always moved upward to reduce the gravity of the frame, so that it can be fixed and stabilized in the sky. Cover with electricity.
Promising propulsion that can be applied to elevators and helicopters if the small flywheel 2 can move to the ground with a solar system in space, and if the movement of the center of rotation of the small flywheel 2 is slower than the propulsion unit movement distance Machine.
小型モーター6、で小型フライホイル2、の直径200ミリ厚さ33ミリの中刳りで重さ約4,5キロを回転数2000回転させる。 The small motor 6 and the small flywheel 2 have a diameter of 200 mm and a thickness of 33 mm.
円形U曲がりリング3、の太さ20ミリにして円形の直径約940ミリです
円形内径は900ミリです、実際はU曲がり分だけ楕円状となる
The circular U-bend ring 3 has a thickness of 20 mm and a circular diameter of about 940 mm. The circular inner diameter is 900 mm.
フランジ駆動ホルダー8、に付けた角型棒バー5、6本の公転数は200回転です。 The number of revolutions of the 6 square bar bars attached to the flange drive holder 8 is 200 revolutions.
大型モーター1、の軸先にはフランジ駆動ホルダー8、を嵌入している、
角型バー5、の長さはフランジ駆動ホルダー8、軸中心から長いローラーベアリング4、先端まで550ミリです。
A flange drive holder 8 is inserted into the shaft end of the large motor 1.
The length of the
超大型モーター10、をフレーム7、に取り付けて、軸先には大型フライホイル9、を嵌入して100回転させる、大型フライホイル9、の中心に大型モーター1、を乗せて固定する。 The super large motor 10 is attached to the frame 7, and the large motor 1 is mounted on the center of the large fly wheel 9 which is inserted into the large flywheel 9 at the shaft end and rotated 100 times.
超大型モーター10、大型モーター1、小型モーター6、共に上段側左回転下段側右回転として上下段の回転反作用のバランスをとる。
The super large motor 10, the large motor 1, and the small motor 6 all balance the rotational reaction of the upper and lower stages as upper left rotation and lower right rotation.
手作り試作では小型モーター6、は自動車のワイパーモーターを使用、小型フライホイル2、は2個だけで自転約500回転と、大型モーター1、は200V、0.75KW可変型を使用、公転は約60回転で、大型フライホイル9、100回転は使用しなかったが、横向きスライド方式にして実験した結果推進力は約1キログラムで高速回転は危険で出来なかった。
実用化には超大型モーター、大型モーター、小型モーター、円形U曲がりリング、フレーム、角型棒バー、など構造、大きさ共に増強して強力な推力を得るようにする、なお図面には補強材は表示していない。
In the handmade prototype, the small motor 6 uses a car wiper motor, the small flywheel 2 uses only two pieces and rotates about 500 revolutions, the large motor 1 uses a 200V, 0.75 kW variable type, and about 60 revolutions. In the rotation, large flywheel 9, 100 rotations were not used, but as a result of experimenting with a lateral slide system, the driving force was about 1 kilogram and high speed rotation was not possible.
For practical use, super large motors, large motors, small motors, circular U-bend rings, frames, square bar bars, etc., increase the structure and size to obtain a strong thrust. Is not displayed.
試算では総推進力は約1144キロです、計算式は下記又は図4で説明する。
瞬間時、推進力 計算式
重量×半径×回転数?=遠心力
4,5kg×0,45m×200回転=405kg
遠心力×小ベクトル係数=左方小ベクトル遠心力
405kg×166%=左672kg (ベクトル図面で算出166%)
左小ベクトル遠心力×大ベクトル係数=総遠心力
672kg× 0% =672kg (ベクトル図面で算出0%)
推定プレセッション揚力×2箇所=推定プレセッション全揚力
(遠心力の半分) 202.5k×2=405kg (大型フライホイルの全体左回転100回転の分)
推定−接線下方向遠心力×2箇所=−接線全下方向推進力 一段目推定自重
(遠心力の半分) 202.5kg×2= 405kg 100 kg
推定-接線全下方向推進力+推定自重=全マイナス推進力
405kg+ 100kg =505kg
(総遠心力+推定プレセッション揚力)−(−推定接線下方向推進力+推定自重)=上段推進力
(672kg+405kg)−( −405kg +100kg )= 572kg
(上段側)572kg+(下段側)572kg=1144kg(総推進力)
理科の先生に計算して貰うと405kgが88.5kgとでる166%掛けると146.9kgで自重より大きい。
In the trial calculation, the total driving force is about 1144 km, and the calculation formula will be explained below or in FIG.
Momentary moment propulsion formula Weight x Radius x Rotation speed? = Centrifugal force
4,5kg × 0,45m × 200rpm = 405kg
Centrifugal force x small vector coefficient = left small vector centrifugal force
405 kg x 166% = left 672 kg (calculated by
Left small vector centrifugal force x large vector coefficient = total centrifugal force
672kg × 0% = 672kg (Calculated with
Estimated precession lift x 2 locations = estimated precession total lift (half of the centrifugal force) 202.5k x 2 = 405 kg (100 minutes of total left turn of large flywheel)
Estimated-Tangent downward centrifugal force x 2 locations =-Tangent full downward propulsive force First stage estimated dead weight (half of the centrifugal force) 202.5 kg x 2 = 405 kg 100 kg
Estimated-tangential full downward propulsive force + estimated dead weight = total negative propulsive force
405kg + 100kg = 505kg
(Total centrifugal force + Estimated precession lift)-(-Estimated tangential downward thrust + Estimated weight) = Upper thrust
(672kg + 405kg)-(-405kg + 100kg) = 572kg
(Upper side) 572kg + (Lower side) 572kg = 1144kg (Total driving force)
Calculated by a science teacher, 405 kg is 88.5 kg, multiplied by 166%, which is 146.9 kg, which is greater than its own weight.
1、大型モーター 9、大型フライホイル
2、小型フライホイル 10、超大型モーター
3、円形U曲がりリング 11、円形U曲がりリング留め金
4、長いローラーベアリング12、角金板
5、角型棒バー
6、小型モーター 13、磁石ホルダー(図2)
7、フレーム 14、リニアモーター駆動コイル(図2)
8、フランジ駆動ホルダー
1. Large motor 9. Large flywheel
2, Small flywheel 10, Super large motor
3. Circular U bend ring 11. Circular U bend ring clasp
4. Long roller bearing 12, square metal plate
5. Square bar
6. Small motor 13, magnet holder (Fig. 2)
7, frame 14, linear motor drive coil (Figure 2)
8. Flange drive holder
Claims (2)
Two semi-circular bars are set up vertically in the front-rear direction, and the two vertices are tilted 60 degrees to the left and right, and the lower ends are connected to the U shape. The wheel surface is perpendicular to the semi-circular surface, and the rotational transition tangent is made by precession at the point when the rotational movement is 0 ° to 180 ° on the circumference so that the sun rises from the left semi-circular side. Since the force is changed in the direction perpendicular to the direction, and at the same time, it is rotated counterclockwise around the center point of the diameter of the semicircular rod, lift is generated in the same way as the former. The power is reduced, the small flywheel moves and rotates on the circumference of the semi-circular rod standing to the right, and the small flywheel guided by the circumferential movement of the semi-circular, from 180 degrees in front Go around 360 degrees to the right side as the sun goes down. If a plurality of small flywheels are attached, and the small flywheels are scattered on the left and right circumferences, the small flywheels are scattered 60 degrees upward on the left and right. The centrifugal force of the small flywheel works and the propulsive force that pulls up in the upward direction is generated by the resultant force of the vector. The upper and lower stages are propulsion units that balance the rotational reaction by reversing the direction of rotation.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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JP2007157084A JP2008309054A (en) | 2007-06-14 | 2007-06-14 | Propelling machine |
Applications Claiming Priority (1)
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JP2007157084A JP2008309054A (en) | 2007-06-14 | 2007-06-14 | Propelling machine |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
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JP2010000294U Continuation JP3158488U (en) | 2010-01-20 | 2010-01-20 | Propulsion machine |
Publications (2)
Publication Number | Publication Date |
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JP2008309054A true JP2008309054A (en) | 2008-12-25 |
JP2008309054A5 JP2008309054A5 (en) | 2009-11-26 |
Family
ID=40236875
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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JP2007157084A Pending JP2008309054A (en) | 2007-06-14 | 2007-06-14 | Propelling machine |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010101300A (en) * | 2008-10-27 | 2010-05-06 | Shoichi Yamaura | Propulsion device |
RU2520776C1 (en) * | 2013-02-20 | 2014-06-27 | Игорь Глебович Богданов | Inertial propulsor of bogdanov |
RU2771702C1 (en) * | 2021-07-25 | 2022-05-11 | Алексей Борисович Шуркевич | Method for creating an adjustable value of the dynamic center of mass and a device for its implementation |
CN115533842A (en) * | 2022-10-24 | 2022-12-30 | 兰州空间技术物理研究所 | Assembling, testing and adjusting device for ion thruster |
-
2007
- 2007-06-14 JP JP2007157084A patent/JP2008309054A/en active Pending
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2010101300A (en) * | 2008-10-27 | 2010-05-06 | Shoichi Yamaura | Propulsion device |
RU2520776C1 (en) * | 2013-02-20 | 2014-06-27 | Игорь Глебович Богданов | Inertial propulsor of bogdanov |
RU2771702C1 (en) * | 2021-07-25 | 2022-05-11 | Алексей Борисович Шуркевич | Method for creating an adjustable value of the dynamic center of mass and a device for its implementation |
CN115533842A (en) * | 2022-10-24 | 2022-12-30 | 兰州空间技术物理研究所 | Assembling, testing and adjusting device for ion thruster |
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Effective date: 20091014 Free format text: JAPANESE INTERMEDIATE CODE: A523 |