Classifications

• • 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
• • 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
  • F03G3/00—Other motors, e.g. gravity or inertia motors
• • 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
  • F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
  • F03H99/00—Subject matter not provided for in other groups of this subclass

Definitions

• the present invention relates to a propulsion method based on inertial forces that can be used in an inertial system, completely controllable.
• propulsion and drive mechanisms are based on the principle: every action causes a reaction. Induction of a force creates a counterforce in response, which is responsible for any propulsion.
• the propulsion mechanisms operate by directly contact or interaction of the medium in or on the place of the propulsion, driven with the object. For all vehicles, the propulsion forces are generated by contact of vehicle wheels with the ground, develop by the friction between wheels and floor or fixed course themselves as opposing forces.
• Maglev train Another terrestrial version is the Maglev train, where, although there is no contact with the ground, it is also an example of interaction (action-reaction), because the electromagnets of the train interact with the electromagnetic field of the fixed rail, which induces a counterforce which is responsible for the propulsion of the train.
• action-reaction Because the electromagnets of the train interact with the electromagnetic field of the fixed rail, which induces a counterforce which is responsible for the propulsion of the train.
• a propeller In water or in air, a propeller is responsible for the propulsion. The propeller turns so that the liquid medium (water or air) is pushing in the opposite direction, inducing so opposite propulsion forces (by ships, submarines, helicopters, planes, etc).
• propulsion mechanisms are the rocket-engines and jet planes-propulsion mechanism, where propulsion forces are achieved by the dismissal of high-pressure gases in the opposite direction.
• the medium on which or in which there is propulsion has the role of the holding up medium for the propelled object, except for rocket-engines.
• the result is the following question: How can a propulsion mechanism work without the existence of any holding up medium, for example in the vacuum of the space, but also without the use of high pressure gases, which have the disadvantages to go running out very quickly and the existence of high risk of explosion.
• the present invention seems to solve this problem with the logic of a resolution applicable and accessible to the known laws of physics, with a device, in which an entirely new propulsion method is using the inertial forces.
• the propulsion mechanism of the dual inertial impulse is formed by a track in form of a circle, by the diameter d, divided in two semi-circles, which are removed one another at a distance s.
• the free ends of the half circles are connected with two straight sections, each with a length s. These straight sections are two parallel sides of an imaginary rectangle.
• a closed loop is formed, similar with the shape of the digit "0" (zero).
• This loop is the form of an orbital-track, moving on it two similar and equally masses of mass m, in the same orbital direction and in a very controlled manner, to compensate the effects of unwanted forces, like gravity or friction.
• the relative orbital distance of the two masses is always a half loop.
• the whole orbit-masses system is called from now on as an orbital system. As long as the masses move, either with accelerated speed or with constant speed, while maintaining their orbital diametrical position, the orbital system as a whole remains almost motionless in space, while each linear velocity of the masses are opposite but equivalent. An imaginary straight line that connects the two masses is always passing by the central point K of the system.
• the masses interact with the orbit-rail by the action of friction forces or electromagnetic counter-forces, which results a slight rotation of the whole orbit system around the central vertical axis which is running through the central point K. This slight rotation has an opposite direction relative to the orbital direction of the masses.
• a second and identical orbital system is coplanar coupled to the first (on the same plane), so that any straight section of the orbital rail of the first orbital system with each straight section of the orbital rail of the second system are forming two parallel sides of an imaginary coplanar rectangle.
• the masses of the second orbital system can move always with opposite orbital direction relative to the masses of the first orbital system.
• Each instantaneous relative position of the four masses leads to the appearance that the one orbital system is the mirror image of the other orbital system. From now on, the two orbital systems together, as a whole system, were as a dual-orbital system mentioned.
• the whole dual-orbital system always lead to an automatically controlled manner at each instantaneous relative position of the masses continuously to the appearance that the one orbital system at any time, is the mirror image of the other orbital system.
• the velocity state of the whole dual- orbital system remains unaffected.
• the effect of gravity on the masses is automatically balanced. If all masses simultaneously achieve certain speed, the retarding mechanisms are activated.
• the masses have an angular momentum as they pass the half-circle of its orbit because they are subject to a half-rotation.
• the highest value of angular momentum is achieved at the maximum orbital velocity v m .
• each mass tends to leave the respective semi-circle of its orbit, in preserving the resulting self- rotation (spin) so that the smooth orbital motion will be disturbed. That is why the masses should be identical disk-shaped and coplanar with the orbital plane. Also they should be free to rotate about their central axis, perpendicular to the orbital plane.
• the driving and / or wheel frame of the masses should be simple, lightness and frictionless as much as possible while resistant to higher back forces. The most ideal construction would be the one where the masses are free floating driven by magnetic fields (like a magnetic train) without the use of a wheel frame.
• the size of the mass m plays an important role. It must be small enough to be accelerated more easily, but big enough to propel the whole system. Therefore the mass ratio m / M (mass of the entire dual-orbital system) is one of the most important factors.
• the second important factor is the maximum orbital velocity v m of the masses.
• the maximum speed must be as high as possible.
• the construction of such a system must withstand those speeds.
• the third factor is the acceleration ⁇ of the masses. This should be as high as possible at the time section (At;) between the dual-impulses, in other words the time section (At*) must be reduced and therefore the frequency n P of repetition of the dual-impulse per time unit must be increased.
• the fourth factor is the length of the distance s and / or its size relative to the diameter d. This factor contributes to the system performance, influencing the period At and the size of ⁇ and therefore the synchronizing of the masses.
• the final version of this propulsion mechanism consists of a complex of several identical dual-orbital systems that are coupled together, in a way where all the straight sections of the orbital tracks with each other, are parallel sides of imaginary rectangles .
• the complex takes the form of either a rosette or a serial array of similar dual-orbital-systems (parallel-connected dual-orbital systems).
• hyper-orbital system is mentioned.
• Each dual-orbital system propels lagged compared with the other dual-orbital-systems in a particular order, repeating in a cycle (hyper- cycle) so that results continuous propulsion of the whole hyper-orbital system.
• the propulsion tends to be smooth and without jolt.
• the efficiency of the Hyper-orbital system will now depend on the capabilities of automation, for coordinating all dual-orbital systems.
• Figure 1 the shape of a loop is shown. It consists of two equal semicircles (arc ⁇ , arc ⁇ ), as well as two equal and parallel straight sections AB and ⁇ with the length of s.
• the straight lines Ex and Ey the two axes of symmetry of the loop, with their intersect point K (symmetry center).
• KA, KB points are the centers of the respective circles of the two sheets of half- circles.
• the imaginary straight sections ⁇ and ⁇ are the same, with a length d and, in parallel, and their midpoints KA and KB.
• ⁇ is an imaginary rectangle.
• Figure 2 shows a dual-orbital system, with the four disc-shaped masses (ml , m2, m3, m4), the masses (ml) and (m3) move on the orbital system (I) and masses (m2) and (m4) on the orbital system (II).
• Each mass is accompanied by an imaginary arrow which shows its linear direction.
• the two orbital systems (I, II.) are coplanar and coupled together by a connecting frame (5).
• the propulsion of the dual-orbital system takes place at the symmetry axis (E3) in the direction of the large imaginary arrow.
• the masses (ml) and (m2) are on an imaginary moving straight line (E1) set, while the masses (m3) and (m4) to a second imaginary moving straight line (E2) are set to be parallel to the (E1) is.
• These two lines (E1) and (E2) are always vertical to the line (E3) directed.
• These two lines (E1 , E2) move, constantly parallel to each other or against each other. Also visible is the driving and wheel frame (8) of the respective masses (ml , m2, m3, m4).
• Figure 3 is a plan view of a rosette version of Hyper-orbital system, consisting of three dual-orbital systems (A, B, ⁇ ), with 6 retarding mechanisms (3), one for each orbital system (Al ., All, Bl., Bit. ⁇ ., ⁇ .), and with the respective disk-shaped masses (Am , Am2, Am3, Am4, Bm1 , Bm2, Bm4 Bm3 I ⁇ m1 , ⁇ 2, ⁇ 3, ⁇ 4).
• Recognizable is the transport system (driving and wheel frame) (8) of the disk-shaped masses (Ami, Am2, Am3, Am4, Bm1 , Bm2, Bm3, Bm4, Tm1, Tm2, Tm3, Tm4), each orbital track (9) the connecting frame (10) of the dual-orbital systems (A, B, ⁇ ) and the imaginary center of symmetry (11) of the whole system.
• Figure 4 shows the same example as Figure 3, in 3D lateral-frontal perspective.
• the connecting frame of each dual-orbital systems (A, B, ⁇ ) is purposely missing, because to reduce the complexity of the picture.
• the three dual-orbital systems (A, B, ⁇ ) can be recognized, and the six-orbital systems (Al., All. Bl., Bll.

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• Engineering & Computer Science (AREA)
• Chemical & Material Sciences (AREA)
• Combustion & Propulsion (AREA)
• Mechanical Engineering (AREA)
• General Engineering & Computer Science (AREA)
• Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
• Measurement Of The Respiration, Hearing Ability, Form, And Blood Characteristics Of Living Organisms (AREA)

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Cited By (5)

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• 2010
  • 2010-06-17 GR GR20100100348A patent/GR20100100348A/el unknown
• 2011
  • 2011-06-17 WO PCT/GR2011/000023 patent/WO2011158048A2/en active Application Filing

Non-Patent Citations (1)

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