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Title:
METHOD AND A SYSTEM FOR GENERATING FUEL EFFICIENT FORCE BY ACCELERATING OBJECT AND USING CENTRIFUGAL FORCE
Document Type and Number:
WIPO Patent Application WO/2018/091962
Kind Code:
A4
Abstract:
This invention is an improvement and completion of my granted USPTO patent (US 8272283 B2) to enhance fuel efficiency by utilizing a number of reaction engines running along a looped track which the said looped track is comprised of two straight paths and two semicircle curved parts and the reaction engines running along the looped track in the manner which is descried within the scope of this invention, will transfer their kinetic energy to the said looped track and consequently generate a unidirectional force on the looped track with more efficient fuel consumption.

Inventors:
VAFAEY, Hossain (Apt 1, 31 East farzan street,,Nelson Mandella avenue, Tehran ., 19176-86111, IR)
Application Number:
IB2017/001398
Publication Date:
September 20, 2018
Filing Date:
November 15, 2017
Export Citation:
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Assignee:
VAFAEY, Hossain (Apt 1, 31 East farzan street,,Nelson Mandella avenue, Tehran ., 19176-86111, IR)
International Classes:
F03H99/00; F02C6/00
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Claims:
AMENDED CLAIMS

received by the International Bureau on 01 August 2018 (01.08.2018)

1) In order to improve and further advance to different field of technology, my granted USPTO patent (US 8272283 B2) with international classification of F03G 3/00 which is a method and system for vibrating an object using centrifugal force which is comprised of an outer shell and a plurality of jet nuzzles that travel along the outer shell air cushioned by means of magnetism and controlled by a CPU or central processing unit to eventually vibrate object, wherein the advancements are characterized by the following;

The embodiment of the current invention is a method and system for generating a unidirectional force comprising a looped track and a plurality of reaction engines, and wherein the looped track comprises a first straight path, a first curved path, a second straight path, and a second curved path and wherein the reaction engines move along the different paths of the looped track with the following steps;

a) The said plurality of reaction engines are activated and accelerate in the first straight path of the looped track with a predetermined force magnitude usually high force and once the said reaction engines reach the end of first straight path of the looped track, their predetermined force will be deactivated and,

b) The said plurality of reaction engines which have gained a substantial kinetic energy will enter the first curved path of the looped track and travel along this path and as a result of the reaction engines movement along the first curved path of the looped track a unidirectional force, centrifugal force, is exerted to the looped track and,

c) The said plurality of reaction engines will decelerate during the second straight path of the looped track by means of drag or other means of forces acting against the reaction engines and,

d) The said plurality of reaction engines will move along the second curved path of the looped track with a low velocity and the said plurality of reaction engines will be positioned at the stage described in step a again and the cycle continues.

As a result where the said plurality of reaction engines repeatedly and continuously render the above mentioned steps a unidirectional force will be generated by the looped track which then the looped track can be attached to any object or vehicle that can benefit from this.

The said plurality of reaction engines as well defined by Wikipedia and other dictionary sources are basically any kind of reaction engine that produces thrust in accordance with Newtonian laws of motion and specifically newton s third law of motion and also includes ions and or charged particles accelerated and decelerated by means of electric field and or electromagnetic wave in conformance with established laws of physic and other related fields. 2) A system according to claim 1, further comprising a second looped track which is fixed to the first looped track back to back and the movement of the said plurality of reaction engines running along these looped tracks must be in opposite directions i.e one in clockwise direction and the other in anticlockwise direction. Both sides must apply centrifugal force to the first curved path of their looped track to achieve a sufficient unidirectional force.

3) A system according to claim 1, further comprising a wire coiled around the section of looped track with electrical current flowing through it, and also the said plurality of reaction engines comprises permanent magnet therefore the said plurality of reaction engines will be floating or air cushioned throughout the looped tracks different paths during run. Reaction engines movement along the looped track in all paths are air cushioned.

4) A system according to claim 1, further comprises automated fuel pumping system at the second curved path of the looped track where the speed of the said plurality of the reaction engines are at their lowest during their afore mentioned cycle explained in claim 1 step d. Furthermore the said plurality of the reaction engines comprises automated valves to receive the fuel while moving along the second curved path of the looped track, and then detach from the fuel pumping system and continue their cycle.

5) A system according to claim 1, wherein the said looped track comprises ferromagnetic coil of wire around its section which conducts high frequency alternating current to generate alternating magnetic field along different paths of the said looped track. The said plurality of reaction engines further comprises coil of wire to receive the alternating current induced by the magnetic field, and when received, the alternating current can then be rectified and transformed to DC current and made available for consumption by electric circuits implemented in each of the said plurality of the reaction engines. The attached coil of wire to the plurality of reaction engines will remain within vicinity and noncontact of the ferromagnetic coil of wire which is the alternating magnetic field supply source, during travel of the reaction engines along the different paths of the said looped track.

6) A system according to claim 1, step c wherein the said plurality of reaction engines comprises a parachute and or airbrake system. Since the reaction engines decelerate at the second straight path of the looped track therefore it is essential to decelerate these reaction engines by means of air drag to be efficient and in order to achieve this goal a parachute and or airbrake mechanism is used and by actuating the parachute or airbrake system to fold open, the cross sectional area of the reaction engine is increased therefore the drag force created will decelerate the reaction engine during its travel at the second straight path of the looped track, and eventually when the reaction engine reaches the end of the second straight path of the looped track its velocity will be at its minimal and the parachute or airbrake is to be folded back and when the reaction engine reaches the first straight path of the looped track the reaction engine is ready to accelerate again.

7) A system according to claim 1, wherein the said looped track comprises a number of sensors alongside it. As the said plurality of reaction engines move along the different paths of the looped track they pass these sensors that are attached to the looped track. While the reaction engines move along the different paths of the looped track and when they align with any of the sensors attached to the looped track, that particular sensor then sends a signal to the processing unit or CPU. The processing unit or CPU will then process the received signal in accordance with the program that has been written to it. The written program can include algorithms and calculations necessary for the processing unit to render. When the processing unit or CPU rendered the calculations based on the written program it will then issue a command for the corresponding reaction engine to execute. The execution command to the reaction engine is transmitted by radio waves from the processing unit or CPU to the corresponding reaction engine.

8) A system according to claim 7, where the sensors that are attached to the looped track are wired to the input pins of the processor or CPU. The processor also has a number of output pins. When the processor receives a signal from the sensors attached to the looped track, and after processing and computing, the processor will activate one of the output pins with respect to the calculations and computing that has been executed. This activated output pin then generates a predetermined radio frequency or encoded message via a frequency channel for the corresponding reaction engine. Since plurality of reaction engines are moving along the looped track and also a number of command orders are needed to control the movement of reaction engines along different paths of the looped track, therefore accordingly sufficient number of output pins are required to send the correct command with respect to the reaction engines position along the looped track to its corresponding reaction engine. To avoid interference either different radio frequency for each output pin is required or by encoding each output pin and using one frequency channel we can transmit the correct command to each reaction engine separately and securely.

9) In order to have the privilege of adjusting the thrust force generated by this invention, the force magnitude acquired by each reaction engine during acceleration which is the movement of reaction engines along the first straight path of the looped track needs to be adjustable so when the operator sets the desired force magnitude needed, all reaction engines running at the first straight path of the looped track must have a uniform force magnitude applied to them therefore having the same acceleration. During this period all reaction engines must have a uniform predetermined force magnitude applied to them and this can be achieved by sending a unique radio frequency that represents the predetermined force magnitude to all reaction engines for the purpose of setting their acceleration to be uniform.

10) A system according to claim 1 and 6, where the said plurality of reaction engines arrive at the second straight path of the looped track for which they need to decelerate and reduce their speed which is done by activating the parachute or airbrake system. Once the reaction engines pass the sensors attached to the second straight path of the looped track the signal will be sent to the processor and the processor after rendering and calculating the speed of reaction engines will send the corresponding command to activate the parachute or airbrake system of the corresponding reaction engine. When the reaction engine reaches the bottom part of the second straight path of the looped track, the parachute or airbrake of the corresponding reaction engine will fold back or become deactivated.