WO2010116384A1 - Générateur de poussée et de couple sans masse de réaction - Google Patents

Générateur de poussée et de couple sans masse de réaction Download PDF

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Publication number
WO2010116384A1
WO2010116384A1 PCT/IN2010/000223 IN2010000223W WO2010116384A1 WO 2010116384 A1 WO2010116384 A1 WO 2010116384A1 IN 2010000223 W IN2010000223 W IN 2010000223W WO 2010116384 A1 WO2010116384 A1 WO 2010116384A1
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WO
WIPO (PCT)
Prior art keywords
gyro
spin
thrust
drive motor
ether
Prior art date
Application number
PCT/IN2010/000223
Other languages
English (en)
Inventor
Rakesh Goel
Original Assignee
S. K. Dynamics Pvt. Ltd.
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 S. K. Dynamics Pvt. Ltd. filed Critical S. K. Dynamics Pvt. Ltd.
Publication of WO2010116384A1 publication Critical patent/WO2010116384A1/fr

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Classifications

    • 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
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect

Definitions

  • the present invention relates to a Thrust and Torque Generator.
  • Thrust and Torque Generator which can generate sufficient continuous thrust or torque from electric power without using reaction mass.
  • the Thrust and Torque Generator of the present invention finds its major application in controlling orientation of satellites or space vehicles.
  • the present invention provides a device to generate Thrust and Torque in space at industrial and/or military and/or space temperature range from electric power without involving reaction mass.
  • the device for generating torque and thrust from electric power comprises of a main shaft and a cone assembly, where the cone assembly is supported on the main shaft and comprises of a spin drive motor and a precession drive motor.
  • the device further comprises of a plurality of magnetized gyro spinning wheels, wherein the gyro spinning wheels are rotated in spin motion by the spin drive motor and the cone assembly is rotated in precession motion by the precession drive motor.
  • the device further comprises of a gyro cover operatively connected to support the plurality of magnetized gyro spinning wheels and comprising a slot, wherein the spin motion and the precession motion causes leaking of ether through the slot.
  • the ether can also be leak through a guide duct operatively connected to the slot to generate the desired torque and thrust.
  • FIG 1 illustrates a Front view of a device according to an embodiment of the present invention.
  • FIG. 1 illustrates a Side view of a device according to an embodiment of the present invention.
  • FIG 3 illustrates a Bottom view of a device according to an embodiment of the present invention.
  • Fig 4 illustrates a Section view of a device according to an embodiment of the present invention.
  • Fig 5 illustrates a Section view of Motors and Bevel Gear assembly in a device according to an embodiment of the present invention.
  • Fig 6 illustrates Spin Wheels of a device according to an embodiment of the present invention.
  • Fig 7 illustrates an alternate design view of a device according to an embodiment of the present invention.
  • FIG 8 is a photograph of a device according to an embodiment of the present invention depicting a 6-spin wheels arrangement.
  • Fig 9 is a photograph of a device according to an embodiment of the present invention.
  • FIG 10 illustrates a device according to an embodiment of the present invention depicting a gyro cover with an ether guiding duct.
  • Fig 11 illustrates a device according to an embodiment of the present invention depicting an alternate arrangement for independent spin motors.
  • the present invention relates to a device for adjusting the orientation/attitude of a satellite. Unlike the existing art, the thrust and torque generator provided by the device is able to generate sufficient, desired, and continuous thrust or torque in space from electric power without using reaction mass.
  • ether The working of the present invention is based on generation of continuous thrust and/or torque by means of leaking of ether. All universe and empty space is filled with a different category of matter named as ether (M4).
  • the ether (M4) is transparent for other forms of matter, viz. Solid (Ml), Liquid (M2) & Gas (M3).
  • Ether is a media for Electro-Magnetic (EM) wave propagation and can flow like fluids. EM waves propagate transversely in ether and flow of ether generates magnetic flux.
  • EM Electro-Magnetic
  • Inertia is the property generated by magnetic induction due to acceleration and retardation in matter.
  • Ether is associated with objects and moves or drags as the object moves. However, there is a. relative motion between the object and its associated ether during acceleration or deceleration process, which is responsible for inertia.
  • Velocity of Transverse wave propagation in ether is equivalent to the speed of light demonstrating that ether has very low density and very high elasticity (bulk modulus).
  • Ether can contain huge energy in the form of flow and vibrations. A combination of magnetic flux, velocity, and vibration in ether can generate force in space by taking reaction from ether. This force is similar to gravitational force.
  • the relative motion between an object and its associated ether requires both acceleration and displacement in the same direction which is applicable in linear motion.
  • a rotary motion has centrifugal acceleration in radial direction, but there is no displacement in that direction. Therefore, the ether associated with object does not leak in constant speed rotary motion.
  • the inertia property is applicable while applying angular acceleration as both angular acceleration and angular displacement are present at that time and ether leaks during angular acceleration.
  • Figure 1 illustrates a front view of a device according to an embodiment of the present invention and depicts a mounting plate 1, a cone assembly 2, an upper cover 3 and spin wheel (gyro) covers, (6 in numbers) 4.
  • the mounting plate 1 forms the uppermost part of the device and supports the rest of the device.
  • the mounting plate 1 is fabricated from an aluminum alloy.
  • the cone assembly 2 has an upper cover 3 on its upper side and Spin wheel (gyro) covers 4 at its lower side.
  • the gyro covers 4 are 6 in numbers, each covering a single spin wheel.
  • the gyro covers 4 are fabricated from an aluminum alloy.
  • Figure 2 illustrates a side view of a device according to an embodiment of the present invention and depicts multiple holes 5 present on the rear side gyro covers 4.
  • the multiple holes 5 acts as an outlet for the leaking ether and helps in generating the desired thrust and a torque.
  • Figure 3 illustrates a bottom view of a device according to an embodiment of the present invention and depicts a hole / slot 6 at the bottom side of the gyro covers 4. As with the multiple holes 5, the hole/slot 6 also assist in the guiding the leaking ether out of the device.
  • Figure 4 illustrates a section view of a device according to an embodiment of the present invention and depicts a main shaft 12, a thrust bearing 7 at the bottom end of the device, ball bearings 8 and 11 to support cone assembly 2 on the main shaft 12, bevel gears 13 for spin wheels covered by the gyro covers 4, ball bearings 9 and 10 to support bevel gear assembly on the main shaft 8, a lower reflector 14, and a top magnetic coil 24.
  • Figure 5 illustrates a section view of motors and bevel gear assembly in a device according to an embodiment of the present invention and depicts a bevel gear 15 of the bevel gear assembly to drive spin wheels, an upper stator 16 for spin motor, a rotor 17 of spin motor, a lower stator 18 for precession drive motor, a rotor 19 of precession drive for rotating cone assembly 2, and a lower cover 20 for precession drive rotor 19 and cone assembly 2.
  • the rotor 17 of spin motor is a BLDC motor which is fabricated with twelve slot stator and sixteen pole rotor.
  • the rotor yoke is fabricated with mild steel and contains 16 pole magnets.
  • the bevel gear 15 is also constructed on this yoke.
  • the rotor 19 of precession drive is a BLDC motor which is fabricated with twelve slot stator and sixteen pole rotor.
  • the rotor yoke is fabricated with mild steel and contains sixteen pole magnets.
  • the lower cover of the mounting cone assembly contains this yoke.
  • Figure 6 illustrates a spin wheel shaft 21 in a device according to an embodiment of the present invention.
  • Figure 7 illustrates an alternative embodiment of the present invention and depicts an 8-spin wheels arrangement on the device.
  • the precession drive motor 22 is at the top of the device and lower reflector 14 is present towards the base of the device.
  • Figure 8 is an actual photograph of the device according to an embodiment of the present invention and depicts the device with a six-spin wheels arrangement.
  • Figure 9 provides a combined view of a drawing and an actual photograph of the device according to an embodiment of the present invention and depicts a two-spin wheels arrangement.
  • Figure 10 illustrates a detailed view of gyro covers in a device according to an embodiment of the present invention and depicts an ether guiding duct 23 and a hole / slot 6 at the bottom side of the gyro covers 4.
  • Figure 11 illustrates a device according to an embodiment of the present invention and depicts an alternate arrangement of spin motor in the device. More particularly, the present embodiment contemplates an arrangement where a single spin drive motor and necessary bevel gears can be done away with. The device, instead, has small spin motors on the shaft of each spinning wheel.
  • the cone assembly 2 is supported on the main shaft 12 using the upper cover 3 and the lower cover 20 with ball bearings 8 and 11.
  • the lower cover 20 acts as rotor to rotate the whole cone assembly 2.
  • the dual stator based motors, 16 and 18, provide the spin and precession drive, respectively.
  • the rotor 17 for spin motor also includes a bevel gear 15 and is mounted on the main shaft 12 with two ball bearings 9 and 10.
  • the spin motor and bevel gear 15 rotates in a counterclockwise direction while viewed from top, it rotates the bevel gears 13 and spin wheels in a counter-clockwise direction when viewed from their rear side of the spin wheels.
  • the precession motor is rotates in a clockwise direction, so the spin wheel speed is the sum of both motor speeds multiplied by the gear ratio.
  • the gyro spinning wheels of the device are rotated at speed above 10000 rpm by the spin drive motor and gear arrangement.
  • the cone, assembly 2 is rotated by precession drive motor 19 between 800 to 1500 rpm.
  • two BLDC control drives are used to control the spin and precession speeds. Both drives are operated from common DC bus to handle regeneration of one drive and dissipate energy in the other drive. Both the drives are controlled by software, which is executed on a computing device using specific software and GUI tools. As a result of the combined spin and precession speeds, ether leaks from the magnetized spinning rotors.
  • each gyro cover 4 has multiple holes 5 on its rear side and a bottom hole 6 for providing path to the leaking ether.
  • the leaking ether is guided to flow through the ether guide duct 23 as it (ether) comes out at slot / hole 6 of gyro cover 4.
  • the slot 6 with ether guide duct 23 can be positioned up, down or tangential to cone assembly 2 to get a down thrust, an up thrust or a torque, respectively.
  • the reflector 14 can also be used to guide the ether flow.
  • the reflector 14 is cylindrical or conical in shape.
  • a sinusoidal high voltage electric signal is applied on the reflector 14 to guide the leaking ether in a faster and efficient manner.
  • high current signal is applied on the top magnetic coil 24 of the device to apply additional energy to the ether to further improve the performance of ether flow.
  • the device is similar to a turbo-charger of automotive engines. Structural features of the device, thus, enable a continuous flow of ether, with suction from one side and exhaust on other side to generate a desired thrust and / or torque.
  • the spin wheels are fabricated from mild steel and magnets are mounted on it to construct multi- poles or monopole on the circumference.
  • the device of the present invention though designed to accommodate six spin wheels, could also accommodate two, three, four or six spin wheels, as was demonstrated during test experiments.
  • Figure 9 particularly depicts two-spin wheels arrangement for a device of the present invention. Therefore, number of spin wheels is not a limitation of the device of the present invention.
  • the device of the present invention can be configured to generate only torque without thrust by proper positioning the slot 6 of gyro cover 4.
  • a combination of two devices could be used in a manner that the torque generated by each one of them negates the effect of other.
  • two devices can be simultaneously used on two sides of a satellite to get good torque from thrust.
  • the present invention provides a device for correcting the orientation/ attitude of satellites and other space objects.
  • the present invention provides a device which uses electric power without using reaction mass.
  • the present invention provides a device that produces a desired combination of either thrust or torque or both.
  • the present invention provides a working device based on the Ether mechanism for generating the desired level of thrust and/or torque.

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

L'invention concerne un dispositif générateur de poussée et de couple dans l'espace dans des plages de température industrielles et/ou militaires et/ou spatiales à partir d'énergie électrique sans faire appel à une masse de réaction. Le dispositif générateur de poussée et de couple à partir d'énergie électrique comprend un arbre principal (12) et un ensemble cône (2), l'ensemble cône (2) étant porté par l'arbre principal (12) et comprenant un moteur d'entraînement en rotation et un moteur de précession (22). Le dispositif comprend en outre une pluralité de toupies gyroscopiques aimantées, les toupies gyroscopiques aimantées étant entraînées en rotation par le moteur d'entraînement en rotation et l'ensemble cône (2) étant animé d'un mouvement de précession par le moteur de précession (22). Le dispositif comprend en outre une coiffe gyroscopique (4) couplée de façon fonctionnelle de manière à porter les toupies gyroscopiques aimantées et comprenant une fente (6), le mouvement de rotation et le mouvement de précession occasionnant une fuite d'éther par la fente (6). La fuite d'éther peut également se faire par un conduit guide (23) couplé de façon fonctionnelle à la fente (6) de manière à générer le couple et la poussée recherchés.
PCT/IN2010/000223 2009-04-08 2010-04-05 Générateur de poussée et de couple sans masse de réaction WO2010116384A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
IN725DE2009 2009-04-08
IN725/DEL/2009 2009-04-08

Publications (1)

Publication Number Publication Date
WO2010116384A1 true WO2010116384A1 (fr) 2010-10-14

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Family Applications (1)

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PCT/IN2010/000223 WO2010116384A1 (fr) 2009-04-08 2010-04-05 Générateur de poussée et de couple sans masse de réaction

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107284690A (zh) * 2017-05-25 2017-10-24 上海卫星工程研究所 适用于sgcmg五棱锥立式布局的桁架支撑装置

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040035229A1 (en) * 2002-08-22 2004-02-26 Meffe Marc E. Radially actuated control moment gyroscope
WO2005095891A1 (fr) * 2004-04-02 2005-10-13 Eco Bond Trading Pte Ltd Appareil de gyroscope
WO2008155746A2 (fr) * 2007-01-11 2008-12-24 Torres Sanchez Edgar Ernesto Dispositif générateur d'une force de couple dans trois dimensions

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040035229A1 (en) * 2002-08-22 2004-02-26 Meffe Marc E. Radially actuated control moment gyroscope
WO2005095891A1 (fr) * 2004-04-02 2005-10-13 Eco Bond Trading Pte Ltd Appareil de gyroscope
WO2008155746A2 (fr) * 2007-01-11 2008-12-24 Torres Sanchez Edgar Ernesto Dispositif générateur d'une force de couple dans trois dimensions

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107284690A (zh) * 2017-05-25 2017-10-24 上海卫星工程研究所 适用于sgcmg五棱锥立式布局的桁架支撑装置

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