WO1992000222A1 - Masse fluide en rotation pour acceleration par desequilibre gravitationnel - Google Patents

Masse fluide en rotation pour acceleration par desequilibre gravitationnel Download PDF

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Publication number
WO1992000222A1
WO1992000222A1 PCT/US1990/006270 US9006270W WO9200222A1 WO 1992000222 A1 WO1992000222 A1 WO 1992000222A1 US 9006270 W US9006270 W US 9006270W WO 9200222 A1 WO9200222 A1 WO 9200222A1
Authority
WO
WIPO (PCT)
Prior art keywords
fluid
centripical
acceleration
mass
imbalance
Prior art date
Application number
PCT/US1990/006270
Other languages
English (en)
Inventor
Dominick Dejoy, Jr.
Original Assignee
Dejoy Dominick Jr
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 Dejoy Dominick Jr filed Critical Dejoy Dominick Jr
Publication of WO1992000222A1 publication Critical patent/WO1992000222A1/fr

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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
    • F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03H99/00—Subject matter not provided for in other groups of this subclass
    • 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
    • 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

Definitions

  • CGIAFF is a device that generates a steady state centripical force imbalance that can be used for a cons cant acceleration drive system.
  • the device has utility in space craft drive systems as well as many other applications requiring a directed force.
  • Present and proposed propulsion systems utilize particle ejection at a means of propulsion. These systems use chemical combustion solid or liquid with the basic concept dating back to the Sung Empire. Proposed modern systems utilize magnetic or nuclear propulsion of particles. In all ejection systems the action of ejection causes a gravitational force imbalance between the rocket/vehicle and the half of the universe behind the vehicle and the half of the universe in front of the vehicle.
  • the device can wholly be explained by these two facts of existing accepted science. I am however obligated to give full disclosure of both theory and known facts regarding this device; This device was concieved based on my theory of Spherical Gravity Time which states that time is a spherical gravitational event where the rate of time "the resultant of the gravitational primary force" is represented everywhere in free space by the equation;
  • This spherical acceleration never gets a second second accelerating only to c. This is because the outer surface (the effective outer surface mass) is moving outwardly at c creating the outer surface of the universe at 4 ⁇ 3.1416 ⁇ c 2 . Thus the acceleration can only be up to c because the "surface Big Bang mass" generat ing the radius pull of c per sec 2 is moving out at c. This I believe generates an acceleration only to c in every direction.
  • the speed of light is not the speed of light; it is the rate of expantion (the creation of space) measured by the rate in which it moves light; it should be thought of as the rate of time in a given direction; light stands still; it is space that moves. That is, space is created by this spherical gravitational event.
  • This theory states that the bulk of the effective mass of this Universe is around its outer surface or has the effect of being around the outer surface; blown out by the Big Bang;
  • the fluid (4) is driven by motor effect around confinement path (O) through arc (A) and through arc (B), where (B) is of less volumetric capacity per centimeter than that of (A). Fluid (4) is forced through arc (B) at greater velocity than through arc (A).
  • the resutant (F) will be the manifestation of the greater centripical force of (B) overcoming the cetripical force of (A). (F) will be an accelaration capable of doing work.
  • Fluid (7) can be driven by semiteroidal coils (8) and (9) with (8) over arc (A) and (9) over arc (B).
  • Conductor brushes (10) and (11) located at 0 and 180 degrees.
  • coils (8) and (9) With current flowing from conductor brush (10) to (11) (or visa versa) through the fluid (7) coils (8) and (9) are energized with a current flowing in a direction that will cause side shift in fluid (7) pushing fluid (7) within arcs (A) and (B) in the same rotory direction.
  • Circle tube (T) (Diagram V) is of the same volumetric capacity for its entire circumferance. It is filled with fluid (12) Hg vapor or similar. At 0 and 180 degrees are located conductor brushes (13) and (14) that make electrical contact with fluid (12). Around circle tube (T) are sectional teroidal coils in this case (17 through 34) (more or less could be used). With electrical current flowing from (13) to (14) through fluid (12) forming a circuit; a current energizes a group of sectional teroidal coils equating to 180 degrees contemporanely all adjacent to each other such as (26 to 34) causing not only side shift in the total fluid (12) mass but also reduction of volumetric capacity of the section around the rim.
  • the arc of the energized sectional teroidal coils; through magnetic confinement creates a (B arc) as in previously described structural confinements (Diagram I).
  • the B side arc can be relocated anywhere around the rim by designating diferent groups of sectional teroidal coils as long as they encompass 180 degrees of the rim. The.
  • circle tube (O) is a CGIAFF as described herein powered and accelerating at a rate of 980 cm per sec 2
  • body ( H ) is a human that is being pulled/accelerated by (O) at the same rate as (O).
  • the resultant effect of gravitational drag acting on (H) pressing (H) against the structure of arc (A) will be the same local gravitational effect as of that experienced on earth for (H).
  • Circle Movement O have a diameter of 50cm
  • the cubic capacity of B is 1 /2 of A, Fluid in B must travel at 2 times the linear rate of A to maintain circular motion or;
  • Diagram IV Semiteroidal Centripical Gravitational Imbalance Acceleration Fluid Flywheel showing location of field coils and conductor brushes.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Plasma Technology (AREA)

Abstract

La présente invention a trait au domaine de la propulsion. Les systèmes de propulsion de l'art antérieur utilisaient l'éjection de particules pour provoquer une poussée dont il résultait de l'énergie perdue. La présente invention résout ce problème en utilisant le déséquilibre centripète d'un fluide en mouvement circulaire pour générer une accélération permanente. On utilise un tube en verre (Diagramme I) ayant la configuration d'un cercle (O), dont une moitié (B) possède une capacité volumétrique inférieure à l'autre moitié (A). A l'intérieur du tube, on fait couler un fluide, tel que du mercure (4), par effet magnéto-hydrodynamique (Diagramme II) dans la voie de confinement (O) à travers l'arc (A) et l'arc (B), l'arc (B) ayant une capacité volumétrique par centimètre inférieure à celle de l'arc (A). Le fluide (4) est poussé à travers l'arc (B) à une vitesse plus grande qu'à travers l'arc (A). La résultante (F) sera la manifestation du fait que la force centripète plus grande de (B) surmonte la force centripète de (A). La résultante (F) sera une accélération fonctionnelle.
PCT/US1990/006270 1990-06-29 1990-10-29 Masse fluide en rotation pour acceleration par desequilibre gravitationnel WO1992000222A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US54783490A 1990-06-29 1990-06-29
US547,834 1990-06-29

Publications (1)

Publication Number Publication Date
WO1992000222A1 true WO1992000222A1 (fr) 1992-01-09

Family

ID=24186341

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US1990/006270 WO1992000222A1 (fr) 1990-06-29 1990-10-29 Masse fluide en rotation pour acceleration par desequilibre gravitationnel

Country Status (2)

Country Link
AU (1) AU6968191A (fr)
WO (1) WO1992000222A1 (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1996034198A1 (fr) * 1995-04-28 1996-10-31 Ramirez Garcia Jose Systeme de propulsion base sur un desequilibre action-reaction
WO1997045639A1 (fr) * 1996-05-24 1997-12-04 Jury Bronislavovich Ekhin Methode permettant de transformer la rotation d'un corps solide en une force de traction lineaire et faisant appel a un procede desequilibre directionnel, et dispositifs de mise en oeuvre de cette methode
GR1002852B (el) * 1996-10-15 1998-02-06 Αυτοπροωθουμενη μηχανη με αξιοποιηση της ωθησης των ρευστων η οποια δημιουργειται απο ηλεκτροκινουμενες φτερωτες.
DE19713613A1 (de) * 1997-04-02 1998-10-08 Kai Kaehler Luftfahrzeug mit Auftriebsaggregat
WO2001009509A2 (fr) * 1999-07-29 2001-02-08 Nagarjuna Rao K Systeme antigravite

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU498476A1 (ru) * 1974-01-25 1976-01-05 Предприятие П/Я А-1742 Гиродвигатель

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU498476A1 (ru) * 1974-01-25 1976-01-05 Предприятие П/Я А-1742 Гиродвигатель

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1996034198A1 (fr) * 1995-04-28 1996-10-31 Ramirez Garcia Jose Systeme de propulsion base sur un desequilibre action-reaction
WO1997045639A1 (fr) * 1996-05-24 1997-12-04 Jury Bronislavovich Ekhin Methode permettant de transformer la rotation d'un corps solide en une force de traction lineaire et faisant appel a un procede desequilibre directionnel, et dispositifs de mise en oeuvre de cette methode
GR1002852B (el) * 1996-10-15 1998-02-06 Αυτοπροωθουμενη μηχανη με αξιοποιηση της ωθησης των ρευστων η οποια δημιουργειται απο ηλεκτροκινουμενες φτερωτες.
DE19713613A1 (de) * 1997-04-02 1998-10-08 Kai Kaehler Luftfahrzeug mit Auftriebsaggregat
WO2001009509A2 (fr) * 1999-07-29 2001-02-08 Nagarjuna Rao K Systeme antigravite
WO2001009509A3 (fr) * 1999-07-29 2001-08-23 Rao K Nagarjuna Systeme antigravite

Also Published As

Publication number Publication date
AU6968191A (en) 1992-01-23

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