WO2008087500A1 - Moteur à turbine - Google Patents

Moteur à turbine Download PDF

Info

Publication number
WO2008087500A1
WO2008087500A1 PCT/IB2007/052812 IB2007052812W WO2008087500A1 WO 2008087500 A1 WO2008087500 A1 WO 2008087500A1 IB 2007052812 W IB2007052812 W IB 2007052812W WO 2008087500 A1 WO2008087500 A1 WO 2008087500A1
Authority
WO
WIPO (PCT)
Prior art keywords
vanes
disk
motor
pressure
high pressure
Prior art date
Application number
PCT/IB2007/052812
Other languages
English (en)
Inventor
Salman Gurbuz
Original Assignee
Salman Gurbuz
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
Priority claimed from TR2007/002442007/00244A external-priority patent/TR200700244A2/xx
Application filed by Salman Gurbuz filed Critical Salman Gurbuz
Publication of WO2008087500A1 publication Critical patent/WO2008087500A1/fr

Links

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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00—Geometry
    • F05B2250/10—Geometry two-dimensional
    • F05B2250/14—Geometry two-dimensional elliptical
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2250/00—Geometry
    • F05B2250/70—Shape

Definitions

  • the present invention relates to a turbine motor which increases the energy it takes in.
  • the present invention generates much more energy than it takes in by allowing high pressure fluids and gases through its specially-manufactured vanes. Following the first propulsion it operates without any need for power from an external supply as it supplies the required energy from its own resource. It is possible to install it at any power level. This is commonly known as infinite energy.
  • the present invention acts as a motor although it operates as a turbine. That is, the invention will take the place of the motors in the state of the art. That's why it can be called 'turbine motor'.
  • An R&D project is prepared in order to prove industrial applicability of this invention.
  • the subject matter of the invention is to increase energy taking advantage of liquid and gas pressure.
  • the ideal material is oil.
  • the producers may produce gas or liquids with special additives. This is not the case.
  • Our case is a TURBINE MOTOR operating on a circulation pump with a lkw electric motor thereon and raising one ton of oil to 40 atu pressure in one hour. This helps making comparisons.
  • Said motor can be used with all the motor vehicles, boats and planes, as well as in producing electricity.
  • Said motor can be operated vertically and horizontally. It is possible to obtain any size of power. Transport will mostly be done by airways. The airplanes can fly for thousands of hours. Transportation vehicles will be helicopters. And these will fly without pilots. The houses might be moved by choppers. Turbine motors can also be used instead of electric motors in plants after installing a pressurized liquid distribution and collection network. All of this may not sound late. But they will all come true. Thanks to easy application of said motor to all means it will be used in everywhere in the world in near future.
  • Figure 1 is a schematic view of the turbine motor with vanes in which the outer cabinet acts as a chassis.
  • Figure 2 is a cross-sectional schematic view of the system with vanes which operates on the two side surfaces of the two edges of a disk of the turbine motor.
  • Figure 3 is a full exterior view of the motor according to the invention.
  • FIG. 4 is a detailed view of the circulation pump and connecting pipes.
  • Figures 5 and 6 show the rotor group.
  • Figure 7 shows ball and spindle bearing for minimizing the friction within the disk channels.
  • FIG 8 shows non-contact state of the vanes. There are 48 vanes.
  • Figure 9 shows the disk lid.
  • Figure 10 is a perspective view of the cabinet of the pressure cells.
  • Figure 11 shows the low pressure and Figure 12 shows high pressure oil circulation conduits.
  • Figure 13 shows a group of rim (together with low pressure oil collection conduit), pin and bearing.
  • Figure 16 is a semi-exploded perspective view of the motor.
  • Figure 17 is a semi-exploded side view of the motor.
  • Figure 18 is a semi-exploded top view of the motor.
  • Figure 19 is a detailed view of low and high pressure zones.
  • Figure 20 is a top view of the vane paths for translating the vanes and bearings moving through said paths.
  • Figure 21 is a detailed view of the vane, describing active surface of the vanes exposed to pressure.
  • the turbine motor (1) operates in such a way that the vanes rotate the disk (5) in the direction of low pressure zone (3) after two of them being pressurized in the high pressure zone (4) in the course of vanes' movement, the vanes moving inward or outward in the order they are arranged on the outer surface of the disk (5) for enabling rotation.
  • the other two vanes (2) move in their order from low pressure zone (3) to high pressure zone at the same time in order to replace the others.
  • the rotational movement of the disk (5) is made continuous.
  • the disk (5) and the vanes (2) are arranged in two ways. In the first arrangement the vanes (2) can move towards the center of and away from the disk (5). And in the second the vanes (2) can move to the right and left, parallel to the central axis of the disk (5).
  • the rotational direction (D) in both arrangements is shown in the drawings.
  • volume (H) among the vanes (2) is 1 V sectioned while in the second the volume (H) is preferably rectangular.
  • fluid or gas within the volume (H) is transferred to the low pressure zone (3) after it finishes its function, the fluid or gas being used for rotating the turbine motor (1).
  • the circulation material, i.e. gas or fluid, within the low pressure zone (3) enables feedback of the pump by being sent back to the inlet of the circulation pump.
  • the movement of the vanes (2) in both embodiments is provided through the movement of bearings in a conduit in the middle of the vanes (2). Due to sine curve form of the conduit the back and forth or right- left movement of the vanes (2) is repeated. The crank methods that support this are well known by the manufacturers. The movement within the conduit by the vanes (2) will be supported from outside.
  • the number and distribution of the pressure cells (8) can be set to a desired power from the turbine motor (1). Following are the two examples of calculation indicating the power gain in case that the turbine motor (1) with 8 pressure cells (8) is run using a IkW circulation pump:
  • a motor of IkW compresses 2000kg water with 20atm pressure in an hour.
  • a motor of IkW compresses 2000kg water with 20atm pressure in an hour.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

La présente invention concerne un moteur à turbine d'énergie pour générer de l'énergie à l'infini. La présente invention vise à former des zones de basse et haute pression autour d'un disque ou d'un arbre à l'aide de fluide ou de gaz sous pression et à assurer la translation des aubes depuis une zone de haute pression vers une zone de basse pression. À cet effet, les extrémités des aubes adjacentes au châssis du moteur doivent être le plus possible de forme ovale. Ainsi les boîtiers d'aubes sont représentés sous une forme ovale dans les dessins. Le châssis doit être résistant à la pression ; et il est également prévu une pompe de circulation assurant la compression de fluide ou de gaz depuis une haute pression vers une basse pression.
PCT/IB2007/052812 2007-01-17 2007-07-13 Moteur à turbine WO2008087500A1 (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
TR2007/002442007/00244A TR200700244A2 (tr) 2007-01-17 2007-01-17 Türbin motorTürbin motor
TR2007/00244 2007-01-17
TR200704887 2007-07-12
TR2007/04887 2007-07-12

Publications (1)

Publication Number Publication Date
WO2008087500A1 true WO2008087500A1 (fr) 2008-07-24

Family

ID=38969891

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/IB2007/052812 WO2008087500A1 (fr) 2007-01-17 2007-07-13 Moteur à turbine

Country Status (1)

Country Link
WO (1) WO2008087500A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018084819A1 (fr) * 2016-11-01 2018-05-11 Salman Gurbuz Moteur fuelless - moteur ufo

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2108967A1 (fr) * 1970-10-23 1972-05-26 Thiriet Armand
DE19647476A1 (de) * 1996-11-16 1998-05-20 Manfred Klenk Pneumatisch hydraulischer Zentrifugalantrieb
DE10129830A1 (de) * 2000-07-13 2002-01-24 Johannes Van Berkum Hydraulische Strömungsmaschine
US20040159090A1 (en) * 2003-02-18 2004-08-19 Tavarez Harold A. Hydromagnetic inertial propulsion

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2108967A1 (fr) * 1970-10-23 1972-05-26 Thiriet Armand
DE19647476A1 (de) * 1996-11-16 1998-05-20 Manfred Klenk Pneumatisch hydraulischer Zentrifugalantrieb
DE10129830A1 (de) * 2000-07-13 2002-01-24 Johannes Van Berkum Hydraulische Strömungsmaschine
US20040159090A1 (en) * 2003-02-18 2004-08-19 Tavarez Harold A. Hydromagnetic inertial propulsion

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2018084819A1 (fr) * 2016-11-01 2018-05-11 Salman Gurbuz Moteur fuelless - moteur ufo

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