CA2345508A1 - Hydrogen rotary generator - Google Patents

Hydrogen rotary generator Download PDF

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Publication number
CA2345508A1
CA2345508A1 CA002345508A CA2345508A CA2345508A1 CA 2345508 A1 CA2345508 A1 CA 2345508A1 CA 002345508 A CA002345508 A CA 002345508A CA 2345508 A CA2345508 A CA 2345508A CA 2345508 A1 CA2345508 A1 CA 2345508A1
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CA
Canada
Prior art keywords
ring shaped
rotary
rotor
hydrogen
generator
Prior art date
Legal status (The legal status 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 status listed.)
Abandoned
Application number
CA002345508A
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French (fr)
Inventor
Florencio Neto Palma
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CA002345508A priority Critical patent/CA2345508A1/en
Publication of CA2345508A1 publication Critical patent/CA2345508A1/en
Abandoned legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
    • F02C5/04Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant the combustion chambers being formed at least partly in the turbine rotor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B43/00Engines characterised by operating on gaseous fuels; Plants including such engines
    • F02B43/10Engines or plants characterised by use of other specific gases, e.g. acetylene, oxyhydrogen
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K21/00Synchronous motors having permanent magnets; Synchronous generators having permanent magnets
    • H02K21/12Synchronous motors having permanent magnets; Synchronous generators having permanent magnets with stationary armatures and rotating magnets
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/08Structural association with bearings
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/18Structural association of electric generators with mechanical driving motors, e.g. with turbines
    • H02K7/1807Rotary generators
    • H02K7/1823Rotary generators structurally associated with turbines or similar engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B53/00Internal-combustion aspects of rotary-piston or oscillating-piston engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/50Bearings
    • F05D2240/51Magnetic
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/30Use of alternative fuels, e.g. biofuels
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Abstract

Hydrogen rotary generator comprising an aluminum alloy ring shaped rotor with permanent magnets interfaced radially and laterally by stationary electromagnets to provide a variable speed brush-less motor generator in which the rotor becomes self-centered within the contained electromagnetic fields to provide a virtual magnetic bearing while in operation. Radial and lateral roller bearings provide support for both the electric generator and the combustion engine ring shaped rotors during power off. The ring-shaped motor generator is directly interfaced to an integral stainless steel hydrogen combustion rotary engine rotor and stator with a plurality of complementary ignition chambers, which uses a mixture of hydrogen fuel and water to provide torque for the generation of electricity and high temperature steam exhaust. Condensed water form ambient air by air conditioners is collected for mixing with hydrogen fuel and supplied for the rotary combustion engine operation.
Optionally, the hydrogen rotary motor generator is capable of providing electricity and jet propulsion, according to specific adaptations to provide a wide range of applications such as: power plants for residential, industrial, automobiles, buses, trucks, trains, ships, flying robotics, airliner jet engines, recuperation applications in oil wells, oil sands garbage disposal and the like.

Description

TITLE: HYDROGEN ROTARY GENERATOR
FIELD OF THE INVENTION
The present invention is directed to a radially and laterally interfaced self-centering electric motor generator, forming an integral part of a directly interfaced ring-shaped hydrogen rotary combustion engine, capable of the production of electricity and jet propulsion at once.
BACKGROUND OF THE INVENTION
The perception that some day cars may run on air has been a vision for many years. The reasoning behind it is that moisture is constantly being released into the atmosphere in immense quantities, worldwide from an immense variety of sources, including humans and other animals. Conventional air conditioners condense the moisture in the air into water, which can be used by an electrolyser to produce hydrogen and oxygen for fuel. The combustion of hydrogen combining with oxygen back to water, after having done its work, creates energy.
Essentially, an air conditioner, an electrolyser and an electric generator, is all that is needed to complete the cycle of water to hydrogen and back to water. By converting the sun's energy into abundant electricity and hydrogen we have what it takes to complete this vision, for as long as the sun continues to power the atmosphere.
The need for environmentally clean energy sources is at the very foundation of a global effort to achieve a viable practical alternative to dwindling fossil fuels and environment pollution. Hydrogen has long been recognized the ideal clean form of fuel and electricity the ideal form of energy. The harnessing of the sun in its three basic forms of solar, wind and waves at once, day and night, the exploitation of the highest energy areas in the rivers and the oceans - directly into electricity and hydrogen fuel, is a distinct possibility.
The process of conversion of hydrogen fuel into electricity and torque to suit an immense scope of applications for residential and industrial power plants, transportation in its various forms, is also a distinct possibility according to this vision.
The eventual shifting from polluting fossil fuels technologies into clean hydrogen fuel technologies will obviously take many years to accomplish.
There have been numerous creative attempts at providing reliable alternative solutions to produce power at competitive costs with fossil fuels. Recently, solar power plants and windmill farms have been proposed as a viable alternative. However, they have drawbacks that may preclude them from becoming reliable long term solutions. These drawbacks include their reliance on intermittent energy sources, they clutter the landscape, they are vulnerable to inclement weather, are a threat to wild life, are costly to produce and maintain, rely on the high costs of fossil fuels for their proliferation.
The concepts of the fuel cell and the hydrogen rotary generator of the present invention represent a viable alternative. It is highly desirable to decentralize power generation as far as possible as a means to eliminate the need for power lines throughout the land and within cities. Atomic power plants, hydropower and thermal generation plants have contributed to the proliferation of power lines, which are costly to install and maintain, are a threat to wildlife and a major disruption to the landscape and the environment.
OBJECTS OF THE INVENTION
An object according to a preferred embodiment of the invention is to provide a ring shape variable speed brushless rotary motor generator, which operates self-centered to a contained electromagnetic field, to provide a magnetic bearing and form a complementary integral part of a rotary hydrogen combustion engine, that collects ambient air condensed water from the vehicle's air conditioner as a basic source for the production of hydrogen fuel and a mixture for the rotary combustion engine operation.
Another object is to provide a ring-shaped hydrogen rotary engine, in which the rotor and stator are fabricated from press-formed stainless steel sheet metal parts that are welded together to achieve a light weight, high temperature strong assembly, which is directly adapted to the inner face of the electric generator's stationary and rotor frames.
Another object is to optionally provide super magnets and super conductors to the brushless motor generator design.
Another object is to provide fan blades to the combustion rotary engine rotor that are press fitted into the electric motor generator ring shaped rotor cavities and specifically designed to cool both rotors and guide the thermal combustion steam exhaust into a ring shaped manifold, for air and jet propulsion.
Another object is to provide a common ring shaped stainless steel tubing manifold for both the hydrogen and water fuel, having threaded couplings matching those of the rotary combustion engine stator, which have a spring loaded steel sphere check valve for each individual manifold coupling in each combustion cavity.
Another object is to provide a common ring shape stainless steel tubing manifold having a high voltage conductor inside with threaded couplings matching those of each high-voltage coupling to the individual spark plugs in each combustion cavity of the rotary combustion engine stator.
Another object is to provide aluminum alloy ring shaped rotor castings specifically configured for the particular application of the electric motor generator.
Another object is to provide aluminum alloy ring shaped complementary stator covers specifically configured for the particular application of the electric motor generator.
Another object is to provide heat sink cooling fins at the inner rim surfaces of the electromagnetic stator covers that are cooled by the high speed air flow by the rotor vanes as a means to provide stator cooling.
Another object is to provide two semi-circular "U"
shaped stainless steel sheet metal electromagnetic containment shields that are press fitted over the complementary aluminum alloy stator covers assembly.
Another object is to provide spring loaded Teflon sealing rings to enclose the ring shaped electric motor generator and form a watertight assembly.
Another object is to provide roller bearings that are specifically designed to provide both radial and lateral support of the rotary electric and combustion engine rotors when on the electric power off mode.
Another object is to provide a ring shaped exhaust manifold to contain and mix the high- pressure, high-temperature steam exhaust according to specific operating temperature and volume levels.
SUMMARY OF THE INVENTION
The hydrogen rotary generator according to a preferred embodiment of the invention is a variable speed, brushless, ring shaped electric motor generator having radial and lateral stator electromagnets installed within aluminum alloy complementary enclosing stator covers and permanent magnets installed in a ring shaped aluminum alloy rotor. The rotor is supported radially and laterally by roller bearings during the power off and self-centering during power ON. Electromagnetic fields form a virtual magnetic bearing, sealed watertight by means of a spring loaded Teflon sealing ring. A semi-circular "U" shaped stainless steel cover is press fitted over the stator cover assembly and fitted with a stand to provide electromagnetic field containment and provide support for the hydrogen rotary generator assembly.
A integral ring shaped hydrogen rotary combustion chamber rotor having slated vanes is press fitted into corresponding slots molded into the electric generator's ring shaped rotor inner face and locked in position by two lateral snap rings. Two stainless steel side covers that are fitted and bolted over the electric motor generator's electromagnetic containment shield, laterally support a complementary stationary ring shaped inner combustion stator. Punch pressed cut outs in the stator side covers provide for air-cooling of the electric generator forced by the rotor slanted vanes and hot steam exhaust from the stator combustion chambers into a ring shaped manifold. The rotary combustion engine stator is interfaced to a lateral stainless steel tubing ring shaped manifold with threaded couplings to a plurality of individual combustion chamber ports. Each manifold coupling has a stainless steel spring loaded sphere check valve to ensure proper distribution of hydrogen fuel and water injection mixture to prevent flame from entering the manifold fuel source. The hydrogen and water supply is computer controlled according to specific interface inputs by servo valves. A plurality of spark plugs also coupled to the same side of the combustion chamber are interfaced to an ignition manifold formed from stainless steel tubing having threaded couplings for each combustion chamber spark plug and a high voltage wire inside for the spark plugs to fire all at once. The combustion exhaust ports are located at the opposite side of the fuel and ignition manifolds and are optionally connected into a ring shaped manifold or, for discharge directly into the atmosphere, or for air and jet engine like operation means of propulsion, depending on application. A ring shaped air intake shutter valve provides a means to control the airflow displaced by the propeller and a radially pivoted shutter provides control of the exhaust mixture for operation of the hydrogen rotary generator to function simultaneously as an electric generator and a jet propulsion engine that combines the ignition of hydrogen fuel with the moisture in the air to achieve jet propulsion.
The variable speed, brush-less electric motor generator operates self-centered by a virtual electromagnetic bearing while on power ON operation. The hydrogen combustion rotor is also self-centering by firing on all cylinders at once. The radial and lateral support roller bearings are common to both the rotary generator and combustion engine rotors in the power OFF
mode of operation. Hydrogen and distilled water being a clean fuel, makes the hydrogen rotary generator very desirable and a reliable source of energy up to very large scales for a very wide scope of potential applications, worldwide.
The hydrogen rotary combustion engine according to the embodiment of the present invention has fuel and ignition manifolds that are adapted to fire all chambers at once. Radial and tangential forces are generated as the hydrogen fuel is ignited by the spark plugs and the heat evaporates the water mixture into hot steam to cool down the engine. As the gas expands the tangential force, forces the rotor chamber to react against the stator chambers and to turn clockwise, and the hot gas to be exhausted through the respective exhaust ports in line, as it prepares for the next cycle. A simple and logical operation process machine, in which the speed can be precisely computer controlled and the output voltage frequency provide a precise reference to fire the spark plugs, the timing of the hydrogen fuel and water servo valves. The air intake and exhaust control valves are also computer controlled to complement harmony of operation with reference to other transducers such as temperature, exhaust speed, power output and the like as deemed necessary.
BRIEF DESCRIPTION OF THE DRAWINGS
Preferred embodiments of the present invention illustrated in the attached drawings in which:
FIG. 1 is an elevation rear view of a hydrogen rotary generator according to a preferred embodiment of the invention.
_ 7 _ FIG. 2 is a perspective sectional view of the ring shaped exhaust manifold.
FIG. 3 is a perspective view of the air intake ring shape shutter control valve.
FIG. 4 is a front elevation view of the hydrogen rotary generator in FIG. 1 the exhaust is coupled to an air conditioner and hydrogen source 39 to form a control loop for the recycling of air moisture for production of electricity and hydrogen fuel and propulsion;
FIG. 5 is a front sectional view of the ring shaped hydrogen rotary generator of FIG. 1 to show the relative position of the main components;
FIG. 6 is a side sectional view of the exhaust side cover;
FIG. 7 is an elevation side view of the ring shaped hydrogen combustion engine rotor with a cut out section to show the configuration of the internal design;
FIG. 8 is an elevation side view of the ring shaped hydrogen combustion engine stator with a cut out section to show the configuration of the internal design.
FIG. 9 is a side view of a cut out section of the air intake side cover;
FIG. 10 is an elevation view of the ring shaped electric motor generator stator aluminum alloy casting left cover;
FIG. 11 is an elevation front sectional view of the ring shaped electric motor generator aluminum alloy casting;
FIG. 12 is an elevation sectional view of the complementary ring shaped electric motor generator stator aluminum alloy right cover casting;
FIG. 13 is a sectional view of the semicircular stainless steel ring shaped cover of the electric motor generator electromagnetic fields containment;
FIG. 14 is an elevation view of the ring shaped ignition manifold;
_ g _ FIG. 15 is an elevation view of the ring shaped fuel manifold;
FIG. 16 is a sectional view of one coupling of the fuel manifold to show the spring loaded ball check valve within;
FIG. 17 is a sectional view of the ring shaped stainless steel bearing track installed into the electric generator aluminum alloy stator covers;
FIG. 18 is a sectional view of the ring shaped stainless steel roller bearing racer that provides radial and lateral support of both the electric and combustion rotors in the power OFF mode, on both sides;
FIG. 19 is a sectional view of the ring shaped stainless steel bearing track installed into the electric generator aluminum alloy rotor on both sides;
FIG. 20 is a sectional view of a ring shaped Teflon watertight seal installed into both side covers;
FIG. 21 is a specially shaped stainless steel wire compression spring for the Teflon sealing ring;
FIG. 22 is an elevation view of an optional exhaust shutter control valve for jet propulsion applications of the hydrogen rotary generator such as for powering airliners;
FIG. 23 is an elevation view of one exhaust shutter segment of FIG. 22;
FIG. 24 is an elevation view of a complementary exhaust shutter segment;
FIG. 25 is a view of a pair of radially interfacing spring-loaded hinging shutter pivots; and FIG. 26 is a simplified example of the rotary engine operation principle model.
DESCRIPTION OF THE PREFERRED EMBODIMENTS

The ring shaped hydrogen rotary generator apparatus according to a preferred embodiment of the present invention is generally shown as 10 in FIG. 1 and FIG. 4 to better illustrate its overall configuration.
FIG. 1 is an elevation rear view of a "U" ring shaped stainless steel frame better shown by FIG. 13 provides a containment shield for the electric generator electromagnetic fields and a clamping reinforcing frame for the stator assembly of the hydrogen rotary generator..
Joint cover 12 is a stainless steel "U" shaped section bolted over to seal and secure the two semicircular frames. Hydrogen combustion exhaust collector manifold 13 is better seen in FIG. 2, which is bolted down in position by a plurality of bolts 14. Exhaust manifold 13 has port 15 to permit collecting the exhaust steam for recycling according to specific applications, including back to water and hydrogen fuel. Hydrogen combustion stator 16 better shown in FIG. 8 is also bolted down by the plurality of bolts 14. A stainless steel standing bracket 17 provides support for the hydrogen rotary generator assembly, for the fuel manifold 18, ignition manifold 19, better illustrated by FIG 14 and FIG. 15 respectively and an electrical power outlet junction box 20, is bolted to the ring shaped assembly 11 by a plurality of bolts 21 and down to the floor by a plurality of bolts 22.
FIG. 2 is a stainless steel ring shaped exhaust manifold generally shown as 13 with an exhaust port 15, which is bolted down to the hydrogen rotary generator side cover generally shown as 23 in FIG 6. The port 15 permits to collect all the steam exhaust for recycling into specific applications, including production of extra hydrogen fuel production.

FIG. 3 is a stainless steel sheet metal ring shaped air intake shutter valve generally shown as 25 having a plurality of punch press formed air inlet shown by arrows 29 through ports 26, which is operated by a bivoted coupling 27 and a servo motor 28, better illustrated by FIG. 4 with a rim fold 30 to contain shutter 25.
FIG. 4 is a front view of the hydrogen rotary generator of FIG. 1 to better illustrate the overall embodiment concept. An air conditioner or heat pump 31 collects moisture from the air 32 and delivers the condensed water 33 to servo valve 34 through check valve 35 and into fuel supply manifold 19. Heat pump 31 is supplied with electricity by the hydrogen rotary generator 10 power lines 36 through transformer 37. A
supply of hydrogen fuel 39 through servo valves 40 and check valve 41 into hydrogen fuel manifold 19 according to computer control programs provide a power control means.
FIG. 5 is a front sectional view of the ring shaped hydrogen rotary generator to better show the relative position and configuration of the respective component parts with arrow 45 showing a clockwise rotation of the complementary rotors by reacting against the respective stators. Air intake valve 25 controls the airflow 29 forced by a plurality of slanted impeller blades 46 and mixed with exhaust water vapor arrow 47 into ring manifold 15 and mixed as exhaust arrow 48. The rotary engine rotor is generally shown as 50 in FIG. 7 with a plurality of wedge shaped ignition chambers 51 and slated vanes 46 which are fabricated from stainless steel sheet metal plate welded together into a precision single piece. A small gap 52 separates the ring shaped rotor 50 from the stator generally shown as 16 by FIG. 8 with a plurality of wedge shaped ignition chambers, which are complementary in size and shape to those in the rotor. A
plurality of spark plug ports 54 and hydrogen and water ports 55, one of each for each camber, provide the combustion according to computer control firing angle.
Stainless steel stationary side plate generally shown in a cut as 56 in FIG. 9 has air inlet cutouts 26 for circulation of ambient air 29 and support of shutter valve 25 of FIG. 3, which provides an enclosure frame wall to interface the rotary engine stator with the electrical motor generator stator. Stainless steel stationary side plate generally shown in a section as 23 in FIG. 6, which is complementary to the stationary plate 56 of FIG. 9 by providing an enclosure frame wall to mix the inlet ambient air 29 and exhaust steam 47 into manifold 15 as shown by arrow 48. Both side plates 23 and 56 are bolted down to interface the electric generator and combustion engine stator ring shaped frames by means of a plurality of indexing pins 57 and screws 58 to form a precision firm strong assembly.
Starting now at the bottom we have a stainless steel mounting bracket 17 with mounting port 22 and a motor generator electric wire junction box 20 for stator wires 59 from the radial stator cores 60 and the complementary lateral stators cores 61 and 61A, which are assembled within complementary aluminum alloy stator covers 62 and 62A joined at gap by "U" shaped semi-circular stainless steel frame 11. Wires 59 lead to the respective stator induction coils 60, 61 and 61A to form electromagnets, which react with the corresponding magnets 64, 65 and 65A
assembled on the ring shaped aluminum alloy electric motor generator rotor, to produce an alternating voltage which frequency is dependent on RPM. A plurality of snap rings 67 ensure that the press fitted and cemented magnets will never come apart. Rotor 66 is radially and laterally supported by a special design of stainless steel roller bearings 68, which components are better illustrated by FIGS. 17, 11 and 19. Teflon sealing rings 69 installed on both stationary covers form a watertight assembly with rotor 66 better shown in FIG. 20. Air cooling fins 70 provide a heat sink for the electric motor generator cooling by force ambient air 29.
FIG. 6 is a elevation inner side view of the stationary lateral stainless steel plate with a plurality of ports for intake air 29 and exhaust 47 stator exhaust ports 71 better shown in FIG. 8 and indexing pins 57 and screws 58 to achieve a precise firm assembly.
FIG. 7 is an elevation view of the ring shaped hydrogen combustion engine rotor, which is built from punch press cut stainless steel plate parts welded together to achieve a precise and strong assembly rated for the specific application, having a plurality of slanted vane propeller, which the amount of displacement is specifically adapted for the specific application. A
plurality of wedge shaped ignition chambers 51 are bridged by a corresponding number of walls 72 are shown through a cutout of laterally welded walls 73 on both sides and radially reinforced by at least one raw of strut wall sections 74 also welded to an outer wall 75 with the slanted vanes 46 welded on according to a jig to ensure a precise and strong stainless steel plate assemble specifically rated for a particular operating temperature and displacement according to a specific amount of hydrogen fuel and water mixture.
FIG. 8 is an elevation view of the complementary ring shaped stator generally shown as 16 having complementary wedge shaped ignition chambers 53 and exhaust ports 71, are shown by a cutout of inner wall 16, lateral walls 76 and 77 and at least one raw of strut wall sections 78 which is also built from punch pressed steel plate parts in a similar process of the complementary rotor and having a plurality of manifold ports 54 and 55 for the supply of fuel and ignition.
FIG. 9 is an elevation sectional view of the ring shaped stainless steel ambient air inlet, fuel and ignition manifold lateral plate generally shown as 56 having ports 26 with rim walls 79 and 80, a plurality of indexing pins 57 and ports 54 and 55 for the respective manifolds of FIG. 8 and 58 for the assembly screws so as to form a precision strong assembly.
FIG. 10 is an elevation sectional view of the ring shaped aluminum alloy casting stator cover of the electric motor generator generally shown as 62 having a plurality of cooling fins 70 and radial and lateral stator core assembly 60, 61,61A guide frames generally shown as 81,81A and 82,82A with lateral support ridges and screw ports 83 respectively to bolt down the stator sections to the covers 62 and 62A. Teflon ring radial cavities 85 and 85A shown in FIG. 20 and roller bearing tracks with retaining grooves 87 and 87A for a stainless steel track cover 88 shown in FIG. 17 in a section.
Ambient air-cooling arrows 29 are shown flowing through fines 70.
FIG. 11 is an elevation sectional view of the ring shaped aluminum alloy casting rotor generally shown as 66 having a plurality of slanted cavities 89 to match the press fitted slated vanes 46 of ring shaped combustion rotor 50 and locked in position by lateral snap rings into ring shaped cavities generally numbered 90, which are similarly used for locking in the respective permanent magnets 64, 65 and 65A in position to form a precision strong assembly. Ring shaped cavities 91 and 92 serve to insert a specially formed stainless steel track 93 for the radial and lateral roller bearing according to FIG. 19.
FIG. 12 is an elevation sectional mirror image view of the complementary stator ring shaped cover described in FIG. 10.
FIG. 13 is a sectional view of the stainless steel electromagnetic containment semi-circular press fitted ring 11 over stator covers 62 and 62A assembly with ports for 57 and 58 for the assembly of the side covers 23 and 56 of FIGS. 6 and 9 respectively.
FIG. 14 is an ignition manifold 19 made of stainless steel tubing with a main coupling 93 which splits into a plurality of threaded couplings 94 that are specifically aligned to the respective spark plugs, fired in all chambers at once.
FIG. 15 is a fuel supply manifold 18 made of stainless steel tubing with a main port 95 which splits into a plurality of threaded couplings 96 that are specifically aligned to the respective fuel port couplings for ignition of all chambers at once. The manifold threaded couplings are all fitted with a spring loaded check valve to prevent flame from entering into the fuel line.
FIG. 16 is a sectional view of threaded couplings 95 and 96 to show the spring-loaded check valve design within, having a spring 97 and a steel ball valve 98.
FIG. 17 is a sectional view of a ring shaped stainless steel roller bearing track 88, which is fitted on the electric generator stator covers 62 and 62A
grooves 87 and 87A.
FIG. 18 is a sectional view of a special ring shaped roller bearing design 68 with a plurality of steel chrome plated rollers 99 to provide both radial and lateral support of both the generator and combustion engine rotors in the power OFF mode of operation, since on power ON the electromagnetic fields self-centers the rotors into a virtual electromagnetic bearing.
FIG. 19 is a sectional view of a special ring shaped stainless steel roller bearing track 93, which is fitted inside the generator 66 rotor into grooves 91 and 92 on both sides FIG. 20 is a sectional view of a ring shaped Teflon sealing ring 69 having a plurality of V shaped indexing protrusions 100 to prevent the seal from turning in the respective cavities 85 and 85A, which are compressed by a special wire spring design inside of the stator covers 62 and 62A.
FIG 21 is a section of a stainless steel special compression spring design, which is wrapped into a ring shape and laid under the Teflon sealing rings.
FIG. 22 is an elevation overall view of an optional stainless steel shutter 101 for the rotary hydrogen combustion engine 10, potential electricity and jet propulsion applications, such as for the powering of airliners and other suitable applications according to automatic computer control of a plurality of shutter vanes 102 and 103 alternately, which are interlocked internally by spring loaded hinging pivots 104 into a support ring shaped stainless steel plate with a plurality of pivoting frames 105.
FIG. 23 is an elevation view of one shutter vane 102 having a pivoted coupling frame 106 to a servomotor to permit to control the position of all other inter-coupled vanes 102 and 103 alternatively. The basic difference of shutter vane 102 and 103 is in the direction in the folding of the edges upward and downward as shown by the arrows 107 and 108 so that they are reinforced and can intermesh when they are operated inward or outward.

FIG. 24 is an elevation view of a complementary shutter vane 103 with downward side folding edges 108.
These vanes can be press formed from a single piece of stainless steel plate and the frames 101 and 105 and welded into a precise strong assembly.
FIG. 25 is a pair of inter-coupling hexagonal shaped spring-loaded pivots 104, which have four inter-matching prongs to form a circular pivoting hinge having a lateral cavity 109 to permit compressing them against the spring for assembly into the shutter vanes 102 and 103 and the supporting cavities in frames 105.
FIG. 26 is a simplified example of the ring shaped rotary combustion engine operating principle: When wedge shaped chambers 51 of the rotor are aligned with stationary complementary chambers 53 of the stator and an hydrogen and water ignition explosion takes place inside, the rotor chambers 51 are forced forward against the stationary chambers 53, as they are pushed forward by the compressed steam, which is exhausted through the exhaust ports 71 and some through gap 52, as they come in alignment for the next explosion, forcing the rotor in direction 45.
There are potential applications where the clean combustion of hydrogen rotary generators for the generation of electricity has important advantages over the cool operation of fuel cells, such as in residential and industrial buildings, automobiles, buses, trains, airplanes, vessels, and more particularly as a means to extract oil from oil wells and oil sands. In these applications the release of clean heated steam becomes a complementary byproduct, which limits the advantage of cool power production of the fuel cell to a very narrow and temporary advantage. Overall, the robustness and simplicity of construction of the hydrogen rotary generator, its versatility and unique ability to scale up to immensely powerful machines. Despite its original promise, much like solar and wind energy harnessing technologies, fuel cells are limited in comparison with the hydrogen rotary generator technology ability to generate electricity, propulsion and many other specific adaptations.
The immense scope of potential applications for the hydrogen rotary motor generator and the basic hydrogen rotary engine by itself as a source of torque is phenomenal. The mass production of electromagnetic propellers, hydrogen rotary generators and hydrogen rotary engines will likely stimulate an industrial revolution of its own with many new spin-off technologies. Meanwhile the demand for fossil fuels and their phasing out will continue for many years.
Ironically with hydrogen fuel assisting in the recuperation of oil and gas and their valuation, and as a contribution to reduced environmental pollution. The synergies for profit and the phasing out of fossil fuels by the corporations presently engaged in oil and gas exploration - are immense.
The brushless motor generator according to the hydrogen rotary generator of the present invention has previously been described in detail in a previous invention disclosure recently filed for patent in the Canadian Patent Office under the name of Robotic Mobile and referred to as electromagnetic propeller. The present invention adds an integral ring-shaped hydrogen rotary combustion engine that uses a mixture of hydrogen and water to provide torque and propulsion, which can be specifically adapted to a very wide rage of specific applications from small power to very powerful applications, with super magnets and super conductor applications to electric motor generator. An integral hydrogen rotary motor generator adapted for electric powered automobiles, buses, trucks, residences, industrial applications, airliners, boats and the like according to the following embodiments of the present invention will be discussed next.
There are potential applications where the clean combustion of hydrogen rotary generators for the generation of electricity has important advantages over the cool operation of fuel cells, such as in residential and industrial buildings, automobiles, buses, trains, airplanes, vessels, and more particularly as a means to extract oil from oil wells and oil sands. In these applications the release of clean heated steam becomes a complementary byproduct, which limits the advantage of cool power production of the fuel cell to a very narrow and temporary advantage. Overall, the robustness and simplicity of construction of the hydrogen rotary generator, its versatility and unique ability to scale up to immensely powerful machines. Despite its original promise, much like solar and wind energy harnessing technologies, fuel cells are limited in comparison with the hydrogen rotary generator technology ability to generate electricity, propulsion and many other specific adaptations.
The immense scope of potential applications for the hydrogen rotary motor generator and the basic hydrogen rotary engine by itself as a source of torque is phenomenal. The mass production of electromagnetic propellers, hydrogen rotary generators and hydrogen rotary engines will likely stimulate an industrial revolution of its own with many new spin-off technologies. Meanwhile the demand for fossil fuels and their phasing out will continue for many years.
Ironically with hydrogen fuel assisting in the recuperation of oil and gas and their valuation, and as a contribution to reduced environmental pollution. The synergies for profit and the phasing out of fossil fuels by the corporations presently engaged in oil and gas exploration - are immense.
The brush less motor generator according to the hydrogen rotary generator of the present invention has previously been described in detail in a previous invention disclosure recently filed for patent in the Canadian Patent Office under the name of Robotic Mobile and referred to as electromagnetic propeller. The present invention adds an integral ring-shaped hydrogen rotary combustion engine that uses a mixture of hydrogen and water to provide torque and propulsion, which can be specifically adapted to a very wide rage of specific applications from small power to very powerful applications, with super magnets and super conductor applications to electric motor generator. An integral hydrogen rotary motor generator adapted for electric powered automobiles, buses, trucks, residences, industrial applications, airliners, boats and the like according to the following embodiments of the present invention will be discussed next.
This hydrogen rotary generator is a precise clean burning engine, configured for maximum efficiency of operation by recuperating the combustion exhaust for a wide scope of specific applications, including heating of residential, industrial, transportation, recuperation of oil from oil wells, oil sand, recycling of garbage and so on.

It will be recognized and appreciated that the basic hydrogen rotary generator can be inverted and that the electric motor generator and the rotary engine can be designed to operate individually with minor modifications to the present design to suite a wide variety of potential applications without departing from the spirit of the present invention.
In accordance with the provisions of the patent statutes, the principle and mode of operation of the invention have been explained and illustrated in its preferred embodiment. However, it must be understood that the invention may be practiced otherwise than as specifically illustrated and described without departing from its spirit or scope.

Claims (9)

1. A hydrogen rotary generator apparatus comprising:
aluminum alloy ring shaped brush-less electric motor generator rotor with permanent magnets interfaced radially and laterally by stationary electromagnets, which provide a virtual self-centering electromagnetic bearing while in operation;
radial and lateral roller bearings to provide support for both the electric generator and the rotary combustion engine ring shaped rotors during the power off;
a ring shaped electric generator rotor that is directly interfaced to a rotary ring shaped combustion engine having a plurality of slanted vanes to provide cooling of the electric generator and propeller for mixing of ambient air with the engine exhaust manifold;
a ring shaped rotary combustion engine rotor having a plurality of internal wedge shaped ignition chambers that react with complementary chambers on a ring shaped stator;
a ring shaped rotary combustion engine stator having a plurality of wedge shaped combustion chambers complementary spaced to a ring shaped rotor and also having ports for fuel and spark plugs couplings and for combustion exhaust ports;
a ring shaped air intake shutter valve installed within the lateral interfacing walls of the electric generator and combustion engine sidewall;
a ring shaped exhaust-collecting manifold that mixes the combustion exhaust with ambient air according to specific proportions and applications;
a computer controlled combustion exhaust shutter valve working in symbiosis with an ambient air intake shutter valve to provide jet propulsion output control according to reference to a plurality of specific transducer interfaces;
a ring shape stainless steel tubing fuel manifold having a plurality of spring-loaded check valves to suit a plurality of ignition stator chambers;
a ring shaped stainless steel tubing ignition manifold having a high voltage cable inside with a plurality of couplings to suit a plurality of spark plugs;
a stand that provides coupling means for the fuel, ignition and electrical wires;
a "V" shape inner face Teflon sealing rings with lateral protrusions compressed by a radial wire spring;
a ring shaped brush-less electric motor generator assembly comprising a rotor and a stator of aluminum alloy molded parts;
a ring shaped rotary combustion engine assembly comprising a rotor and a stator of stainless steel plate parts welded together;
a "U" shaped stainless steel plate semi-circular cover with electromagnetic containment properties and providing a mounting frame for the interfacing of a rotary combustion engine;
2. The apparatus according to claim 1 wherein the electric motor generator can optionally operate individually and interfaced to propellers, shafts and the like.
3. The apparatus according to claim 2 wherein the electric motor generator basic design can be reversed by having the rotor forming an outer ring shaped rotor.
4. The apparatus according to claim 1 wherein the rotary combustion engine can optionally operate individually by providing the bearing to the rotor rim cover.
5. The apparatus according to claim 4 wherein the basic rotary combustion engine can be reversed by having the rotor forming an inner ring shaped rotor that can be adapted to propellers, shafts and the like.
6. The apparatus according to claim 1 wherein the hydrogen rotary generator can be scaled in models ranging in power output from small to immensely large units for stationary residential and industrial power to a very wide range of potential applications.
7. The apparatus according to claim 4 wherein the hydrogen rotary generator can be applied to a very wide scope of applications to the transportation industry, including automobiles, buses, trucks, trains, vessels, helicopters, airplanes and airliners.
8. The apparatus according to claim 6 wherein the hydrogen rotary generator can be applied to recuperation of oil from wells and tar sands by taking advantage from its precisely controlled pressure and hot exhaust temperatures and electric power output.
9. The apparatus according to claim 8 wherein the hydrogen rotary engine is specifically adapted for the recycling and incineration of garbage and recuperation of its byproducts in environmental friendly ways, by their combined energy.
CA002345508A 2001-04-26 2001-04-26 Hydrogen rotary generator Abandoned CA2345508A1 (en)

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7556015B2 (en) 2004-05-20 2009-07-07 Staffend Gilbert S Rotary device for use in an engine
WO2012156593A1 (en) * 2011-05-16 2012-11-22 Bernard Perriere Electric current generating turbine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7556015B2 (en) 2004-05-20 2009-07-07 Staffend Gilbert S Rotary device for use in an engine
WO2012156593A1 (en) * 2011-05-16 2012-11-22 Bernard Perriere Electric current generating turbine
FR2975546A1 (en) * 2011-05-16 2012-11-23 Bernard Perriere TURBINE GENERATING ELECTRICAL CURRENT
CN103765734A (en) * 2011-05-16 2014-04-30 塞弗工程公司 Electric current generating turbine
US10066605B2 (en) 2011-05-16 2018-09-04 Save Innovations Electric current generating turbine

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