Combined hydrodynamic - inertial rotoset - selfbooster

Abstract

The Combined Hydrodynamic-Inertial Rotoset-Selfbooster is a non-fuel power unit which includes: the hydrodynamic vane-fairing inertial rotor placed inside a closed loop tubular tunnel; a hydraulic module with a rotary pump propelling operative liquid in selfboosting manner to drive said rotor, cavitation preventor, and the electromechanical structure with the starter, electric output generator, storage battery, charger, drives, cooler, meters, control. The total combined rotor's torque is a sum of selfboosting hydrodynamic portion, and selfboosting inertial portion of the common integrated power produced simultaneously by the united rotor. The technology of rotoset-selfbooster can comprise various designes including mono- and poly-tunnel-rotor sets with a wide varieties of operative liquids, rotary pumps, and output power structures. The total power ratio is about 7.5 depending on design and KW required.

Description

CROSS-REFERENCE OF RELATED APPLICATIONS

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FEDERALLY SPONSORED RESEARCH

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SEQUENCE LISTING OR PROGRAM

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BACKGROUND OF THE INVENTION

This proposal relates to hydrodynamic and mechanical inertial disk rotor devices. It also relates to energy integrating systems with high power ratio of effective selfboosting technologies with limited losses.

The general idea and approach are similar to some closed testing wind and water fluidynamic tunnels with their well-known high energy ratios, which never were used as regular sources of power.

The method and principle of this proposal are near to the patent application Ser. No. 11/399,661 entitled HYDRODYNAMIC CLOSED LOOP TURBOSET-SELFBOOSTER filed Apr. 7, 2006 and published Feb. 22, 2007 by the US PTO under number 20070041830.

Said turboset, developed by present author, is based on liquid flow driving axial bispindle wing-turbines in closed loop tubular circuit. The general idea of said turboset and present proposal is philosophically similar to selfboosting cordial structures of humans and animals. The said cordial systems can be considered as a prior art-idea to the present proposal, as an idea granted by our mother-nature.

In the current proposal the ring-selfboosting technology is developed with combined usage of:

• a) hydrodynamic power high energy ratio of cyclically propelled operative liquid flow driving a vane-fairing disc rotor in a closed loop tunnel, and
• b) said rotor's inertial energy, which is produced constantly supported, and conservated in united rotating structure with newly developed inertial time-radius connected parameters of said rotor.

Some conventional now and new solutions of similar devices like turborotors, blade-apparates, fluid pressure combined motors are presented in classes 29,60,415 of the USA Patent Classification. Any of them don't combine selfboosting hydrodynamic and inertial energy of the united rotor in integrating manner with high power ratio.

Other prior arts directly related to my present proposal, based on cyclically selfboosting flow of operative liquid driving a vane fairing disk rotor for obtaining integrated hydrodynamic and inertial energy in united self-amplifying structure were not found.

BRIEF SUMMARY OF THE INVENTION

The objects of this proposal development are:

• an effective universal non-fuel power-set based on energy integrating selfboosting technology with hydrodynamic-inertial vane rotors, and
• ecologically clean, natural method without any pollution and other harm effects, and possibilities of various power and design applications.

The nature and substance of the Combined Hydrodynamic-Inertial Rotoset-Selfbooster is a vane-fairing disk rotor installed inside a circular closed loop tunnel filled with operative liquid driven by a rotary pump and driving said rotor when smoothly passing over rotor's vanes.

Said rotor is a hydrodynamic flywheel with inertia energy been provided by newly developed method of effective rotating mass selfboosting.

Said tunnel has a module with a rotary pump, which propels said operative liquid inside said tunnel driving fairing vanes of said rotor.

Said pump works in series with itself propelling said liquid for itself and for said rotor, rising the liquid pressure cyclically up to definite level.

Said rotor develops its total torque as a sum of a hydrodynamic and inertial portions produced by kinetic energy of high potential liquid flow and inertial selfboosting simultaneously.

The initial rotation of said rotor is provided by a starter; the rotoset includes an electric battery with a charger.

The rotoset is driven by operative liquid selfboosting flow and by selfboosting mass-inertia momentum integrating both and providing united output power for multiple and different receivers by design.

The natural energy losses are small because of vane-fairing rotor and improved inertia time-radius parameters in combined design. The average total power ratio is about 7.5 depending on output task.

DRAWING FIGURES

The drawings are schematic, and simplified for better clarity of solutions developed. The well known regular elements of mechanical and electrical infrastructures like details of transmissions, relays, switches, etc are not shown as obvious. Numbers of views and sections correspond to the numbers of figures where they are shown.

FIG. 1 illustrates a front view of a Combined Hydrodynamic-Inertial Rotoset-Selfbooster as a voltage generator.

FIG. 2 is a plan view taken in FIG. 1

FIG. 3 is a vertical cross section view taken in FIG. 1.

FIG. 4 shows a scanned electrical scheme of the rotoset represented at FIGS. 1, 2, 3.

FIG. 5 is a partial section taken in FIG. 1 and turned to horizontal.

FIGS. 6A, 6B, 6C, 6D show various equal embodiments of rotors' fairing vanes depending on design requirements. Said vanes performances correspond the section 6-6 taken in FIG. 3.

REFERENCE NUMERALS AND SYMBOLS IN DRAWINGS

Numerals: 20—hydrodynamic-inertial vane-fairing disk rotor, 21—V-vane, 22—W-vane, 23—compound vane, 24—O-vane, 25—vane plate 26—rotor rim, 27—rotor disk, 28—rotor shaft, 29—rotor bearing, 30—closed loop tunnel, 31—tunnel outer rim, 32—tunnel wall, 33—tunnel inner rim, 34—static packing, 35—dynamic packing, 36—dynamic packing ring, 37—operative liquid manometer, 38—packing insert, 39—springed piston valve, 40—starter motor, 41—starter drive, 42—starter clutch, 43—output clutch, 44—output drive, 45—output electric generator 50—pump module, 51—rotary pump impeller, 52—pump motor, 53—pump drive, 54—meter panel, 55—frame element, 56—damper, 57—operative liquid, 58—pump bearing 60—fan cooler, 61—fan electric motor, 62—cooling fin 70—storage battery, 71—electric charger, 72—electric rectifier 73—electric transformer, 74—general control panel

Symbols: operative liquid flow, —rotor rotation, wiring, —vane gaps, voltage outputs

Numerals 29,34,35,40,41,42,43,44,45,51,52,53,54,55,56,60,61,62, 70,71,72,73,74 are conventional units and structures used in present new method of combined hydrodynamic-inertial selfboosting power generation

DETAILED DESCRIPTION OF THE INVENTION

The Combined Hydrodynamic-Inertial Rotoset-Selfbooster in a monotunnel and monorotor design, illustrated in FIG. 1 includes:

• a hydrodynamic-inertial vane-fairing rotor 20,
• a round closed loop tubular tunnel 30,
• a pump module 50 with a rotary pump impeller 51, pump drive 53,
• a springed piston valve 39 for cavitation limitation, meters 54,37
• an output power electric generator 45 with output drive 44,
• a fan cooler 60, cooling fins 62,
• an electromechanical infrastructure.

Said tunnel 30 and module 50 are assembled together as shown and filled with operative liquid 57, which is propelled by rotary pump impeller FIG. 1 also shows rotor's 20 vanes 21, rim 26, disk 27, packing insert 38, Static packing 34, electric motors 40,52,61, tunnel's 30 wall 32, outer rim Pump bearing 58, frame elements 55, dampers 56.

FIG. 2, in addition to FIG. 1, shows the starter's units 40, 41, 42; electric units 70, 71, 72, 73; clutches 42, 43.

FIG. 3, in addition to FIGS. 1, 2, illustrates the mutual arrangement of said rotor 20 and tunnel 30. Are shown: rotor's: vanes 21, 22 with theirs plates 25, rim 26, disk 27, shaft 28, bearings 29; tunnel's outer and inner rims 31, 33, walls 32, static and dynamic packings 34, 35, dynamic packing rings 36, radial gap g, operative liquid 57.

FIG. 4 shows an exemplary wiring scheme of the mono-rotoset shown in FIGS. 1, 2, 3. The electric units 40,45,52,61,70,71,72,73 are shown. The power of the generator 45 can be used directly with voltage V and/or by voltage V after a transformer 73.

FIG. 5 illustrates the connection of said tunnel 30 and module 50. Are shown: tunnel's walls 32, outer and inner rims 31,33, dynamic and static packings 35,34, packing insert 38, rings 36; rotor's vane 21, vane plates 25, rim 26, disk 27; operative liquid 57.

FIGS. 6A, 6B, 6C, 6D show the equal various embodiments of fairing vanes connected to the rotor's rim 26. Are shown different vanes 21,22,23,24, vane plates 25, tunnel walls 32, side gaps g directions of rotor 20 rotation and liquid 57 flow.

Operation

Initial technological steps:

• the starter units 40,41,42 slowly drive the rotor 20;
• the rotary pump impeller 51 propels the operative liquid 57 up to definite liquid velocity and dynamic pressure level, accelerating said rotor 20 up to designed angular velocity; starter units stop.
• the rotor 20 develops integrating momentum from hydrodynamic forces of said vanes 21, and/or 22,23,24, and inertial force effects of all rotating masses simultaneously.

Any kind of said vanes, getting dynamic pressure of liquid flow 57, simultaneously let a part of said flow 57 pass over and by said vanes into the gaps g and g thus providing the flow 57 kinetic energy rising for high hydrodynamic energy ratio.

The total united torque T of the rotor's 20 shaft 28 consists of hydrodynamic portion T and inertial portion T Said torque T is transmitted to electric generator 45 by clutch 43, drive 44 for obtaining output voltage V, charging battery 70 by elements 72,71, and feeding electric motors 52,61. A transformer 73 provides different output voltage V

The springed piston valve 39 provides needed liquid flow static pressure in order to limit and/or prevent the possible vortices, cavitation, and fluctuations inside said tunnel 30 and module 50.

The static and dynamic packings 34,35, and packing insert 38 provide needed hydraulic conditions; the meters 37,54 provide data for the control panel 74.

In addition and/or equally instead of said generator 45, other receivers of rotor's 20 torque can be used including mechanical, hydraulic, and/or combined.

The interactions of said Rotoset-Selfbooster are based on combined integrating work of two united structures:

• a) the rotary pump impeller 51, which operates in actual series with itself, propelling the liquid 57 cyclically at itself, for itself, and drives said rotor 20 rising the liquid dynamic pressure inside tunnel 30 up to definite level;
• b) rotor's 20 inertial momentum with newly developed time-radius interdependence generates and supports the inertial portion of common torque for integrated high power ratio.

Said above newly developed inertial rotor parameters are expressed by equation: R=F·P, where: R—is rotor's radius, P—is rotor's period of rotation, F—is a function of rotor mass and dimensions proportions.

The total integrated combined rotor's torque T is a sum;

T= T+ T, where

• Hydrodynamic torque portion T=P·S Z R, where P is the liquid integrated dynamic pressure, S, Z, R, are the vanes cross area, number, mean radius, and hydrodynamic efficiency respectively;
• Inertial torque portion T=M R W, where M, W, are rotor's mass, angular velocity, and inertial efficiency respectively.

The total power ratio of the Combined Hydrodynamic-Inertial Rotoset-Selfbooster as a non-fuel source of energy is about 7.5, depending on design and KW required.

Claims

1. A Combined Hydrodynamic-Inertial Rotoset-Selfbooster comprises at least by one structure of:

a vane-fairing disk-inertial rotor placed into a circular closed loop tubular tunnel, and

a storage battery with a charger, and

output power devices including, for example, an electric generator transformers, meters, control.

2. The Rotoset-Selfbooster of claim 1 wherein said tunnel has a hydraulic module with a rotary pump inside said module.

3. The Rotoset-Selfbooster of claims 1 and 2 wherein said tunnel with said module are filled with operative liquid which is propelled by said pump in order to drive said rotor.

4. The Rotoset-Selfbooster of claim 1 wherein said rotor includes radial fairing vanes, which can equally be V-vane, and/or W-vane, and/or O-vane, and/or compound and combined for any rotor.

5. The Rotoset-Selfbooster of claims 1,2,3,4 wherein said rotary pump propels said operative liquid inside said tunnel and module, working in actual series with itself, for itself in order to rise cyclically the circular liquid flow dynamic pressure and drive said vane rotor in high potential operative liquid flow in energy-integrating and thus hydrodynamically selfboosting manner.

6. The Rotoset of claim 1 wherein said tubular tunnel includes:

a springed piston valve for operative liquid cavitation limitation and prevention by liquid static pressure adjusting, and

a gasketing insert in order to provide appropriate hydraulic connection with said module, and

dynamic and static packings, and

a fan cooler device

7. The Rotoset of claim 1 wherein the parameters of said vane-fairing rotor, in order to provide the utmost inertial portion of common selfboosting, are corresponding to the equation R=F P,

where: R—is rotor's radius, P—is rotor's period of rotation, F—is a function depending on rotor's elements masses and dimensions proportions.

8. The Rotoset of claim 1 wherein said vane-fairing rotor is installed in said tunnel with radial and side gaps in order to provide a smooth operative liquid flow with vortex limitation, thus contributing to both hydrodynamic and inertial portions of total rotor-selfboosting and to the common united rotor's torque.