CA2228864A1 - Modulated diameter mass slider propulser - Google Patents
Modulated diameter mass slider propulser Download PDFInfo
- Publication number
- CA2228864A1 CA2228864A1 CA 2228864 CA2228864A CA2228864A1 CA 2228864 A1 CA2228864 A1 CA 2228864A1 CA 2228864 CA2228864 CA 2228864 CA 2228864 A CA2228864 A CA 2228864A CA 2228864 A1 CA2228864 A1 CA 2228864A1
- Authority
- CA
- Canada
- Prior art keywords
- rotor
- shaft assembly
- propulser
- mass
- movement
- 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
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
- F03G3/00—Other motors, e.g. gravity or inertia motors
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Harvester Elements (AREA)
Abstract
The present invention incorporates special ROTOR-SHAFT-ASSEMBLIES mounted in suitable bearings, affixed at appropriate places with articulated MASS-BODY-COMPONENTS - - installed in evenspaced arrangement and capable of sliding inwardly and outwardly in perpendicular-to-axis-of-rotorshaft-assembly-movement in response to special SIGNAL-STROKE-MOVEMENT-AMPLIFICATION-MEANS, which are activated by having special CONTOUR-CONTACT-TRACKING-WHEELS, suitably affixed in bearings, track special STATIONARY-PROGRAM-CONTROL-CONTOUR-SLEEVE-COMPONENTS
surrounding in NON-CONTACT-WITH-ROTOR-SHAFT-ASSEMBLIES fashion aforesaid ROTOR-SHAFT-ASSEMBLIES, whereas aforesaid PROGRAM-CONTROL-CONTOUR-SLEEVE-COMPONENTS
are rigidly, securely and suitably fastened to an appropriate MACHINE BASE
BOX STRUCTURE, whereinwhich ROTORSHAFT BEARING SUPPORTS likewise are securely and rigidly fastened to said machine base box structure, thusly making possible to have articulated rotor MASS BODY COMPONENT segments, suitably contained in radially installed SLIDE-CAGE-CONTAINERS, change the effective DIAMETER
respectively RADIUS of ROTARY MASS MOVEMENT in preprogrammed intended function through an arc of rotation of somewhat LESS than 180 0; thusly converting the INPUT
ENERGY
of suitable PRIME MOVER attached to ROTOR-SHAFT-ASSEMBLY, INTO a certain UNIDIRECTIONAL FORCE such as LIFT.
surrounding in NON-CONTACT-WITH-ROTOR-SHAFT-ASSEMBLIES fashion aforesaid ROTOR-SHAFT-ASSEMBLIES, whereas aforesaid PROGRAM-CONTROL-CONTOUR-SLEEVE-COMPONENTS
are rigidly, securely and suitably fastened to an appropriate MACHINE BASE
BOX STRUCTURE, whereinwhich ROTORSHAFT BEARING SUPPORTS likewise are securely and rigidly fastened to said machine base box structure, thusly making possible to have articulated rotor MASS BODY COMPONENT segments, suitably contained in radially installed SLIDE-CAGE-CONTAINERS, change the effective DIAMETER
respectively RADIUS of ROTARY MASS MOVEMENT in preprogrammed intended function through an arc of rotation of somewhat LESS than 180 0; thusly converting the INPUT
ENERGY
of suitable PRIME MOVER attached to ROTOR-SHAFT-ASSEMBLY, INTO a certain UNIDIRECTIONAL FORCE such as LIFT.
Description
SPECIFICATION:
There are a total of 10 drawings pertaining to the specification numbered from Figure 1 to Figure 10.
In figure number 1. is shown that the present invention consists of a special overall Shaft and Rotor Assembly 1 made of a suitable assembly of shaft segments equipped with prime driver Coupling 2 at respective ends, special option bearing equipped support Rail Wheels 3 supporting the overall Shaft and Rotor assembly by being attached appropriately to support structure 10 and having 1 ride on 3 by means of circular track component 13 appropriately attached to main shaft body assembly 23, thusly making possible an extra large Diameter configuration of Shaft and Rotor assembly and allowing minimal wear Shaft main bearing means.
Also shown in Figure 1 are direction of propulsive force indicator arrow 12 as wE~ll as direction of rotation indicator arrows 11. Overall Shaft and Rotor assemb-ly 23 is supported by Bearing Housing Support Structure 10, which is firmly aiaached to Machine Base Box Structure 9. Also shown are Mass Body Slider comp-orients 4, whose outward- respectively inward sliding movements are in perpendicul-ar-to-shaft-axis-orientation enabled thusly by being contained within radiatively installed Slider-Cage-Sheath-Container-Frame-Boxes 5 equipped with suitable bear-ing wheels 14. 15 are reinforcing gussets for 5. 8 are suitable high tensile strength steel or other suitable material cables securely attached to 4 and capab-l~e of pulling Mass Body Slider components 4 back to a certain Inner Diameter of Rotor position from an Outer Diameter of Rotor Mass position being thusly activat-ed by Amplified Motion Stroke Impulse Signals emanating from suitable motion-stroke-Amplifiercomponent Modules 30. 6 is a suitable Shroudcase-Coverstructure encasing the overall Rotor Shaft Assembly in order to prevent air turbulance drag when Rotor Shaft Assembly is being rotated up to operational and further high output revolution-per-minute speed. 38 are suitable shock absorber components suitably installed here in order to dampen the inherent shocks, when Centrifugal Force slams Mass Body Slider components 4 outward against the end cap segment of 5.
In Figure 2 are shown again Machine Base Box Structure 9. To it are attached Rotor Shaft Assembly support legs 10 supporting Rotor Shaft Assembly bearing support housing 22 containing main Rotor Shaft Assembly Roller Bearing component 21. 6 again denotes Shroudcase-Coverstructure. 11 are direction of revolution indicator arrows. 2 is Prime Mover mating coupling segment of 23. 15 are reinforcing gusset components for 5, 16 is a perpendicularly-to-Rotor-Shaft-Assembly-Axis -installed Control-Program-Contour-Track-Ring component, which serves to create activation stroke impulse signals in preprogrammed reference frame, such component 16 securely and rigidly affixed to 9 at an appropriate location by support leg structure 24. 19 are suitable Program Contour Tracking Wheels affixed within suitable bearing supports 20. 18 are female slider portsheaths for component-20-sliding-supportstem 17.
In Figure 3 one sees , here only outlined and indicating relative position reinforcing gussets 15. 6 denotes again Shroudcase-Coverstructure, encasing Rcrtor Shaft Assembly 23. 16 is Program Control Contour Track Ring component wherein segment 26 of 16 on the left side shows the Contraction-Induction segment of 16 and 25 on the other side denotes the Expansion-Induction segment of 16. 18 here are appropriate components so installed and in such a way as to anticipate Change of Control Contour and ascertain and make possible a lesser shock exposure of component group 19-17-18.
There are a total of 10 drawings pertaining to the specification numbered from Figure 1 to Figure 10.
In figure number 1. is shown that the present invention consists of a special overall Shaft and Rotor Assembly 1 made of a suitable assembly of shaft segments equipped with prime driver Coupling 2 at respective ends, special option bearing equipped support Rail Wheels 3 supporting the overall Shaft and Rotor assembly by being attached appropriately to support structure 10 and having 1 ride on 3 by means of circular track component 13 appropriately attached to main shaft body assembly 23, thusly making possible an extra large Diameter configuration of Shaft and Rotor assembly and allowing minimal wear Shaft main bearing means.
Also shown in Figure 1 are direction of propulsive force indicator arrow 12 as wE~ll as direction of rotation indicator arrows 11. Overall Shaft and Rotor assemb-ly 23 is supported by Bearing Housing Support Structure 10, which is firmly aiaached to Machine Base Box Structure 9. Also shown are Mass Body Slider comp-orients 4, whose outward- respectively inward sliding movements are in perpendicul-ar-to-shaft-axis-orientation enabled thusly by being contained within radiatively installed Slider-Cage-Sheath-Container-Frame-Boxes 5 equipped with suitable bear-ing wheels 14. 15 are reinforcing gussets for 5. 8 are suitable high tensile strength steel or other suitable material cables securely attached to 4 and capab-l~e of pulling Mass Body Slider components 4 back to a certain Inner Diameter of Rotor position from an Outer Diameter of Rotor Mass position being thusly activat-ed by Amplified Motion Stroke Impulse Signals emanating from suitable motion-stroke-Amplifiercomponent Modules 30. 6 is a suitable Shroudcase-Coverstructure encasing the overall Rotor Shaft Assembly in order to prevent air turbulance drag when Rotor Shaft Assembly is being rotated up to operational and further high output revolution-per-minute speed. 38 are suitable shock absorber components suitably installed here in order to dampen the inherent shocks, when Centrifugal Force slams Mass Body Slider components 4 outward against the end cap segment of 5.
In Figure 2 are shown again Machine Base Box Structure 9. To it are attached Rotor Shaft Assembly support legs 10 supporting Rotor Shaft Assembly bearing support housing 22 containing main Rotor Shaft Assembly Roller Bearing component 21. 6 again denotes Shroudcase-Coverstructure. 11 are direction of revolution indicator arrows. 2 is Prime Mover mating coupling segment of 23. 15 are reinforcing gusset components for 5, 16 is a perpendicularly-to-Rotor-Shaft-Assembly-Axis -installed Control-Program-Contour-Track-Ring component, which serves to create activation stroke impulse signals in preprogrammed reference frame, such component 16 securely and rigidly affixed to 9 at an appropriate location by support leg structure 24. 19 are suitable Program Contour Tracking Wheels affixed within suitable bearing supports 20. 18 are female slider portsheaths for component-20-sliding-supportstem 17.
In Figure 3 one sees , here only outlined and indicating relative position reinforcing gussets 15. 6 denotes again Shroudcase-Coverstructure, encasing Rcrtor Shaft Assembly 23. 16 is Program Control Contour Track Ring component wherein segment 26 of 16 on the left side shows the Contraction-Induction segment of 16 and 25 on the other side denotes the Expansion-Induction segment of 16. 18 here are appropriate components so installed and in such a way as to anticipate Change of Control Contour and ascertain and make possible a lesser shock exposure of component group 19-17-18.
In Figure 4 shown are in Close-up Bottom view a typical Mass Body Slider compon-ent unit 4 having an appropriate number of suitable steel cables or made of other suitable material cables 8 attached to it and held in place securely by cable eye lock pin 27 wherein 8 serves to retract 4 inwardly when appropriate and at an appropriate rate of speed and suitable retraction cycle; further also is shown in partially fragmentary view Slide-Sheath-Cage-Container-Frame Box 5 equipped with reinforcing gussets 15 together with bearing equipped slide action enhancing wheels 14.
In Figure 5 is shown a partly schematic side view of overall Rotor Shaft Assembly 23 arrangement revolved WITHLN Activation Program Control Contour Ring component ( perpendicular to shaftaxis orientation version ) 16, wherein can be seen the Mass Body Slider components 4 contained suitably within Slide-Sheath-Cage-Con-tainer-Frame Boxes 5 suitably mounted and securely attached to 23. Also denoted in drawing Figure 5 are shown Angle-of-Pull-Change anchor sheaves 31. 33 are bearing equipped hinge-anchor pins for 31. 24 are support structures for 16.
Rotor Shaft Assembly 23 here also is shown with suitably placed Motion Stroke Amplifier modules 30. Also in drawing Figure 5 one finds elements and components previously described and identified in preceding drawings.
In Figure 6 is shown basically the same partly schematic side view of Rotor Shaft Assembly as shown in Figure 5 with the added optional feature of an appropriate activation signal transfer Chain being used here instead of cables 8. Also shown is spring-loaded compression pack 29 and here Rotor Shaft Assembly 23 is shown being revolved within and being surrounded by in this case a horizontally disposed Activation-Program-Control-Program-Contour-Track-Ring-component 16/
version, wherein 16/28 sends initial control program stroke signals in a horiz-ontal plane movement that is to say parallell with Rotor Shaft Axis orientation, arnd longitudinally therewith.
Figure 7 shows a flat and un-wrapped so to speak partial portion projection bottom view of a staggered arrangement of Mass Body Slider components within their Slider-Cage-Sheath-Container-Frame-Boxes, wherein this arrangement makes possible a more effective Rotor performance. Also shown is the alternate version of 4 themselves being optionally equipped with their own suitable roll-and-slide-enabling means 37.
Figure 8 shows Motion Stroke Amplification Module 30 with an alternate arrange-ment of amplification action lever-linkage embers 43 with suitable pivotable ( articulated ) pivot joints 56; 41 is a direction-of-signal-stroke indication arrow. 29 are compression spring-pack-return components. 49 are brackets supporting appropriately certain cable transmission-sheave-components.
46-8-45- group component shows an added and alternate motion stroke amplification means; whereinwhich 46 is in stationary installation attached to support frame 44; 45 an articulated sheave part attached to 43.
Figure 9 represents a partial side view of Rotor Shaft Assembly group 23 affixed with shaft reinforcing gussets 47 whereinwhich 48 is a suitable ring gear power transmission component affixed to 23. 58 is Outward direction of movement indicator arrow of 4. 59 is Inward direction of movement indicator arrow of 4. 8 is retraction activation cable, guided through positioning anchor sheave 31 and motion stroke amplifier group 46-8-45 component. 49 are support brackets. 16 is Program Control Contour track ring ( perpendicular version ) here mounted to 9 between shroudcase cover structure 6 and Rotor Shaft Main Support End Bearing support component 22-10. 29 are compression spring- Repositioning packs. 30 are Motion Stroke Amplifier Modules contained within shroudcase coverstructure 6. 38 are suitable shock absorber components.
Figure 10 shows a somewhat differently constructed amplifier module 30 wherein the motion stroke amplification function is obtained by appropriately installed sequentially interacting and intermeshing transmission gearwheel group 51.-52-53-54 initially activated by control impulse signal transmitting sliding gear rack component 50.
In Figure 5 is shown a partly schematic side view of overall Rotor Shaft Assembly 23 arrangement revolved WITHLN Activation Program Control Contour Ring component ( perpendicular to shaftaxis orientation version ) 16, wherein can be seen the Mass Body Slider components 4 contained suitably within Slide-Sheath-Cage-Con-tainer-Frame Boxes 5 suitably mounted and securely attached to 23. Also denoted in drawing Figure 5 are shown Angle-of-Pull-Change anchor sheaves 31. 33 are bearing equipped hinge-anchor pins for 31. 24 are support structures for 16.
Rotor Shaft Assembly 23 here also is shown with suitably placed Motion Stroke Amplifier modules 30. Also in drawing Figure 5 one finds elements and components previously described and identified in preceding drawings.
In Figure 6 is shown basically the same partly schematic side view of Rotor Shaft Assembly as shown in Figure 5 with the added optional feature of an appropriate activation signal transfer Chain being used here instead of cables 8. Also shown is spring-loaded compression pack 29 and here Rotor Shaft Assembly 23 is shown being revolved within and being surrounded by in this case a horizontally disposed Activation-Program-Control-Program-Contour-Track-Ring-component 16/
version, wherein 16/28 sends initial control program stroke signals in a horiz-ontal plane movement that is to say parallell with Rotor Shaft Axis orientation, arnd longitudinally therewith.
Figure 7 shows a flat and un-wrapped so to speak partial portion projection bottom view of a staggered arrangement of Mass Body Slider components within their Slider-Cage-Sheath-Container-Frame-Boxes, wherein this arrangement makes possible a more effective Rotor performance. Also shown is the alternate version of 4 themselves being optionally equipped with their own suitable roll-and-slide-enabling means 37.
Figure 8 shows Motion Stroke Amplification Module 30 with an alternate arrange-ment of amplification action lever-linkage embers 43 with suitable pivotable ( articulated ) pivot joints 56; 41 is a direction-of-signal-stroke indication arrow. 29 are compression spring-pack-return components. 49 are brackets supporting appropriately certain cable transmission-sheave-components.
46-8-45- group component shows an added and alternate motion stroke amplification means; whereinwhich 46 is in stationary installation attached to support frame 44; 45 an articulated sheave part attached to 43.
Figure 9 represents a partial side view of Rotor Shaft Assembly group 23 affixed with shaft reinforcing gussets 47 whereinwhich 48 is a suitable ring gear power transmission component affixed to 23. 58 is Outward direction of movement indicator arrow of 4. 59 is Inward direction of movement indicator arrow of 4. 8 is retraction activation cable, guided through positioning anchor sheave 31 and motion stroke amplifier group 46-8-45 component. 49 are support brackets. 16 is Program Control Contour track ring ( perpendicular version ) here mounted to 9 between shroudcase cover structure 6 and Rotor Shaft Main Support End Bearing support component 22-10. 29 are compression spring- Repositioning packs. 30 are Motion Stroke Amplifier Modules contained within shroudcase coverstructure 6. 38 are suitable shock absorber components.
Figure 10 shows a somewhat differently constructed amplifier module 30 wherein the motion stroke amplification function is obtained by appropriately installed sequentially interacting and intermeshing transmission gearwheel group 51.-52-53-54 initially activated by control impulse signal transmitting sliding gear rack component 50.
Claims
CLAIMS:
The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows: An assembly of certain parts and components forming a propulsion apparatus with certain co-functioning elements within a certain programming and timing and specific locations within certain reference frame areas calibrated in their actions in cooperative and conjunctive manner comprised of a MACHINE BASE BOX STRUCTURE affixed to which and firmly attached thereto is a CONTROL PROGRAM CONTOUR TRACK RING Component surrounding and enveloping in NON-TOUCHING fashion a specially fashioned ROTOR AND SHAFT
ASSEMBLY mated to, driven by and rotated by a suitable PRIME MOVER MOTOR of appropriate power output, whereinwhich such special ROTOR AND SHAFT ASSEMBLY
also is suitably mounted to and supported by appropriate support leg structures and furtherwherein aforesaid special rotor and shaft assembly is equipped with special articulated Mass Body Slider components ( weights ) contained in suitable slide means equipped container frame cage boxes affixed to aforesaid ROTOR AND
SHAFT ASSEMBLY in evenspaced arrangement in a manner allowing sliding movement of Mass Body Slider components in radial orientation and perpendicular to axis of ROTOR AND SHAFT ASSEMBLY inwardly and alternatingly outwardly in a manner preprogrammed by suitable activation mechanisms activated by appropriate impulse transmitter tracking wheels affixed with bearings of suitable composition and suitably attached to ROTOR AND SHAFT ASSEMBLY, tracking and following aforesaid control program contour track ring along it's appropriate control contour, whereby separate activation mechanisms equipped with MOTION STROKE
AMPLIFICATION
MEANS, pass on individual ACTIVATION PROGRAM CONTROL CONTOUR TRACK RING
triggered motive signal impulses after being stroke length amplified towards correspondingly appropriate articulated MASS BODY SLIDER COMPONENTS and cause RETRACTION INWARDLY of aforementioned MASS BODY SLIDER COMPONENTS toward the ROTOR AND SHAFT ASSEMBLY axis within the effect-intended reference frame arc of rotation segment, OVERCOMING the CENTRIFUGAL FORCE forcing MASS BODY
SLIDER COMPONENTS outwardly FROM ROTOR and SHAFT ASSEMBLY axis whereinwhich the desired lift and propulsive force in this machine is created by having THUSLY
an effective ROTOR MASS DIAMETER LARGER within a certain, somewhat LESS than 180 o Arc Segment of rotary movement than the remainder of rotary movement wiithin a certain ROTARY MOVEMENT OF MASS REFERENCE FRAME creating a CERTAIN
CONSTANT IMBALANCE manifest within specific and intended PREPROGRAMMING of mechanical ACTION that way creating and producing a PROPULSIVE FORCE OF
UNIDIRECTIONAL NATURE, in turn being transfused to the propulser apparatus and propulser group respectively propulser cluster suitably installed within a suitable Transport vehicle capable of HELICOPTER-LIKE CAPABILITIES, whereinwhich in a CLOCKWISE
REVOLVED PROPULSER UNIT the LARGER DIAMETER activated ROTOR SEGMENT is held within an ARC OF ROTOR MOVEMENT extending FROM the 12 o'clock POSITION THROUGH
the 3 o'clock POSITION TO the 6 o'clock POSITION of ROTATION OF MASS AND
whereinwhich in a COUNTERCLOCKWISE REVOLVED PROPULSER UNIT the LARGER DIAMETER
activated ROTOR SEGMENT is held within an arc of ROTOR MOVEMENT FROM the 12 o'clock POSITION THROUGH the 9 o'clock POSITION to the 6 o'clock POSITION of ROTATION OF MASS in this PROPULSER UNIT and furtherwherein a proper PROPULSER UNIT in COMPLETE ASSEMBLY consists of two ROTOR AND SHAFT ASSEMBLY
UNITS, wherein the ONE is ROTATED IN AN OPPOSITE DIRECTION to the OTHER in order to COUNTERACT counterproductive torque moments.
The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows: An assembly of certain parts and components forming a propulsion apparatus with certain co-functioning elements within a certain programming and timing and specific locations within certain reference frame areas calibrated in their actions in cooperative and conjunctive manner comprised of a MACHINE BASE BOX STRUCTURE affixed to which and firmly attached thereto is a CONTROL PROGRAM CONTOUR TRACK RING Component surrounding and enveloping in NON-TOUCHING fashion a specially fashioned ROTOR AND SHAFT
ASSEMBLY mated to, driven by and rotated by a suitable PRIME MOVER MOTOR of appropriate power output, whereinwhich such special ROTOR AND SHAFT ASSEMBLY
also is suitably mounted to and supported by appropriate support leg structures and furtherwherein aforesaid special rotor and shaft assembly is equipped with special articulated Mass Body Slider components ( weights ) contained in suitable slide means equipped container frame cage boxes affixed to aforesaid ROTOR AND
SHAFT ASSEMBLY in evenspaced arrangement in a manner allowing sliding movement of Mass Body Slider components in radial orientation and perpendicular to axis of ROTOR AND SHAFT ASSEMBLY inwardly and alternatingly outwardly in a manner preprogrammed by suitable activation mechanisms activated by appropriate impulse transmitter tracking wheels affixed with bearings of suitable composition and suitably attached to ROTOR AND SHAFT ASSEMBLY, tracking and following aforesaid control program contour track ring along it's appropriate control contour, whereby separate activation mechanisms equipped with MOTION STROKE
AMPLIFICATION
MEANS, pass on individual ACTIVATION PROGRAM CONTROL CONTOUR TRACK RING
triggered motive signal impulses after being stroke length amplified towards correspondingly appropriate articulated MASS BODY SLIDER COMPONENTS and cause RETRACTION INWARDLY of aforementioned MASS BODY SLIDER COMPONENTS toward the ROTOR AND SHAFT ASSEMBLY axis within the effect-intended reference frame arc of rotation segment, OVERCOMING the CENTRIFUGAL FORCE forcing MASS BODY
SLIDER COMPONENTS outwardly FROM ROTOR and SHAFT ASSEMBLY axis whereinwhich the desired lift and propulsive force in this machine is created by having THUSLY
an effective ROTOR MASS DIAMETER LARGER within a certain, somewhat LESS than 180 o Arc Segment of rotary movement than the remainder of rotary movement wiithin a certain ROTARY MOVEMENT OF MASS REFERENCE FRAME creating a CERTAIN
CONSTANT IMBALANCE manifest within specific and intended PREPROGRAMMING of mechanical ACTION that way creating and producing a PROPULSIVE FORCE OF
UNIDIRECTIONAL NATURE, in turn being transfused to the propulser apparatus and propulser group respectively propulser cluster suitably installed within a suitable Transport vehicle capable of HELICOPTER-LIKE CAPABILITIES, whereinwhich in a CLOCKWISE
REVOLVED PROPULSER UNIT the LARGER DIAMETER activated ROTOR SEGMENT is held within an ARC OF ROTOR MOVEMENT extending FROM the 12 o'clock POSITION THROUGH
the 3 o'clock POSITION TO the 6 o'clock POSITION of ROTATION OF MASS AND
whereinwhich in a COUNTERCLOCKWISE REVOLVED PROPULSER UNIT the LARGER DIAMETER
activated ROTOR SEGMENT is held within an arc of ROTOR MOVEMENT FROM the 12 o'clock POSITION THROUGH the 9 o'clock POSITION to the 6 o'clock POSITION of ROTATION OF MASS in this PROPULSER UNIT and furtherwherein a proper PROPULSER UNIT in COMPLETE ASSEMBLY consists of two ROTOR AND SHAFT ASSEMBLY
UNITS, wherein the ONE is ROTATED IN AN OPPOSITE DIRECTION to the OTHER in order to COUNTERACT counterproductive torque moments.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA 2228864 CA2228864A1 (en) | 1998-04-20 | 1998-04-20 | Modulated diameter mass slider propulser |
| PCT/US1999/008644 WO1999057462A1 (en) | 1998-04-20 | 1999-04-20 | Modulated diameter mass slider propulser |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA 2228864 CA2228864A1 (en) | 1998-04-20 | 1998-04-20 | Modulated diameter mass slider propulser |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2228864A1 true CA2228864A1 (en) | 1999-10-20 |
Family
ID=4162082
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA 2228864 Abandoned CA2228864A1 (en) | 1998-04-20 | 1998-04-20 | Modulated diameter mass slider propulser |
Country Status (2)
| Country | Link |
|---|---|
| CA (1) | CA2228864A1 (en) |
| WO (1) | WO1999057462A1 (en) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2422644B (en) * | 2005-01-26 | 2009-04-29 | Alan William Hart | Dynamic drive engine |
| ES2311319B1 (en) * | 2005-10-26 | 2009-11-10 | Juan Morales Contreras | KINETIC ENERGY AMPLIFIER. |
| WO2016151406A2 (en) * | 2015-03-24 | 2016-09-29 | Avci Selim | Drive assembly |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR933483A (en) * | 1946-08-31 | 1948-04-22 | Method and device for obtaining a force | |
| US3968700A (en) * | 1974-08-01 | 1976-07-13 | Cuff Calvin I | Device for converting rotary motion into a unidirectional linear motion |
| FR2288882A1 (en) * | 1974-10-22 | 1976-05-21 | Coutant Jean Pierre | Rotary machine driven by potential energy - has weights driven around circular guide placed eccentrically of horiz. shaft |
-
1998
- 1998-04-20 CA CA 2228864 patent/CA2228864A1/en not_active Abandoned
-
1999
- 1999-04-20 WO PCT/US1999/008644 patent/WO1999057462A1/en active Application Filing
Also Published As
| Publication number | Publication date |
|---|---|
| WO1999057462A1 (en) | 1999-11-11 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP4050441B2 (en) | Wind power generator | |
| CN102906460A (en) | Hydrodynamic coupling device, in particular a torque converter | |
| KR20140040145A (en) | Wheel suspension with rotation damper | |
| CN103108764A (en) | A wheel with an electrical unit | |
| CN2816401Y (en) | Road energy-storage power supplying apparatus | |
| CN102022496A (en) | Accessory drive tensioner assembly | |
| CN110315520B (en) | Energy controllable redundant elastic driver based on metamorphic mechanism | |
| JP2013540959A (en) | Kinetic energy storage method and rotor device for kinetic energy storage and dissipation | |
| KR20190126700A (en) | Vibration Mechanism, Machine and Implementation Method with Simultaneous Cross Centrifugation | |
| CN106062413B (en) | With the electromechanical rotary shock absorber for drawing stop part and pressure stop part | |
| CA2228864A1 (en) | Modulated diameter mass slider propulser | |
| CN113404838A (en) | Harmonic speed reducer for barrier gate and barrier gate device | |
| CN109844345A (en) | Centrifugal clutch | |
| CN105987160A (en) | Device for damping vibration of transmission | |
| CN206682207U (en) | The mechanical damper of nuclear power | |
| WO2002063185A1 (en) | Bi-directional to unidirectional torque conversion method and apparatus | |
| US20110041630A1 (en) | Propulsion mechanism employing conversion of rotary motion into a unidirectional linear force | |
| US20080060460A1 (en) | Propulsion device employing conversion of rotary motion into a unidirectional linear force | |
| JP2012116251A (en) | Camber angle adjusting device | |
| CN107725665B (en) | A kind of damping stored energy mechanism adjusted based on telescopic device | |
| JP2021519424A (en) | Improved mechanism for rotating devices | |
| CN203339868U (en) | Oriented working acceleration flywheel | |
| CN104973153A (en) | Novel suspension system for tracked mobile robot | |
| CN216994604U (en) | Self-adaptive deformable robot moving platform | |
| US20110290047A1 (en) | Oscillating Device For Generating Seismic Loads And Compacting Soil |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| FZDE | Dead |