CA2610998A1 - Electro pressure differential flying device - Google Patents
Electro pressure differential flying device Download PDFInfo
- Publication number
- CA2610998A1 CA2610998A1 CA002610998A CA2610998A CA2610998A1 CA 2610998 A1 CA2610998 A1 CA 2610998A1 CA 002610998 A CA002610998 A CA 002610998A CA 2610998 A CA2610998 A CA 2610998A CA 2610998 A1 CA2610998 A1 CA 2610998A1
- Authority
- CA
- Canada
- Prior art keywords
- gaseous
- surface plate
- positively charged
- fluid material
- fluid
- 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
- 239000012530 fluid Substances 0.000 claims abstract description 25
- 239000000463 material Substances 0.000 claims abstract description 20
- 150000002500 ions Chemical class 0.000 claims abstract description 12
- 239000004020 conductor Substances 0.000 claims abstract description 6
- 230000005672 electromagnetic field Effects 0.000 claims abstract description 6
- 230000005611 electricity Effects 0.000 abstract description 3
- 230000007935 neutral effect Effects 0.000 abstract 1
- 239000012811 non-conductive material Substances 0.000 description 5
- 150000001875 compounds Chemical class 0.000 description 4
- 230000008901 benefit Effects 0.000 description 3
- 239000002801 charged material Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005686 electrostatic field Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/001—Flying saucers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H99/00—Subject matter not provided for in other groups of this subclass
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
Abstract
The invention (device) produces directional force propelling itself with no mechanical moving parts in a gaseous or fluid material such as Earth's atmosphere by employing multiple principles found in the theories of Electricity, Electromagnetism, Electrostatics and Fluid dynamics. The invention is comprised of two partial hollow spheres spliced together at a small radial cross-section with one forming the top surface plate of the device and the other forming the bottom surface plate. The top and bottom surface plates are made of highly electrical conductive materials which are charged in opposite electric potentials by an internal high voltage DC power system. The positively charged surface plate ionizes the gaseous or fluid material on the device's external surface stripping away the negatively charged electrons leaving heavy positive ions.
The positively charged surface plate repels the positively charged ions creating a low pressure cavity over the positively charged surface plate. A current induced, internal wire solenoid, traveling around the perimeter of the device, generates an electromagnetic field which is used to capture the gaseous or fluid positive ions on the exterior of the device over the positively charged surface plate and direct them to the opposite, negatively charged, side of the device. This action produces a fluid flow of positive ions and neutral gaseous or fluid material around the device further lowering the pressure on the positively charged side of the device. The pressure differential produced between the lower pressure positive side of the device and the nominal pressure on the negative side of the device produces a directional force in the direction of the positively charged side of the device.
The positively charged surface plate repels the positively charged ions creating a low pressure cavity over the positively charged surface plate. A current induced, internal wire solenoid, traveling around the perimeter of the device, generates an electromagnetic field which is used to capture the gaseous or fluid positive ions on the exterior of the device over the positively charged surface plate and direct them to the opposite, negatively charged, side of the device. This action produces a fluid flow of positive ions and neutral gaseous or fluid material around the device further lowering the pressure on the positively charged side of the device. The pressure differential produced between the lower pressure positive side of the device and the nominal pressure on the negative side of the device produces a directional force in the direction of the positively charged side of the device.
Description
ELECTRO PRESSURE DIFFERENTIAL FLYING DEVICE
The invention (device) produces directional force propelling itself in a gaseous or fluid environment with no mechanical moving parts.
BACKGROUND OF THE INVENTION
There is no such invention of any similarity with a patent known to exist with claims of any similarity.
The invention possesses numerous benefits and advantages over existing flying devices. In particular, since it has no mechanical moving parts, there is no mechanical energy loss. Another benefit is, if the DC power system is a derivative of a nuclear power system, the device can maintain its generated directional force indefinitely or for as long the nuclear power system can produce DC power. This device also has the ability to vertically lift itself off a surface which can be very beneficial depending the application use.
A practical example of the flexibility possessed by the invention resides in its ability to be applied to various flight application uses. Some of these application uses include but are not limited to existing flight uses and functions currently performed by conventional helicopter, blimp and airship systems. A particular flight use is transportation. Another flight use is surveillance.
The invention (device) produces directional force propelling itself in a gaseous or fluid environment with no mechanical moving parts.
BACKGROUND OF THE INVENTION
There is no such invention of any similarity with a patent known to exist with claims of any similarity.
The invention possesses numerous benefits and advantages over existing flying devices. In particular, since it has no mechanical moving parts, there is no mechanical energy loss. Another benefit is, if the DC power system is a derivative of a nuclear power system, the device can maintain its generated directional force indefinitely or for as long the nuclear power system can produce DC power. This device also has the ability to vertically lift itself off a surface which can be very beneficial depending the application use.
A practical example of the flexibility possessed by the invention resides in its ability to be applied to various flight application uses. Some of these application uses include but are not limited to existing flight uses and functions currently performed by conventional helicopter, blimp and airship systems. A particular flight use is transportation. Another flight use is surveillance.
Inventor: Robert Derneb Address: 15 Sagres Crescent, Toronto, Ont., M6N 5E4 Phone:41inlr6-059-1500 Erneil: maameii(~orneil.com Date: 12I02I2007 SUMMARY OF THE INVENTION
The invention (device) produces directional force propelling itself with no mechanical moving parts in a gaseous or fluid material such as Earth's atmosphere by employing multiple principles found in the theories of Electricity, Electromagnetism, Electrostatics and Fluid dynamics. The invention is comprised of two partial hollow spheres spliced together at a small radial cross-section with one forming the top surface plate of the device and other forming the bottom surface plate. The top and bottom surfaces are made of highly electrical conductive material. The two surface plates are separated and internally laced with highly non-conductive material. In the interior of the device, just inside where the two sphere cross-sections meet, is a varying, high voltage, electric, closed-loop, conducting wire-solenoid(s) which travels around the internal perimeter of the device which is used the produce an electromagnetic field with a field direction pointing up on exterior of the device. The device generates an extremely high varying electrostatic positive charge potential ranging from OVDC to in excess of +40000VDC
on the top plate and an equally corresponding negative charge on the bottom plate by means of a built-in high voltage DC power system which can be a battery, gasoline powered electric DC generator, or any other power device utilizing a high voltage transformer placed in the center of the interior of the device between the two surface plates and the non-conductive material. The high voltage DC power system is incased in a container which shields its contents from the electrostatic and electromagnetic fields with a layer of non-conductive material and another of conductive material.
Electric conductive wiring attaches the high voltage DC power system to the top and bottom plates providing the positive and negative charge respectively and provides electric current to the wire-solenoid traveling around the interior diameter of the device.
The high electrostatic positive potential on the top plate separates electrons from the surrounding gaseous material elements or compounds above the device and absorbs it leaving heavy, positively charged material elements or compounds (positive ions). The positively charged top plate and the positively charged ions repel each other creating a low pressure cavity (vacuum) between the top plate and gaseous material. The magnetic field generated by the interior wire-solenoid(s) captures and directs the positive ions to the negatively charge bottom of the device which produces a gaseous material to flow around the device from top to bottom. This gaseous flow further assists the lower the pressure above the device by invoking the principles of the Coanda effect and lift force which are fundamental to standard Fluid dynamics. The pressure differential above the below the device cause the device to move in the direction of the positively charged top plate, which, if the device has its bottom plate facing the ground in Earth's atmosphere, is called lift. In essence, this device floats on air as a boat floats on water.
In the drawings, which form a part of this specification, Fig. 1 is a side and top cross sectional view the invention;
Fig. 2 is an operational view of the mechanisms and fields being used to produce directional force;
The invention (device) produces directional force propelling itself with no mechanical moving parts in a gaseous or fluid material such as Earth's atmosphere by employing multiple principles found in the theories of Electricity, Electromagnetism, Electrostatics and Fluid dynamics. The invention is comprised of two partial hollow spheres spliced together at a small radial cross-section with one forming the top surface plate of the device and other forming the bottom surface plate. The top and bottom surfaces are made of highly electrical conductive material. The two surface plates are separated and internally laced with highly non-conductive material. In the interior of the device, just inside where the two sphere cross-sections meet, is a varying, high voltage, electric, closed-loop, conducting wire-solenoid(s) which travels around the internal perimeter of the device which is used the produce an electromagnetic field with a field direction pointing up on exterior of the device. The device generates an extremely high varying electrostatic positive charge potential ranging from OVDC to in excess of +40000VDC
on the top plate and an equally corresponding negative charge on the bottom plate by means of a built-in high voltage DC power system which can be a battery, gasoline powered electric DC generator, or any other power device utilizing a high voltage transformer placed in the center of the interior of the device between the two surface plates and the non-conductive material. The high voltage DC power system is incased in a container which shields its contents from the electrostatic and electromagnetic fields with a layer of non-conductive material and another of conductive material.
Electric conductive wiring attaches the high voltage DC power system to the top and bottom plates providing the positive and negative charge respectively and provides electric current to the wire-solenoid traveling around the interior diameter of the device.
The high electrostatic positive potential on the top plate separates electrons from the surrounding gaseous material elements or compounds above the device and absorbs it leaving heavy, positively charged material elements or compounds (positive ions). The positively charged top plate and the positively charged ions repel each other creating a low pressure cavity (vacuum) between the top plate and gaseous material. The magnetic field generated by the interior wire-solenoid(s) captures and directs the positive ions to the negatively charge bottom of the device which produces a gaseous material to flow around the device from top to bottom. This gaseous flow further assists the lower the pressure above the device by invoking the principles of the Coanda effect and lift force which are fundamental to standard Fluid dynamics. The pressure differential above the below the device cause the device to move in the direction of the positively charged top plate, which, if the device has its bottom plate facing the ground in Earth's atmosphere, is called lift. In essence, this device floats on air as a boat floats on water.
In the drawings, which form a part of this specification, Fig. 1 is a side and top cross sectional view the invention;
Fig. 2 is an operational view of the mechanisms and fields being used to produce directional force;
Inventor: Robert pemelo Address: 15 Sagres Crescent, Toronto, Ont., M6N 5E4 Phone:416-459-15tb Email: mainframeii~a)omeilcom Date: 121022007 DETAILED DESCRIPTION OF THE INVENTION
The invention (device) produces directional force propelling itself with no mechanical moving parts in a gaseous or fluid material by employing multiple principles found in the theories of Electricity, Electromagnetism, Electrostatics and Fluid dynamics.
As best seen in Fig. 1, the invention is comprised of two partial hollow spheres spliced together at a small radial cross-section with one forming the top surface plate 1 of the device and other forming the bottom surface plate 3. The top and bottom surfaces are made of highly electrical conductive material. These two surface plates are separated and internally laced with highly non-conductive material 4. In the interior of the device, just inside where the two sphere cross-sections meet, is a varying high voltage electric, closed-loop, conducting wire-solenoid(s) 2 which travels around the internal perimeter of the device.
As best seen in Fig. 2, the wire-solenoid(s) is used the produce an electromagnetic field having a field direction pointing up on the exterior of the device 5. The device generates an extremely high varying electrostatic positive charge potential ranging from OVDC to in excess of +40000VDC on the top surface plate 2 and an equally corresponding negative charge on the bottom surface plate 6 by means of a built-in high voltage DC
power system which can be a battery, gasoline powered electric DC generator, or any other power device utilizing a high voltage transformer placed in the center of the interior of the device between the two plates as seen in Fig. 1, 7.
As best seen in Fig. 1, the DC power system is incased in a container 5 which shields its contents from the electrostatic and electromagnetic fields with a layer of non-conductive material and another of conductive material. Electric conductive wiring 8 attaches the high voltage DC transformer to the top and bottom plates providing a positive and negative charge respectively and provides electric current to the wire-solenoid(s) traveling around the interior diameter of the device.
As best seen in Fig. 2, the high electrostatic positive charge potential on the top surface plate 2 separates electrons from the surrounding gaseous material elements or compounds 3 above the device and absorbs the electrons leaving heavy, positively charged material elements or compounds (positive ions) 4. The positively charged top plate and the positively charged ions repel each other creating a low pressure cavity (vacuum) 1 between the top plate and gaseous material. The magnetic field generated by the interior wire-solenoid(s) captures and directs the positive ions to the negatively charged surface plate of the device 7 which makes the gaseous material flow around the device from positive surface plate to negative surface plate. This gaseous flow further assists in lowering the pressure above the device by invoking the principles of the Coanda effect and lift force which are fundamental to standard Fluid dynamics. The pressure differential of the gaseous or fluid material on the two opposite surfaces of the device cause the device to move in the direction of the positively charged top surface plate, which, if the device has its bottom plate facing the ground in Earth's atmosphere, is called lift. In essence, this device floats on air as a boat floats on water.
The invention (device) produces directional force propelling itself with no mechanical moving parts in a gaseous or fluid material by employing multiple principles found in the theories of Electricity, Electromagnetism, Electrostatics and Fluid dynamics.
As best seen in Fig. 1, the invention is comprised of two partial hollow spheres spliced together at a small radial cross-section with one forming the top surface plate 1 of the device and other forming the bottom surface plate 3. The top and bottom surfaces are made of highly electrical conductive material. These two surface plates are separated and internally laced with highly non-conductive material 4. In the interior of the device, just inside where the two sphere cross-sections meet, is a varying high voltage electric, closed-loop, conducting wire-solenoid(s) 2 which travels around the internal perimeter of the device.
As best seen in Fig. 2, the wire-solenoid(s) is used the produce an electromagnetic field having a field direction pointing up on the exterior of the device 5. The device generates an extremely high varying electrostatic positive charge potential ranging from OVDC to in excess of +40000VDC on the top surface plate 2 and an equally corresponding negative charge on the bottom surface plate 6 by means of a built-in high voltage DC
power system which can be a battery, gasoline powered electric DC generator, or any other power device utilizing a high voltage transformer placed in the center of the interior of the device between the two plates as seen in Fig. 1, 7.
As best seen in Fig. 1, the DC power system is incased in a container 5 which shields its contents from the electrostatic and electromagnetic fields with a layer of non-conductive material and another of conductive material. Electric conductive wiring 8 attaches the high voltage DC transformer to the top and bottom plates providing a positive and negative charge respectively and provides electric current to the wire-solenoid(s) traveling around the interior diameter of the device.
As best seen in Fig. 2, the high electrostatic positive charge potential on the top surface plate 2 separates electrons from the surrounding gaseous material elements or compounds 3 above the device and absorbs the electrons leaving heavy, positively charged material elements or compounds (positive ions) 4. The positively charged top plate and the positively charged ions repel each other creating a low pressure cavity (vacuum) 1 between the top plate and gaseous material. The magnetic field generated by the interior wire-solenoid(s) captures and directs the positive ions to the negatively charged surface plate of the device 7 which makes the gaseous material flow around the device from positive surface plate to negative surface plate. This gaseous flow further assists in lowering the pressure above the device by invoking the principles of the Coanda effect and lift force which are fundamental to standard Fluid dynamics. The pressure differential of the gaseous or fluid material on the two opposite surfaces of the device cause the device to move in the direction of the positively charged top surface plate, which, if the device has its bottom plate facing the ground in Earth's atmosphere, is called lift. In essence, this device floats on air as a boat floats on water.
Inventor: Robert Demelo Address: 15 Sagres Crescent, Toronto, Ont., M6N 5E4 Phone: 416-459-1500 Email: naintrarneii(a)amail.com Date: 17102/2007
Claims (7)
1. This invention (device) produces directional force and propels itself with no mechanical moving parts through a gaseous or fluid material or environment.
2. In combination defined in claim 1, directional force in a gaseous or fluid material is generated by means of pressure differential between the two oppositely charged halves of the invention.
3. In combination defined in claim 2, the pressure differential that causes directional force in a gaseous or fluid material is produced by ionizing the gaseous or fluid material above the invention's positively charged surface plate into positive ions which are then repelled away from the invention's positively charged surface plate producing low pressure cavity between the positively charged surface plate and the gaseous or fluid material. The gaseous or fluid pressure on the negatively charged surface plate remains nominal which produces direction force propelling the invention into the lower pressure cavity on the opposite side of the invention.
4. In combination defined in claim 3, the magnetic field generated by the internal wire-solenoid(s) which travels around the internal perimeter of the invention near where the two surface plates meet but never touch due to non-conducting material separating the plates, is used to further reduce the pressure above the positively charged top plate by capturing the heavy positive ions in its magnetic field and forcing them around the device to the negatively charge surface plate of the device.
5. In combination defined in claim 4, the electromagnetic field is used to generate fluid flow of the gaseous or fluid material around the device which lowers the gaseous or fluid pressure above the positive surface plate of the invention.
6. In combination defined in claim 4, the wire-solenoid(s) and the magnetic field it generates is further used to control the stability and direction of the invention as it propels itself through the gaseous or fluid material or environment by varying the electric current in the wire-solenoid(s).
7. In combination defined in claim 6, the electrically charged surface plates along with the generated magnetic field is further used to control the stability and direction of the device as it propels itself through the gaseous or fluid material or environment by varying the electrically charged potential in the surface plates of the device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA002610998A CA2610998A1 (en) | 2007-12-20 | 2007-12-20 | Electro pressure differential flying device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CA002610998A CA2610998A1 (en) | 2007-12-20 | 2007-12-20 | Electro pressure differential flying device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA2610998A1 true CA2610998A1 (en) | 2009-06-20 |
Family
ID=40792418
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002610998A Abandoned CA2610998A1 (en) | 2007-12-20 | 2007-12-20 | Electro pressure differential flying device |
Country Status (1)
| Country | Link |
|---|---|
| CA (1) | CA2610998A1 (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2489908A (en) * | 2011-01-07 | 2012-10-17 | Tomasz Bohun | Charged gas propulsion for aircraft and rockets |
| GB2607360A (en) * | 2021-09-27 | 2022-12-07 | Isaksen Guttorm | A light aircraft with an electrostatic propulsion system |
-
2007
- 2007-12-20 CA CA002610998A patent/CA2610998A1/en not_active Abandoned
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2489908A (en) * | 2011-01-07 | 2012-10-17 | Tomasz Bohun | Charged gas propulsion for aircraft and rockets |
| GB2607360A (en) * | 2021-09-27 | 2022-12-07 | Isaksen Guttorm | A light aircraft with an electrostatic propulsion system |
| GB2607360B (en) * | 2021-09-27 | 2023-07-12 | Isaksen Guttorm | A light aircraft with an electrostatic propulsion system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request |
Effective date: 20130228 |
|
| FZDE | Discontinued |
Effective date: 20151005 |