GB2331555A - Force producing apparatus - Google Patents
Force producing apparatus Download PDFInfo
- Publication number
- GB2331555A GB2331555A GB9724578A GB9724578A GB2331555A GB 2331555 A GB2331555 A GB 2331555A GB 9724578 A GB9724578 A GB 9724578A GB 9724578 A GB9724578 A GB 9724578A GB 2331555 A GB2331555 A GB 2331555A
- Authority
- GB
- United Kingdom
- Prior art keywords
- repulse
- turbo
- motor
- shaft
- turbine
- 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.)
- Withdrawn
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
- F03H—PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03H99/00—Subject matter not provided for in other groups of this subclass
-
- 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
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B17/00—Other machines or engines
- F03B17/005—Installations wherein the liquid circulates in a closed loop ; Alleged perpetua mobilia of this or similar kind
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Gear Transmission (AREA)
Abstract
The apparatus comprises two turbine/impeller-like devices 18,21 drivingly connected to each other by gearing, so that when shaft 3 is driven by an internal combustion engine or by batteries, the device 21 rotates at a slower speed than the device 18. Liquid (eg. water or water mixed with mercury) is impelled by the device 20 through part 5 of a closed channel to impact the blades of the device 21, allegedly producing an upward force on apparatus. A plurality of the apparatuses may be used to propel a space-ship (figures 4 and 5).
Description
2331555 i
FIELD AND SU MMA RY OF THE INVENTION
An object of the invention is the propelling of a spaceship in space for interplanetary travel by the "Turbo Repulse Motor". This uses turbines, driven by an internal combustion engine or a heavy duty battery.
The Turbo Repulse Motor comprises of a four radial cornered housing body provided with multiple turbines. The fast rotating turbine repulse against liquid (for example water, ora mixture of water and mercury). on the a-b radial zone arranged on the horizontal line x-x. This forces the turbines to go in an upward direction. The slow rotating turbine brakes and slows down the fast running liquid on c-d radial zone. This forces the turbine to go in an upward direction.
Another object of this invention is a platform type spaceship fitted with multiple Turbo Repulse Motors. This would enable take-off, control of balance, vertical landing and turning the spaceship upside-down and propelling it in the opposite direction to reduce the high speed before landing on another planet. The spaceship is provided with two small similar motors arranged sideways (which are turnable) to,prevent spin and for cruising purposes. The platform can be equipped for transporting atom waste containers into outer-space, collecting space debris and transporting valuable materials in our solar system. Such spaceships would be ideal for tourism.
BRIEF DESCRIPTION OF THE INVENTION
A specific embodiment of the invention will now be described by way of example with reference to the accompanying drawings which:
Fig 1: shows a Turbo Repulse Motor.
Fig 2: is a sectional view of fig 1 on line A-A.
Fig 3: shows a diagrammatic gear transmission.
Fig 4: is a top view of the platform spaceship.
Fig 5: is a side view of the platform spaceship.
1 1 1 1 lim a Turbo Repulse Motor comprising of a four radial cornered channel housing body 8 (see fig 1 and 2) for running a liquid (water or mixture of water with mercury etc). The housing body is provided with two turbines 18 and 21 positioned centrally on the horizontal line x-x. The channelled end 10 via the radial bend 22 to the other end 2 is twice as wide than on the lower channelled part 5, see fig 1 and 2. The turbine 18 having a shaft 3, assembled in the bearing housings 4 an 16. One end of the shaft would be connected to an internal combustion engine anda bevel gear 11 is fitted to the other end of the shaft 3, see figure 1. The bevel gear 11 turns the second bevel gear 15 of the same size having the same amount of teeth and is fitted on the shaft 14 which rotate in the bracket 23 fixed to the housing body between the two turbines (see fig 3). A similar third bevel gear 24 is fitted on the other end of the same shaft 14. The bevel gear 24 turns a large bevel gear 13 which is fitted on the shaft 19 of the turbine 21. The large bevel gear has twice as many teeth. Therefore, if the small gear 11, from the turbine 18, turns 2000 rpm, then the large gear 13, from the turbine 21, will turn 1000 rpm only. The two turbines have the same amount of blades 20 and same diametrical size. The blades of the turbine 21 are twice as wide as those on the turbine 18.
The left hand side turbine 18 is the repulse turbine whose blades 20 repulse against liquid on the a-b radial zone and force the housing body to go upward. The right hand side turbine 21 is the braking turbine which blades 20 slow down the fast running liquid on the c-d radial zone thus causing the housing body to go upward; Twice the volume of slow running liquid runs at a slower speed through the upper part d-a zone then through the lower part b-c zone of the narrow channel 5, thus causing an equal centrifugal force pull between upper radial part 22 and the lower radial part 17 of the turbo repulse motor (see gear ratio shown on fig 3). The room between the two wide blades 20 of the turbine 21 will suddenly be filled with thrusting liquid from the narrow channel 5, at the end 10, thus forcing the turbine to go in an upward direction.
For'rigidity, the housing body is supported by ribs 9, see fig 1 and 2. Two arrows in the centre of the housing body showthe direction of the rotating shafts 3 and 19, see fig 2. Bolts 6, base 7, a large boss 12 for extended shaft 19 of the turbine 21 to support the large level gear 13.
On figure 3 is a view of the diagrammatic gear transmission having a bevel gear 11 mounted on the shaft 3 of the turbine 18, which turns the similar bevel gear 15 mounted on the shaft 14 which is accommodated in the bearing housing 23. The other end of the shaft 14 having a third similar bevel gear 24 which turns a large bevel gear 13 provided with twice as many teeth than any of the three small bevel gears in order to reduce the Turbo Repulse Motor comprising of a four radial cornered channel housing body 8 (see fig 1 and 2) for running a liquid (water or mixture of water with mercury etc). The housing body is provided with two turbines 18 and 21 positioned centrally on the horizontal line x-x. The channelled end 10 via the radial bend 22 to the other end 2 is twice as wide than on the lower channelled part 5, see fig I and 2. The turbine 18 having a shaft 3, assembled in the bearing housings 4 an 16. One end of the shaft would be connected to an internal combustion engine anda bevel gear 11 is fitted to the other end of the shaft 3, see figure 1. The bevel gear 11 turns the second bevel gear 15 of the same size having the same amount of teeth and is fitted on the shaft 14 which rotate in the bracket 23 fixed to the housing body between the two turbines (see fig 3) A similar third bevel gear 24 is fitted on the other end of the same shaft 14. The bevel gear 24 turns a large bevel gear 13 which is fitted on the shaft 19 of the turbine 21. The large bevel gear has twice as many teeth. Therefore, if the small gear 11, from the turbine 18, turns 2000 rpm, then the large gear 13, from the turbine 21, will turn 1000 rpm only. The two turbines have the same amount of blades 20 and same diametrical size. The blades of the turbine 21 are twice as wide as those on the turbine 18.
The left hand side turbine 18 is the repulse turbine whose blades 20 repulse against liquid on the a-b radial zone and force the housing body to go upward. The right hand side turbine 21 is the braking turbine which blades 20 slow down the fast running liquid on the c-d radial zone thus causing the housing body to go upward. Twice the volume of slow running liquid runs at a slower speed through the upper part d-a zone then through the lower part b-c zone of the narrow channel 5, thus causing an equal centrifugal force pull between upper radial part 22 and the lower radial part 17 of the turbo repulse motor (see gear ratio shown on fig 3). The room between the two wide blades 20 of the turbine 21 will suddenly be filled with thrusting liquid from the narrow channel 5, at the end 10, thus forcing the turbine to go in an upward direction.
For rigidity, the housing body is supported by ribs 9, see fig 1 and 2. Two arrows in the centre of the housing body showthe direction of the rotating shafts 3 and 19, see fig 2. Bolts 6, base 7, a large boss 12 for extended shaft 19 of the turbine 21 to support the large level gear 13.
On figure 3 is a view of the diagrammatic gear transmission having a bevel gear 11 mounted on the shaft 3 of the turbine 18, which turns the similar bevel gear 15 mounted on the shaft 14 which is accommodated in the bearing housing 23. The other end of the shaft 14 having a third similar bevel gear 24 which turns a large bevel gear 13 provided with twice as many teeth than any of the three small bevel gears in order to reduce the 4 rotation of the turbine 21 and to decelerate the running speed of the liquid on c-d zone. See fig 2.
Figure 4 is a top view of the platform type spaceship comprising of a platform 46 on which 8 Turbo Repulse Motors are mounted in pairs number 26 and 27, 28 and 29, 30 and 31, 32 and 33 (in cross-way arrangement) to enable the spaceship to lift up with balancing control and propels into space. Each Turbo Repulse Motor is provided with internal combustion engine to drive the multiple turbines to generate repulse, numbered as follows: 34 and 35, 36 and 37, 38 and 39, 40 and 41. (See also figure 5).
Figure 5 is a side view of the platform type spaceship having an external body 50 to accommodate the astronauts and tourists. Also there is a room for other necessities. The platform 46 is mounted on top of the body and supported by several brackets (42 and 55). Smaller sized Turbo Repulse Motors 47 and 54 are fitted under the platform for cruising purposes above the earth and other planets. These also prevent spin and are for changing direction during the cruise. The spaceship is provided with workshop 45, forward observation post 43 provided with window 44 and landing observation post 52 with window 51. Two smaller types of internal combustion engines or heavy duty batteries 48 to drive the small Turbo Repulse Motors.
-T
Claims (4)
1. A Turbo Repulse Motor comprising a housing body provided with multiple turbines arranged on the horizontal line xx, having a wide upper part channelled body 1 through which a liquid runs at a slow speed and a narrow lower part channelled body 5 through which a liquid runs at a fast speed, produced by the multiple turbines, a turbine 18 having a shaft 3 accommodated in a bearing housings 4 and 16 grab with the provided blades 20 the slow runnning liguid from a wide channelled body 1 and throw away the fast running liquid produced by the turbine 18 into a narrow channelled body 5 via a radial bend 17 escaping through the end 10 and strike forcibly against the blades 20 of a slow rotating turbine 21, thus causing the Turbo repulse Motor to go in an upwards direction.
2. A Turbo Repulse Motor as claimed in claim 1, provided for a platform type spaceship, with multiple Turbo Repulse Motors fitted securely on or under a platform for a lift up balancing and propelling the spaceship and with a smaller size multiple turbo repulse motors fitted on the outside periphery of the spaceship to prevent the spin, also for cruising pruposes above the surface of the earth and other planets.
A Turbo Repulse Motor as claimed in claim 1, having a bevel gear 11 mounted on the shaft
3 which turns a similar bevel gear 15 mounted on a shaft 14, said the shaft which is accommodated in the bearing housing 23 having a third similar bevel gear 24 which turns a large bevel gear 13bmounted on a shaft 19 of the turbine 21, are provided to control the rotating speed of the two turbines for variable speed (rpm) in order to achieve a necessary repulse and equal centrifugal force pull of the upper and lower parts of the Turbo Repulse Motor.
4. A Turbo Repulse Motor as claimed in claim 1, diamond shaped housing body with four radial corners, having two turbines on each side, the housing body channel (tunel) is provided with liquid stored pernanently, when t-he two turbines are in motion the liquid in the turbines opposite casing, nearby the two directional arrows, is absent.
A Turbo Repulse Motor as claimed herein before described with refe!.rence to figures 1, 2, 3 and 4 of the accompanying drawings.
4.
A Turbo Repulse Motor as herein before described with reference to figures 1 to 5 of the accompanying drawings.
Amendments to the claims have been filed as folkws CLAIMS 3.
1. A Turbo Repulse Motor comprising a housing body provided with multiple turbines arranged on the horizontal line xx, having a wide upper part channelled body'l through which a liquid runs at a slow speed and a harrow lower part channelled body 5 through which a liquid runs at a fast speed, produced by the multiple turbines, a turbine 18 having a shaft 3 accommodated in a bearing housings 4 and 16 grab with the provided blades 20 the slow runnning liquid from a wide channelled body 1 and throw away the fast running liquid produced by the turbine 18 into a narrow channelled body 5 via a radial bend 17 escaping through the end 10 and: vLs forcibly against the blades 20 of a slow rotating turbine 21, thus causing the Turbo repulse Motor to go in an upwards direction.
A Turbo Repulse Motor as claimed in claim 1, provided for a platform type spaceship, with multiple Turbo Repulse Motors fitted securely on or under a platform for a lift up balancing and propelling the spaceship and with a smaller size multiple turbo repulse motors fitted on the outside periphery of the spaceship to prevent the spin, also for cruising pruposes above the surface of the earth and other planets.
A Turbo Repulse Motor as claimed in claim 1, having a bevel gear 11 mounted on the shaft 3 which turns a similar bevel gear 15 mounted on a shaft 14, said the shaft which is accommodated in the bearing housing 23 having a third similar bevel gear 24 which turns a large bevel gear 13 mounted on a shaft 19 of the turbine 21, are provided to control the rotating speed of the two turbines for variable speed (rpm) in order to achieve a necessary repulse and equal centrifugal force pull of the upper and lower parts of the Turbo Repulse Motor.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9724578A GB2331555A (en) | 1997-11-20 | 1997-11-20 | Force producing apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9724578A GB2331555A (en) | 1997-11-20 | 1997-11-20 | Force producing apparatus |
Publications (2)
Publication Number | Publication Date |
---|---|
GB9724578D0 GB9724578D0 (en) | 1998-01-21 |
GB2331555A true GB2331555A (en) | 1999-05-26 |
Family
ID=10822397
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9724578A Withdrawn GB2331555A (en) | 1997-11-20 | 1997-11-20 | Force producing apparatus |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2331555A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009081086A1 (en) * | 2007-12-24 | 2009-07-02 | Byson Peter Roger J R | Self powered pneumatic engine |
WO2012137366A1 (en) * | 2011-04-06 | 2012-10-11 | グレースマリー・ワールド株式会社 | Space propulsion and space endurance flight system |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1094169A (en) * | 1965-10-13 | 1967-12-06 | Twin Disc Clutch Co | Multiple stage, hydraulic jet propulsion apparatus for water craft |
GB1119687A (en) * | 1966-11-21 | 1968-07-10 | Buehler Corp | Watercraft propulsion pump |
GB1582980A (en) * | 1976-08-09 | 1981-01-21 | Bizzarri A | Fluid flow devices |
GB2297358A (en) * | 1995-01-26 | 1996-07-31 | John Hunter | Turbine system |
WO1996034198A1 (en) * | 1995-04-28 | 1996-10-31 | Ramirez Garcia Jose | Propulsion system based on action-reaction imbalance |
-
1997
- 1997-11-20 GB GB9724578A patent/GB2331555A/en not_active Withdrawn
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1094169A (en) * | 1965-10-13 | 1967-12-06 | Twin Disc Clutch Co | Multiple stage, hydraulic jet propulsion apparatus for water craft |
GB1119687A (en) * | 1966-11-21 | 1968-07-10 | Buehler Corp | Watercraft propulsion pump |
GB1582980A (en) * | 1976-08-09 | 1981-01-21 | Bizzarri A | Fluid flow devices |
GB2297358A (en) * | 1995-01-26 | 1996-07-31 | John Hunter | Turbine system |
WO1996034198A1 (en) * | 1995-04-28 | 1996-10-31 | Ramirez Garcia Jose | Propulsion system based on action-reaction imbalance |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2009081086A1 (en) * | 2007-12-24 | 2009-07-02 | Byson Peter Roger J R | Self powered pneumatic engine |
WO2012137366A1 (en) * | 2011-04-06 | 2012-10-11 | グレースマリー・ワールド株式会社 | Space propulsion and space endurance flight system |
Also Published As
Publication number | Publication date |
---|---|
GB9724578D0 (en) | 1998-01-21 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |