US20070160472A1 - Additional drive system by diverting a fluid flow - Google Patents

Additional drive system by diverting a fluid flow Download PDF

Info

Publication number
US20070160472A1
US20070160472A1 US10/598,157 US59815705A US2007160472A1 US 20070160472 A1 US20070160472 A1 US 20070160472A1 US 59815705 A US59815705 A US 59815705A US 2007160472 A1 US2007160472 A1 US 2007160472A1
Authority
US
United States
Prior art keywords
use according
channel
propulsion
vehicle
diversion
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
US10/598,157
Inventor
Wolfgang Jobmann
Peter Stamme
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.)
Wolfgang Jobmann GmbH
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Assigned to WOLFGANG JOBMANN GMBH reassignment WOLFGANG JOBMANN GMBH ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: JOBMANN, WOLFGANG, STAMME, PETER
Publication of US20070160472A1 publication Critical patent/US20070160472A1/en
Abandoned legal-status Critical Current

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H9/00Marine propulsion provided directly by wind power
    • B63H9/02Marine propulsion provided directly by wind power using Magnus effect
    • 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
    • Y02T70/00Maritime or waterways transport
    • Y02T70/50Measures to reduce greenhouse gas emissions related to the propulsion system
    • Y02T70/5218Less carbon-intensive fuels, e.g. natural gas, biofuels
    • Y02T70/5236Renewable or hybrid-electric solutions

Definitions

  • the invention relates to a new use of a drive system working on the basis of the Magnus effect for the purpose of an additional drive for an existing propulsion system.
  • Additional wind drive systems are known which are based on the Magnus effect (Magnus, 1852), which make use of further physical bases (Prantl, 1904) for this and were implemented for the first time in the development of the Flettner rotor (Flettner, 1922), cf. also GB-A 2 102 755 (Blohm & Voss) with a “Flettner rotor” for ship propulsions.
  • the Flettner rotor was put into practice on the basis of tests of AVA, Göttingen (1922-1924) by Germania-Werft with the rebuilding of the “Buckau” sailing ship (1924) and the RMS “Barbara” (1926).
  • the object of the invention is an additional drive system which can generate a propulsion even in the case of a fluid flow that impacts directly from the front.
  • the fluid may consist both of air, gases or liquids.
  • the examples are directed to an air flow, the invention nevertheless comprises all types of fluid flows (claims 1 , 2 , 17 , 20 ).
  • the idea covered by the invention is the diverting of fluid generated by the travel speed that impinges on a rotating cylinder from the front to generate a propulsion on the basis of the Magnus effect.
  • the additional drive system is connected with a vehicle which itself and independently has a further drive which can be called the main drive.
  • the additional drive system which utilizes the fluid flow caused by the motion is used in addition to this main drive (in the direction of a forwardly directed driving power). It is in particular advantageous to additionally drive such vehicles and to thus reduce driving energy in the sense of fuels, which have a normal speed range between 50 km/h and 100 km/h, in particular in the range of more or less 80 km/h.
  • Land craft such as trucks or automobiles which are mentioned here with preference, but not exclusively, are moved relatively quickly (measured above the ground) and, nevertheless, they can utilize the additional effects of the rotating cylinder at speeds which are far below of those of aircraft, against which fluid generated by the travel speed flows, namely after a diverting.
  • the supplementary propulsion is caused by the Magnus effect in such a way that the craft is additionally driven in the propulsion direction saving a noticeable amount of its own fuel or resources that are required by the main drive.
  • the use covers the influence of the fluid entering the channel from the front with its diverting so that it is passed onto the Magnus rotor which is vertically or horizontally disposed (claim 1 , claim 2 ).
  • Claims 14 to 16 cover the vehicles that are moved relatively quickly and move above the respective ground, i.e. have a speed of more than about 10 km/h in the case of ships and naval craft, and clearly more than this speed, more than substantially 50 km/h to 100 km/h in the case of land craft, but clearly less than the speed of aircraft, the speed of which is too high since in these speed ranges the effectiveness of the additional drive system by the Magnus effect is no longer advantageously created as in the speed ranges indicated above.
  • GB-A 371,691 (Medvedeff) describes an airship with an angularly designed channel in which three Magnus rotors are inserted, which are electrically driven. These rotors are located horizontally to the plane of the main ship and together are of a U-shape, only the central rotor providing for the propulsion in the longitudinal direction of the airship. Several turbines suck in air through laterally existing openings to a channel, which is supplied to the rotors for the generation of a propulsion force from the one rotor and for generating a lifting power as regards the two other rotors. An additional drive system is not described here.
  • GB-A 2 256 410 (MacDuff) shows a watercraft according to FIGS.
  • FIG. 4 to 6 thereof which can also be used in a floating platform according to FIG. 11 thereof or a submarine according to FIG. 12 thereof, a water flow in a water channel being utilized, which is generated by a pump in the channel.
  • This drive system provides for the propulsion of the “naval craft” (as a summary term for the mentioned individual objects), but it is not designed in addition to another existing system, but is the only main drive system for the propulsion of the naval craft.
  • GB-A 494,093 Gavrilov
  • individual rotors working in accordance with the Magnus principle are shown in FIG. 12 thereof, which are described as “finger-like” elements. These finger-like elements can be disposed on a plurality of points of a ship or a submarine, cf.
  • FIGS. 4 to 12 thereof, said points being not explained in detail here, but are used in addition to a presumably existing main drive system of the ship.
  • no fluid flow in a channel is utilized in the arrangement of these finger-like elements, but the fluid flow laterally flowing past the ship, which, however, is not diverted.
  • FIG. 1 shows a possible design, in which the relative wind F enters a channel 10 and is upwardly diverted.
  • FIG. 2 is a front view of the air inlet of the channel 10 in two variants as FIGS. 2 a , 2 b.
  • FIG. 3
  • FIG. 3 a is a variant with changed diversion.
  • FIG. 4
  • FIG. 4 a is a further variant with a changed position of the rotating cylinder.
  • FIG. 5 is a variant with a baffle plate in front of the diversion section.
  • FIG. 6 is a variant with a diversion of the fluid generated by the travel speed towards below.
  • FIG. 1 A first variant is shown in FIG. 1 .
  • the relative wind F enters the channel 10 and is upwardly diverted before it impinges on the horizontally disposed, rotating cylinder 20 .
  • the first force 30 and the second force 40 result which act on the channel 10 .
  • the drive or transverse drive 50 that is generated by the rotating cylinder is, however, several times higher, and the “resultant force” 60 results as a propulsion.
  • This force is transmitted to the vehicle Z (not shown) (in FIG. 2 outlined below the channel 10 ).
  • the main propulsion system e.g. an engine, that is not represented in greater detail, is disposed, which drives wheels through a transmission.
  • the relative wind entering the channel 10 is drawn entering an inlet opening 10 ′ as indicated in FIG. 1 , it is then guided along a section of the channel and upwardly diverted by a diversion point 10 ′′, in order to be guided to the rotating cylinder 20 which is disposed in a higher section.
  • the rotational speed and/or direction ⁇ of the cylinder is drawn so that the corresponding air flow on one side of the cylinder is added to the speed and is subtracted from it on the other side of the cylinder.
  • the drive or transverse drive 50 and the force 30 that is vertical to it results from this.
  • the resultant force 60 is transmitted to the channel 10 and from there to the craft which is represented in two variants in FIG. 2 , on the one hand, with a completely open air inlet 10 as in FIG.
  • FIG. 2 a and FIG. 2 b are in each case intended with reference to an entire vehicle Z and/or an entire vehicle width.
  • FIG. 2 shows a front view of two types of the air entry and/or the channel guiding 10 ′ or 10 + with divided air inlets F′.
  • the guiding of the fluid is positively covered with a channel which guides the fluid, but on the other hand, is also described as such with “air inlet”, “passing on of air” and “diversion”. This is to be complimentarily understood, on the one hand, the guided fluid, and, on the other hand, the object guiding it.
  • the latter is coupled to the vehicle at a connection surface 10 a.
  • the speed of the cylinder 20 is preferably in the order of between twice to four times the air speed in the channel 10 which can also be coordinated with the regular locomotion speed of the respective vehicle and also be changed by means of a control means.
  • the main speed is meant by regular driving speed which a vehicle has, e.g. trucks which are preferably operated in a range of more or less 80 km/h in the forward direction in the long run or automobiles which, if there is a speed restricted, are operated at a speed of 50 km/h to 100 km/h. In the case of craft on the water the speed is reduced, always in relation to the medium on which the craft is moved “relatively quickly”, here, at more than 10 km/h.
  • the diversion 10 ′′ of the air flow F that impacts from the front (and enters the channel 10 ) can be implemented by an angle deviating from 90° as shown in FIGS. 3, 3 a ; due to this, a changed direction of the resultant force 60 ′ is achieved.
  • the transverse drive 50 generated by the rotating cylinder 20 can be increased in a further variant by the fact that this cylinder is not disposed in the center of the fluid channel 10 , but asymmetrically to it.
  • the differences in the masses b, c show this, the diameter d of the rotating cylinder 20 being the same.
  • the fluid channel may be covered by a baffle plate 80 in front of its diversion 10 ′′ in order to reduce the aerodynamic drag of the fluid generated by the travel speed.
  • the diverting of the relative wind (as an example of the fluid) can both be implemented upwards and downwards.
  • the direction of the resultant force 60 is shifted by this as is shown in FIG. 6 .
  • a propulsion is generated in both variants.
  • a further variant (not shown) comprises one or several rotating cylinders 20 that are vertically disposed (as in the Flettner rotor). A diversion of the air flow in the fluid channel 10 takes place towards the side in order to generate the desired propulsion.
  • the channel 10 may be designed in a rectangular fashion as shown in FIGS. 1, 2 (variant 1 ). Alternatively, the channel 10 may be divided; here, these (several) channels 10 * may in each case be of a rectangular, elliptical or circular design. as is shown in FIG. 2 b.

Landscapes

  • Engineering & Computer Science (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Ocean & Marine Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Wind Motors (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
  • Preparation Of Compounds By Using Micro-Organisms (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Massaging Devices (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Earth Drilling (AREA)
  • Toys (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Pipe Accessories (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • External Artificial Organs (AREA)
  • Flow Control (AREA)
  • Paper (AREA)

Abstract

The invention relates to the use of a drive system worlding on the basis of the Magnus Effect which is used to provide a drive mechanism in addition to an existing drive device. The aim of the invention is to produce a drive directly in front of the front impacting fluid flow. The invention also relates to the use of a drive system for a relatively fast moving vehicle by means of a first drive system, said drive system comprising a rotating, horizontally arranged cylinder (20) provided with end disks (70) as an additional drive. A fluid flow (F), which is produced by the first drive system, enters into a channel (10) and is diverted (10″) in the direction thereof in said channel whereupon it impinges upon the rotating cylinder (20). The complimentary drive is produced in a desired direction based on the Magnus Effect.

Description

  • The invention relates to a new use of a drive system working on the basis of the Magnus effect for the purpose of an additional drive for an existing propulsion system.
  • Additional wind drive systems are known which are based on the Magnus effect (Magnus, 1852), which make use of further physical bases (Prantl, 1904) for this and were implemented for the first time in the development of the Flettner rotor (Flettner, 1922), cf. also GB-A 2 102 755 (Blohm & Voss) with a “Flettner rotor” for ship propulsions.
  • The Flettner rotor was put into practice on the basis of tests of AVA, Göttingen (1922-1924) by Germania-Werft with the rebuilding of the “Buckau” sailing ship (1924) and the RMS “Barbara” (1926).
  • With these additional wind drive systems wind and relative wind flows directly against a driven rotating circular cylinder (rotor); quite a considerable propulsion is generated by the Magnus effect.
  • A disadvantage of these additional drive systems is that they can only generate a propulsion in the case of specific directions of the wind (up to 2 points in the direction of motion).
  • For this reason, these known additional drive systems cannot be used for vehicles which are moving relatively quickly, since, due to the strong relative wind, the entire wind flow takes place substantially from the front and is thus outside the range of action.
  • The object of the invention is an additional drive system which can generate a propulsion even in the case of a fluid flow that impacts directly from the front.
  • Here, the fluid may consist both of air, gases or liquids. Although the examples are directed to an air flow, the invention nevertheless comprises all types of fluid flows (claims 1, 2,17, 20).
  • The idea covered by the invention is the diverting of fluid generated by the travel speed that impinges on a rotating cylinder from the front to generate a propulsion on the basis of the Magnus effect. For this purpose, the additional drive system is connected with a vehicle which itself and independently has a further drive which can be called the main drive. The additional drive system which utilizes the fluid flow caused by the motion is used in addition to this main drive (in the direction of a forwardly directed driving power). It is in particular advantageous to additionally drive such vehicles and to thus reduce driving energy in the sense of fuels, which have a normal speed range between 50 km/h and 100 km/h, in particular in the range of more or less 80 km/h. Land craft such as trucks or automobiles which are mentioned here with preference, but not exclusively, are moved relatively quickly (measured above the ground) and, nevertheless, they can utilize the additional effects of the rotating cylinder at speeds which are far below of those of aircraft, against which fluid generated by the travel speed flows, namely after a diverting. The supplementary propulsion is caused by the Magnus effect in such a way that the craft is additionally driven in the propulsion direction saving a noticeable amount of its own fuel or resources that are required by the main drive.
  • The use covers the influence of the fluid entering the channel from the front with its diverting so that it is passed onto the Magnus rotor which is vertically or horizontally disposed (claim 1, claim 2).
  • Special designs of the shape of the channel (claims 10 to 12) and the orientation of the diversion (claims 3 to 7) enable adaptations to the use, e.g. in the case of land craft (claim 13) which are vehicles that are moved relatively quickly and in which the relative wind (as a fluid) flows substantially from the front. The relative wind itself is (primarily) generated by the regular drive (propulsion) of the vehicle and enables thus the utilization of this flowing fluid with and by the additional drive system that is provided with the diversion. A displacement of the rotating cylinder from the center of the channel (claim 8, claim 9) enables an increase in this effect.
  • Claims 14 to 16 cover the vehicles that are moved relatively quickly and move above the respective ground, i.e. have a speed of more than about 10 km/h in the case of ships and naval craft, and clearly more than this speed, more than substantially 50 km/h to 100 km/h in the case of land craft, but clearly less than the speed of aircraft, the speed of which is too high since in these speed ranges the effectiveness of the additional drive system by the Magnus effect is no longer advantageously created as in the speed ranges indicated above.
  • It is understood that the use inherently also covers a process as a driving process (claim 18) and that, since an additional drive system is covered, the device as such includes its inherent function as the use in additional to an existing drive system (claims 21, 22).
  • GB-A 371,691 (Medvedeff) describes an airship with an angularly designed channel in which three Magnus rotors are inserted, which are electrically driven. These rotors are located horizontally to the plane of the main ship and together are of a U-shape, only the central rotor providing for the propulsion in the longitudinal direction of the airship. Several turbines suck in air through laterally existing openings to a channel, which is supplied to the rotors for the generation of a propulsion force from the one rotor and for generating a lifting power as regards the two other rotors. An additional drive system is not described here. GB-A 2 256 410 (MacDuff) shows a watercraft according to FIGS. 4 to 6 thereof, which can also be used in a floating platform according to FIG. 11 thereof or a submarine according to FIG. 12 thereof, a water flow in a water channel being utilized, which is generated by a pump in the channel. This drive system provides for the propulsion of the “naval craft” (as a summary term for the mentioned individual objects), but it is not designed in addition to another existing system, but is the only main drive system for the propulsion of the naval craft. In GB-A 494,093 (Gavrilov) individual rotors working in accordance with the Magnus principle are shown in FIG. 12 thereof, which are described as “finger-like” elements. These finger-like elements can be disposed on a plurality of points of a ship or a submarine, cf. in this connection FIGS. 4 to 12 thereof, said points being not explained in detail here, but are used in addition to a presumably existing main drive system of the ship. However, no fluid flow in a channel is utilized in the arrangement of these finger-like elements, but the fluid flow laterally flowing past the ship, which, however, is not diverted.
  • Examples explain and supplement the invention.
  • FIG. 1 shows a possible design, in which the relative wind F enters a channel 10 and is upwardly diverted.
  • FIG. 2 is a front view of the air inlet of the channel 10 in two variants as FIGS. 2 a, 2 b.
  • FIG. 3,
  • FIG. 3 a is a variant with changed diversion.
  • FIG. 4,
  • FIG. 4 a is a further variant with a changed position of the rotating cylinder.
  • FIG. 5 is a variant with a baffle plate in front of the diversion section.
  • FIG. 6 is a variant with a diversion of the fluid generated by the travel speed towards below.
  • A first variant is shown in FIG. 1. In this variant, the relative wind F enters the channel 10 and is upwardly diverted before it impinges on the horizontally disposed, rotating cylinder 20. The first force 30 and the second force 40 result which act on the channel 10. The drive or transverse drive 50 that is generated by the rotating cylinder is, however, several times higher, and the “resultant force” 60 results as a propulsion. This force is transmitted to the vehicle Z (not shown) (in FIG. 2 outlined below the channel 10). Here, the main propulsion system, e.g. an engine, that is not represented in greater detail, is disposed, which drives wheels through a transmission.
  • The relative wind entering the channel 10 is drawn entering an inlet opening 10′ as indicated in FIG. 1, it is then guided along a section of the channel and upwardly diverted by a diversion point 10″, in order to be guided to the rotating cylinder 20 which is disposed in a higher section. The rotational speed and/or direction ω of the cylinder is drawn so that the corresponding air flow on one side of the cylinder is added to the speed and is subtracted from it on the other side of the cylinder. The drive or transverse drive 50 and the force 30 that is vertical to it results from this. The resultant force 60 is transmitted to the channel 10 and from there to the craft which is represented in two variants in FIG. 2, on the one hand, with a completely open air inlet 10 as in FIG. 1 and, on the other hand, with several channels 10*, which are adjacent in order to guide the direction of flow of the fluid F, to divert it and to then guide it onto the rotating cylinder 20 which is driven by an engine M (not shown) and held by bearings 18, 19, which are shown in greater detail in FIG. 2.
  • The representation that two different types of the guiding of the flow are represented in one picture one above the other is not to obscure the fact that the left-hand and right-hand sides of FIG. 2, i.e. FIG. 2 a and FIG. 2 b, are in each case intended with reference to an entire vehicle Z and/or an entire vehicle width.
  • As shown in FIG. 2 the rotating cylinder 20 is disposed transversely to the direction of travel in this variant and, in a further variant, it is preferably provided with end plates 70 in order to further increase the effect of the Magnus effect. This FIG. shows a front view of two types of the air entry and/or the channel guiding 10′ or 10+ with divided air inlets F′.
  • The guiding of the fluid is positively covered with a channel which guides the fluid, but on the other hand, is also described as such with “air inlet”, “passing on of air” and “diversion”. This is to be complimentarily understood, on the one hand, the guided fluid, and, on the other hand, the object guiding it. The latter is coupled to the vehicle at a connection surface 10 a.
  • The speed of the cylinder 20, that is driven by the engine, is preferably in the order of between twice to four times the air speed in the channel 10 which can also be coordinated with the regular locomotion speed of the respective vehicle and also be changed by means of a control means. The main speed is meant by regular driving speed which a vehicle has, e.g. trucks which are preferably operated in a range of more or less 80 km/h in the forward direction in the long run or automobiles which, if there is a speed restricted, are operated at a speed of 50 km/h to 100 km/h. In the case of craft on the water the speed is reduced, always in relation to the medium on which the craft is moved “relatively quickly”, here, at more than 10 km/h.
  • In further variants, the diversion 10″ of the air flow F that impacts from the front (and enters the channel 10) can be implemented by an angle deviating from 90° as shown in FIGS. 3, 3 a; due to this, a changed direction of the resultant force 60′ is achieved.
  • As is shown in FIGS. 4, 4 a, the transverse drive 50 generated by the rotating cylinder 20 can be increased in a further variant by the fact that this cylinder is not disposed in the center of the fluid channel 10, but asymmetrically to it. The differences in the masses b, c show this, the diameter d of the rotating cylinder 20 being the same.
  • Due to this asymmetric arrangement, the speed of the air on the side of the cylinder which is in the direction of travel is additionally accelerated and the generated vacuum is increased to bring about the transverse drive 50.
  • As is represented in FIG. 5, the fluid channel may be covered by a baffle plate 80 in front of its diversion 10″ in order to reduce the aerodynamic drag of the fluid generated by the travel speed.
  • The diverting of the relative wind (as an example of the fluid) can both be implemented upwards and downwards. The direction of the resultant force 60 is shifted by this as is shown in FIG. 6. However, a propulsion is generated in both variants.
  • A further variant (not shown) comprises one or several rotating cylinders 20 that are vertically disposed (as in the Flettner rotor). A diversion of the air flow in the fluid channel 10 takes place towards the side in order to generate the desired propulsion.
  • The channel 10 may be designed in a rectangular fashion as shown in FIGS. 1, 2 (variant 1). Alternatively, the channel 10 may be divided; here, these (several) channels 10* may in each case be of a rectangular, elliptical or circular design. as is shown in FIG. 2 b.

Claims (24)

1. Use of a propulsion system for a vehicle which is moved relatively quickly with a first propulsion system, which comprises a rotating, horizontally disposed cylinder (20), preferably with end plates (70), as an additional propulsion, a fluid flow (F) generated by the first propulsion system entering a channel (10) and being diverted in the channel in its direction (10″) and impinging on the rotating cylinder (20), whereby the supplementary propulsion is generated on the basis of the Magnus effect in a desired direction.
2. The use of a propulsion system on the basis of the Magnus effect with a rotating, vertically disposed cylinder (20), preferably with end plates, in addition to an existing propulsion system, wherein a fluid flow (F) in a channel (10), which is diverted in its direction, impinges onto the rotating cylinder (20) and generates a supplementary propulsion in a desired direction.
3. The use according to claim 1, wherein the diversion (10″) takes place upwards.
4. The use according to claim 1, wherein the diversion takes place downwards.
5. The use according to claim 2, wherein the diversion takes place laterally.
6. The use according to claim 2, wherein the diversion by 90° takes place.
7. The use according to claim 1 or 2, wherein the diversion by an angle deviating from 90° takes place.
8. The use according to claim 1 or 2, wherein the rotating cylinder is mounted in the center of the channel (10) behind the diversion point (10″).
9. The use according to claim 1 or 2, wherein the rotating cylinder (20) is asymmetrically mounted in the channel, in particular closer to the side of the travel direction.
10. The use according to claim 1 or 2, wherein the channel (10) is covered by a baffle plate (80) to reduce a fluid resistance formed during the propulsion before the diversion section, in particular above and spatially above or before the bend point (10″) of the channel (10, 10*).
11. The use according to claim 1 or 2 with only a single channel (10) with a rectangular cross-section.
12. The use according to claim 1 or 2 with several channels (10*) which have rectangular, elliptic or circular cross-sections.
13. The use according to claim 1 or 2, wherein the vehicle is a road or land vehicle, in particular a truck or an automobile.
14. The use according to claims 1 or 2, wherein the relatively rapid movement is less than 150 km/h, in particular describes the speed of the vehicle above the ground.
15. The use according to claims 1 or 2, wherein the relatively rapid movement is more than 10 km/h, in particular more than substantially 50 km/h, preferably in the range of between 60 km/h and 100 km/h.
16. The use according to claim 1 or 2, wherein the relatively rapid movement is a movement of more than 10 km/h, in a naval craft.
17. The use according to claim 1 or 2, wherein the vehicle is no aircraft.
18. A process according to any of claims 1 or 2, for the additional driving, in particular the driving of a vehicle, on which an additional drive system is mounted in addition to an independent main propulsion that is spaced from the additional drive.
19. The process according to claim 18, wherein a regular speed of the vehicle is between 50 km/h and 100 km/h, measured above ground.
20. The process according to claim 18, wherein the fluid flow is air and flows substantially from the front as a relative wind.
21. Additional drive system on the basis of the Magnus effect comprising a rotating, horizontally disposed cylinder (20) with end plates (17), characterized in that a fluid flow in a channel (10,10*), which is diverted in its direction, impinges on the rotor (20) in order to generate an additional propulsion (60) in a desired direction.
22. Additional drive system on the basis of the Magnus effect comprising a rotating, vertically disposed cylinder (20) with end plates (17), characterized in that a fluid flow in a channel, which is diverted in its direction, impinges on the rotor (20) in order to generate the propulsion (60) formed (in addition to a main propulsion) in a desired direction.
23. The use according to claim 13, wherein the relatively rapid movement is less than 150 km/h, in particular describes the speed of the vehicle above the ground.
24. The use according to claim 14, wherein the relatively rapid movement is more than 10 km/h, in particular more than substantially 50 km/h, preferably in the range of between 60 km/h and 100 km/h.
US10/598,157 2004-02-24 2005-02-23 Additional drive system by diverting a fluid flow Abandoned US20070160472A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP04004172.5 2004-02-24
EP04004172A EP1568602B1 (en) 2004-02-24 2004-02-24 Auxiliary propulsion unit using the deviation of a fluid stream
PCT/EP2005/050775 WO2005080195A1 (en) 2004-02-24 2005-02-23 Additional drive system by diverting a fluid flow

Publications (1)

Publication Number Publication Date
US20070160472A1 true US20070160472A1 (en) 2007-07-12

Family

ID=34745874

Family Applications (1)

Application Number Title Priority Date Filing Date
US10/598,157 Abandoned US20070160472A1 (en) 2004-02-24 2005-02-23 Additional drive system by diverting a fluid flow

Country Status (19)

Country Link
US (1) US20070160472A1 (en)
EP (2) EP1568602B1 (en)
JP (1) JP2007522997A (en)
CN (1) CN101087714A (en)
AT (1) ATE359208T1 (en)
AU (1) AU2005214092A1 (en)
BR (1) BRPI0507955A (en)
CA (1) CA2557365A1 (en)
CY (1) CY1106651T1 (en)
DE (1) DE502004003459D1 (en)
DK (1) DK1568602T3 (en)
ES (1) ES2285289T3 (en)
MX (1) MXPA06009726A (en)
NO (1) NO20064331L (en)
PT (1) PT1568602E (en)
RU (1) RU2006126240A (en)
SI (1) SI1568602T1 (en)
WO (1) WO2005080195A1 (en)
ZA (1) ZA200606822B (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101930683A (en) * 2010-09-07 2010-12-29 河海大学 Wind tunnel-free Magnus effect demonstrating experiment device
US7986054B2 (en) 2007-08-02 2011-07-26 Egen Llc Magnus force fluid flow energy harvester
EP2679807A1 (en) * 2012-06-26 2014-01-01 Wasilewski, Jerzy Boleslaw Vertical-axis wind turbine with Flettner rotors
US10118696B1 (en) 2016-03-31 2018-11-06 Steven M. Hoffberg Steerable rotating projectile
US11712637B1 (en) 2018-03-23 2023-08-01 Steven M. Hoffberg Steerable disk or ball

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011098605A1 (en) * 2010-02-15 2011-08-18 Winkler Joern Paul Vessel comprising a stowable magnus-effect rotor
EP2374681A1 (en) * 2010-04-12 2011-10-12 Herbert Gernert Device for vehicles and method for operating a vehicle
CN101898635B (en) * 2010-07-26 2013-03-27 哈尔滨工业大学 Duct single screw aircraft based on Magnus effect
DE102010040905A1 (en) * 2010-09-16 2012-03-22 Aloys Wobben ship
US10859065B1 (en) * 2019-12-12 2020-12-08 Li Li Supplemental propulsion system for vehicles

Citations (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2985406A (en) * 1959-04-29 1961-05-23 Bump Harold Wilson Aircraft sustained by cylindrical rotors
US3017848A (en) * 1960-11-14 1962-01-23 Charles R Bishop Boat propulsion unit
US3065928A (en) * 1960-07-16 1962-11-27 Dornier Werke Gmbh Multiple drive for aircraft having wings provided with transverse flow blowers
US3140065A (en) * 1962-06-27 1964-07-07 Alvarez-Calderon Alberto High lift and control system for aircraft
US3276415A (en) * 1961-12-12 1966-10-04 Firth Cleveland Ltd Device consisting of a drive and a rotating wheel producing thrust for the propulsion of boats
US3804548A (en) * 1970-10-14 1974-04-16 Buderus Eisenwerk Blower construction
US3940215A (en) * 1972-12-28 1976-02-24 Matsushita Electric Industrial Co., Ltd. Blower
US4048947A (en) * 1975-01-22 1977-09-20 Charles Andre Sicard Rotary device driven by a moving fluid
US4113299A (en) * 1976-10-04 1978-09-12 Johnson David W Rotating magnus tubes
US4116151A (en) * 1976-09-08 1978-09-26 John Guthrie Wind powered apparatus
US4132282A (en) * 1977-01-17 1979-01-02 Sparks Keith L Automotive electric generator
US4134469A (en) * 1976-10-08 1979-01-16 Turbopanel Motors, Inc. Linear turbine
US4168759A (en) * 1977-10-06 1979-09-25 Hull R Dell Automobile with wind driven generator
US4179007A (en) * 1978-06-01 1979-12-18 Howe Robert R Wind operated power generating apparatus
US4398895A (en) * 1981-05-14 1983-08-16 Asker Gunnar C F Wind propulsion devices
US4401284A (en) * 1980-03-20 1983-08-30 Austin Kenneth A Collapsible magnus-effect rotor
US4502724A (en) * 1980-10-16 1985-03-05 Grenadier R Miles Vehicle payload lightener
US4576581A (en) * 1981-11-30 1986-03-18 Borg John L Reversible Magnus propeller
US4582013A (en) * 1980-12-23 1986-04-15 The Holland Corporation Self-adjusting wind power machine
US4602584A (en) * 1984-06-12 1986-07-29 Henry North Propulsion device for a ship
US4630997A (en) * 1981-11-24 1986-12-23 Fondation Cousteau Apparatus for producing a force when in a moving fluid
US5280827A (en) * 1992-12-22 1994-01-25 Cletus L. Taylor Venturi effect charging system for automobile batteries
US5287004A (en) * 1992-09-04 1994-02-15 Finley Michael D Automobile air and ground effects power package
US5296746A (en) * 1992-12-17 1994-03-22 Burkhardt Harry E Extended range charging system for electrical vehicle
US5386146A (en) * 1993-04-22 1995-01-31 Hickey; John J. In-line auger driven charging system
US5875627A (en) * 1995-06-07 1999-03-02 Jeswine; William W. Fluid propulsion system for accelerating and directionally controlling a fluid
US6138781A (en) * 1997-08-13 2000-10-31 Hakala; James R. System for generating electricity in a vehicle
US6857492B1 (en) * 2003-01-09 2005-02-22 Airflow driven electrical generator for a moving vehicle
US6897575B1 (en) * 2003-04-16 2005-05-24 Xiaoying Yu Portable wind power apparatus for electric vehicles
US6910873B2 (en) * 2003-08-20 2005-06-28 Arthur Kaliski Self regulating rotor
US7135786B1 (en) * 2006-02-11 2006-11-14 Edward Deets Wind driven generator for powered vehicles
US7147069B2 (en) * 2002-05-08 2006-12-12 Maberry Robert L Wind turbine driven generator system for a motor vehicle
US7398841B2 (en) * 2004-05-17 2008-07-15 Jay Stephen Kaufman Vehicle power assist by brake, shock, solar, and wind energy recovery

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB371691A (en) * 1930-07-07 1932-04-28 Nicholas John Medvedeff Improvements in or relating to flying machines
GB494093A (en) * 1937-04-16 1938-10-17 Ivan Alexander Gavrilof Method and apparatus for controlling ships and like vessels
DE3123287C2 (en) * 1981-06-12 1986-06-05 Blohm + Voss Ag, 2000 Hamburg Wind propulsion for ships
GB2179014A (en) * 1985-07-19 1987-02-25 Thomas Macduff Improvements in propulsion systems
GB9111851D0 (en) * 1991-06-03 1991-07-24 Macduff Thomas A marine propulsion system

Patent Citations (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2985406A (en) * 1959-04-29 1961-05-23 Bump Harold Wilson Aircraft sustained by cylindrical rotors
US3065928A (en) * 1960-07-16 1962-11-27 Dornier Werke Gmbh Multiple drive for aircraft having wings provided with transverse flow blowers
US3017848A (en) * 1960-11-14 1962-01-23 Charles R Bishop Boat propulsion unit
US3276415A (en) * 1961-12-12 1966-10-04 Firth Cleveland Ltd Device consisting of a drive and a rotating wheel producing thrust for the propulsion of boats
US3140065A (en) * 1962-06-27 1964-07-07 Alvarez-Calderon Alberto High lift and control system for aircraft
US3804548A (en) * 1970-10-14 1974-04-16 Buderus Eisenwerk Blower construction
US3940215A (en) * 1972-12-28 1976-02-24 Matsushita Electric Industrial Co., Ltd. Blower
US4048947A (en) * 1975-01-22 1977-09-20 Charles Andre Sicard Rotary device driven by a moving fluid
US4116151A (en) * 1976-09-08 1978-09-26 John Guthrie Wind powered apparatus
US4113299A (en) * 1976-10-04 1978-09-12 Johnson David W Rotating magnus tubes
US4134469A (en) * 1976-10-08 1979-01-16 Turbopanel Motors, Inc. Linear turbine
US4132282A (en) * 1977-01-17 1979-01-02 Sparks Keith L Automotive electric generator
US4168759A (en) * 1977-10-06 1979-09-25 Hull R Dell Automobile with wind driven generator
US4179007A (en) * 1978-06-01 1979-12-18 Howe Robert R Wind operated power generating apparatus
US4401284A (en) * 1980-03-20 1983-08-30 Austin Kenneth A Collapsible magnus-effect rotor
US4502724A (en) * 1980-10-16 1985-03-05 Grenadier R Miles Vehicle payload lightener
US4582013A (en) * 1980-12-23 1986-04-15 The Holland Corporation Self-adjusting wind power machine
US4398895A (en) * 1981-05-14 1983-08-16 Asker Gunnar C F Wind propulsion devices
US4630997A (en) * 1981-11-24 1986-12-23 Fondation Cousteau Apparatus for producing a force when in a moving fluid
US4576581A (en) * 1981-11-30 1986-03-18 Borg John L Reversible Magnus propeller
US4602584A (en) * 1984-06-12 1986-07-29 Henry North Propulsion device for a ship
US5287004A (en) * 1992-09-04 1994-02-15 Finley Michael D Automobile air and ground effects power package
US5296746A (en) * 1992-12-17 1994-03-22 Burkhardt Harry E Extended range charging system for electrical vehicle
US5280827A (en) * 1992-12-22 1994-01-25 Cletus L. Taylor Venturi effect charging system for automobile batteries
US5386146A (en) * 1993-04-22 1995-01-31 Hickey; John J. In-line auger driven charging system
US5875627A (en) * 1995-06-07 1999-03-02 Jeswine; William W. Fluid propulsion system for accelerating and directionally controlling a fluid
US6138781A (en) * 1997-08-13 2000-10-31 Hakala; James R. System for generating electricity in a vehicle
US7147069B2 (en) * 2002-05-08 2006-12-12 Maberry Robert L Wind turbine driven generator system for a motor vehicle
US6857492B1 (en) * 2003-01-09 2005-02-22 Airflow driven electrical generator for a moving vehicle
US6897575B1 (en) * 2003-04-16 2005-05-24 Xiaoying Yu Portable wind power apparatus for electric vehicles
US6910873B2 (en) * 2003-08-20 2005-06-28 Arthur Kaliski Self regulating rotor
US7398841B2 (en) * 2004-05-17 2008-07-15 Jay Stephen Kaufman Vehicle power assist by brake, shock, solar, and wind energy recovery
US7135786B1 (en) * 2006-02-11 2006-11-14 Edward Deets Wind driven generator for powered vehicles

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7986054B2 (en) 2007-08-02 2011-07-26 Egen Llc Magnus force fluid flow energy harvester
CN101930683A (en) * 2010-09-07 2010-12-29 河海大学 Wind tunnel-free Magnus effect demonstrating experiment device
EP2679807A1 (en) * 2012-06-26 2014-01-01 Wasilewski, Jerzy Boleslaw Vertical-axis wind turbine with Flettner rotors
WO2014001358A1 (en) * 2012-06-26 2014-01-03 Wasilewski Jerzy Boleslaw Vertical -axis wind turbine with flettner rotors
US10184449B2 (en) 2012-06-26 2019-01-22 House Of Inventors Sp. Zo.O. Vertical-axis wind turbine with flettner rotors
US10118696B1 (en) 2016-03-31 2018-11-06 Steven M. Hoffberg Steerable rotating projectile
US11230375B1 (en) 2016-03-31 2022-01-25 Steven M. Hoffberg Steerable rotating projectile
US11712637B1 (en) 2018-03-23 2023-08-01 Steven M. Hoffberg Steerable disk or ball

Also Published As

Publication number Publication date
EP1568602B1 (en) 2007-04-11
RU2006126240A (en) 2008-03-27
ATE359208T1 (en) 2007-05-15
ES2285289T3 (en) 2007-11-16
WO2005080195A1 (en) 2005-09-01
ZA200606822B (en) 2007-12-27
CY1106651T1 (en) 2012-01-25
CN101087714A (en) 2007-12-12
PT1568602E (en) 2007-07-17
DK1568602T3 (en) 2007-08-20
CA2557365A1 (en) 2005-09-01
JP2007522997A (en) 2007-08-16
EP1718524A1 (en) 2006-11-08
BRPI0507955A (en) 2007-07-17
AU2005214092A1 (en) 2005-09-01
NO20064331L (en) 2006-09-25
SI1568602T1 (en) 2007-10-31
DE502004003459D1 (en) 2007-05-24
EP1568602A1 (en) 2005-08-31
MXPA06009726A (en) 2007-08-15

Similar Documents

Publication Publication Date Title
US20070160472A1 (en) Additional drive system by diverting a fluid flow
CN101195348B (en) Fluid motion device for accelerating and energy-saving
CN100447047C (en) Propulsion system for a fast seagoing ship, especially a naval ship
CN102164812A (en) Land vehicle provided with an internal air flow propulsion system
JPH026678B2 (en)
US20210122249A1 (en) Wind Based Electrical Generation System for Vehicles.
CN2771100Y (en) Hydrojet propeller
CN113291444A (en) Novel reverse sailing structure device of water sailing body
US20220048491A1 (en) Hovercraft having stealth function
CN101196203A (en) Composite device for accelerating movement body and energy-saving with fluid cavity
CN104494711B (en) Windage governor motion and the transporting equipment using the windage governor motion
CN211568224U (en) Self-made hull structure
CN201099288Y (en) Flow guiding structure capable of decelerating wind resistance
JP6031663B2 (en) Air resistance reduction device for automobiles
RU2163207C1 (en) Aero(hydro)dynamic device
CN216069507U (en) Full-floating amphibious vehicle
EA016742B1 (en) Transport system and a method for operating said system
JP5982458B2 (en) Ship structure
KR102542942B1 (en) Front active spoiler apparatus for vehicle
RU2729326C1 (en) Floating method of surface floating machine
US20060264126A1 (en) Jet drive for an amphibious vehicle
CN110641612A (en) Self-made hull structure
US20230339332A1 (en) Wind based electrical generation system for vehicles
NL1030011C2 (en) Bowscrew device with several outlet channels also comprise housing with several outlet channels cross ways to inlet channel, extending in different directions
RU2822072C1 (en) Air-cushion amphibious vehicle

Legal Events

Date Code Title Description
AS Assignment

Owner name: WOLFGANG JOBMANN GMBH, GERMANY

Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:JOBMANN, WOLFGANG;STAMME, PETER;REEL/FRAME:018873/0507

Effective date: 20061027

STCB Information on status: application discontinuation

Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION