GB2493241A - A vessel propulsion system with a driven oscillating blade means - Google Patents
A vessel propulsion system with a driven oscillating blade means Download PDFInfo
- Publication number
- GB2493241A GB2493241A GB1210089.7A GB201210089A GB2493241A GB 2493241 A GB2493241 A GB 2493241A GB 201210089 A GB201210089 A GB 201210089A GB 2493241 A GB2493241 A GB 2493241A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbulent
- text
- propulsor
- propulsor according
- blade
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H1/00—Propulsive elements directly acting on water
- B63H1/30—Propulsive elements directly acting on water of non-rotary type
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C33/00—Ornithopters
- B64C33/02—Wings; Actuating mechanisms therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H23/00—Transmitting power from propulsion power plant to propulsive elements
- B63H23/02—Transmitting power from propulsion power plant to propulsive elements with mechanical gearing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/003—Aircraft not otherwise provided for with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Transmission Devices (AREA)
Abstract
A propulsion system comprises a pushing blade 1, a steering unit, a transmission arrangement (Fig 7) and an engine (36, Fig 7). The transmission arrangement converts rotational movement from the engine into a figure eight motion in which the pushing blade is driven to propel a vessel 24 forward. The transmission arrangement may contain a longitudinal swinging mechanism (Fig.11), a transversal swinging mechanism (Fig.12) and a turning mechanism (Fig 10) which between them drive the pushing blade in the figure eight motion. The propulsion system may be used to drive both watercraft and aircraft.
Description
TURBULENT PROPULSOR
This invention relates to the propulsion system.
Most of the modern vessels are propelled by an engine and propeller. The rotating propeller throws the flow of water backward, pushing the vessel forward. Half of the engine's energy is converted into a backwards flow of water and only the second half of the engine's energy is converted into movement of the vessel.
It is well known, that when using this method of propulsion, it is impossible to significantly reduce power of the engine without losing the optimum performance of the vessel.
According to the present invention a mechanical transmission is provided which converts the rotational motion of the engine into the oscillatory -swivel motion of the blade. This motion creates turbulent vortices which resist the backwards movement of the blade, pushing the vessel forward.
A less powerful engine is required for the movement of the vessel with this type of propulsion system, as no energy is wasted On creating a sternward accelerated column of water.
On this type of vessel the circular variations of the directions of thrust provides effective steering control.
This type of propulsion can be used both for the watercraft and aircraft.
A specific embodiment of the invention will now be described by way of example with reference to the accompanying drawing in which: Fig.1 illustrates how turbulent vortices emerge when the blade is moving.
Fig.2 illustrates the trajectory and position of the blade during the motion.
For clarity, the trajectory is divided frito two parts.
Fig.3 shows a general view of the vessel and location of the blade.
Fig.4 shows the trajectory of the blade during the motion. For clarity, the trajectory is divided into two parts.
Fig.5 illustrates that the trajectory of the blade is a repeated side to side, turning and two back-and-forth motions.
Fig.6 illustrates the crank mechanism converting circular motion into rotary reciprocation motion.
Fig.7 shows the blade, engine and oscillating transmission assembly.
Fig.8 shows the internal mechanisms of oscillating transmission.
Fig.9 shows the perpendicular stack up of supporting brackets of the oscillation mechanisms which has freedom of swinging.
Fig. 10 shows the transformation mechanism of rotation into a turning motion of the blade.
Fig.1 1 shows the transformation mechanism of rotation into a back-and-forth motion of the blade.
Fig.12 shows the transformation mechanism of rotation into a side to side motion of the blade.
Fig. 13 shows the constant-velocity joint with a spring-loaded floating centering element.
Fig. 14 illustrates a possible upgrade option such as integration of the engine into the oscillation transmission, or replacement of the balljoint in order to increase the angle of oscillation of the blade.
Fig. 15 shows how the oscillation transmission converts rotational motion into an oscillation trajectory of the blade.
As shown in Fig.1, when the blade 1 is moving, with the wide side perpendicular to the direction of movement 2, the turbulent vortices 3 emerges on the opposite side of the blade. These vortices 3 provide resistance to the movement 2 of the blade.
During the movement 2 of the blade 1, on the edge of its trajectory, the blade is rotated parallel to the direction of thrust 4 and does not resist the movement of the vessel, as shown in Fig.2.
Going through the middle part of its trajectory, the blade is rotated perpendicular to the direction of its movement 2. The emerging turbulent vortices 3 provide resistance to the movement of the blade, pushing the vessel forward 4.
For every turn 9 of the blade around it vertical axis, there is one swing 10 from side to side and two swing 11 back and forth, as shown in Fig5.
For the basic principal of the oscillation transmission is the transformation of rotation motion 8 by the crank mechanism 7 with the connecting rod 6 into swinging motion 5. The crank mechanism is connected to the toothed rocking lever 14 which turns the toothed gear 12 in order to increase the angle of turning 9 of the blade as shown in Fig.6.
A general view of the vessel 24 with the propulsive blade I and the protective dome shell 35 is shown in Fig.3.
The rotation motion 8 of the engine 36 is transmitted to the oscillation transmission via spur gears 16. The cylindrical shape of the oscillation transmission housing body 17 is rotated by the steering mechanism 15 with worm gear 19 in order to control the direction of the movement of the vessel, as shown in Fig.7. The vessel hull 24 and protective dome shell 35 of the bellows 18 are represented in the cutaway view.
The key principal of the oscillation transmission is the perpendicular arrangement of supporting brackets of the longitudinal 20 and transverse 21 rocking mechanism which has freedom of swinging, as shown in Fig.9.
Both mechanisms of the oscillatory movements are connected by the shaft with spline and the double universal joint 22 which has only one point of the bend. The first universal joint 31 is connected to the second universal joint 32 with a spring-loaded 34 floating centering element 33, as shown in Fig.13.
The overall look and layout of mechanical components in the oscillation transmission is shown in Fig. 8. The cylindrical housing body 17 and hermetically sealed bellows 18 are represented in the cutaway view.
The rotation motion of the engine 8 is transmitted through the double universal joint 27 to the bevel gears 29. The crank mechanism 7 with connecting rod 6 converts the rotation motion into a swinging motion of the rocking housing body 28, and is responsible for the longitudinal movement 11 of the blade, asshown in Fig.11.
Then the same rotation motion 8 is transmitted through a double universal joint 22 to the bevel gears 25. The crank mechanism 7 with connecting rod 6 cornierts the rotation motion into swinging motion of the rocking housing body 30, and is responsible for the transversal movement 10 of the blade, as shown in Fig.12.
The same rotation motion 8 is transmitted through a double universal joint 22 to the spur gears 26. The crank mechanism 7 with connecting rod 6 is converting the rotation motion 8 into swinging motion of the toothed rocking lever 14, which turns the toothed gear 12. This gear is responsible for turning movement 9 of the blade I through the balljoint with hub 23, as shown in Fig.10.
The combination of these three movements determines the trajectory 2 of the blade 1, as shown in Fig.4.
Some possible upgrade options such as integration of the engine into the oscillation transmission, or replacement of the balljoint 23 in order to increase the angle of oscillation of the blade, as shown in Fig. I 4 Working moment when oscillation transmission tilting the blade is shown in Fig.15. The oscillation transmission housing body 17 is represented in the cutaway view.
The other transport, such an air propulsion vehicle, can be created when using different modifications of the oscillation transmission.
Claims (1)
- <claim-text>CLAIMS1 A turbulent propulsor is the generating thrust device, in which the rotational motion of the engine is converted through the transmission into a trajectory motion, which resembles figure eight, of the pushing blade, wherein the emerged turbulent vortices are resistant to the movement of the blade on the inner part of this trajectory, provides propulsive force.</claim-text> <claim-text>2 A turbulent propulsor according to claim 1, in which the trajectory motion of the pushing blade is created by synchronously operating the mechanism of longitudinal oscillation, the mechanism of transversal oscillation and the turning mechanism which swivels the pushing blade.</claim-text> <claim-text>3 A turbulent propulsor according to claim 2, in which the longitudinal and transversal mechanisms of oscillation are in a perpendicular arrangement on the freely oscillating bases.</claim-text> <claim-text>4 A turbulent propulsor according to claim 3, in which the steeiing is achieved by changing the circular directing of the propulsive force.</claim-text> <claim-text>S A turbulent propulsor according to claim 4, in which the engine is directly integrated into the oscillating transmission, as part of the oscillatory mechanism.</claim-text> <claim-text>6 A turbulent propulsor according to any of the preceding claims: in which the mechanisms of longitudinal and transverse oscillations are located side by side asa parallelogram or one above the other 7 A turbulent propulsor according to any of the preceding claims, in which the mechanisms of longitudinal and transversal oscillations are mechanically connected by a constant-velocity joint which has only one point of bending.8 A turbulent propulsor according to any of the preceding claims, in which the crank-connecting rod mechanism swivels the pushing blade, with large angle of deflection, about the central axis.9 A turbulent propulsor according to any of the preceding claims, in which the longitudinal and transversal mechanisms are the crank-connecting rod unit where the crankshaft is an oscillation element.A turbulent propulsor according to any of the preceding claims, in which the floating centering element of cOnstant-velocity joints move freely along the longitudinal and transversal supported attachments.11 A turbulent propulsor according to any of the preceding claims, in which the balljoint of the pushing blade is replaced on a mounting unit as a universal joint with a hub.12 A turbulent propulsor according to any of the preceding claims, in which the amplitude of oscillation of the pushing blade increases or decreases, when the distance changes between the oscillating mechanisms in the transmission.13 A turbulent propulsor according to any of the preceding claims, which can be used both for the watercraft and aircraft.14 A turbulent propulsor substantially as herein described and illustrated in the accompanying drawing.</claim-text>
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB1112832.9A GB201112832D0 (en) | 2011-07-26 | 2011-07-26 | Turbulent propulsor |
Publications (3)
Publication Number | Publication Date |
---|---|
GB201210089D0 GB201210089D0 (en) | 2012-07-25 |
GB2493241A true GB2493241A (en) | 2013-01-30 |
GB2493241B GB2493241B (en) | 2018-10-31 |
Family
ID=44652332
Family Applications (4)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GBGB1112832.9A Ceased GB201112832D0 (en) | 2011-07-26 | 2011-07-26 | Turbulent propulsor |
GBGB1204628.0A Ceased GB201204628D0 (en) | 2011-07-26 | 2012-03-16 | Turbulent propulsor |
GBGB1206346.7A Ceased GB201206346D0 (en) | 2011-07-26 | 2012-04-11 | Turbulent propulsor |
GB1210089.7A Expired - Fee Related GB2493241B (en) | 2011-07-26 | 2012-06-07 | Turbulent propulsor |
Family Applications Before (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GBGB1112832.9A Ceased GB201112832D0 (en) | 2011-07-26 | 2011-07-26 | Turbulent propulsor |
GBGB1204628.0A Ceased GB201204628D0 (en) | 2011-07-26 | 2012-03-16 | Turbulent propulsor |
GBGB1206346.7A Ceased GB201206346D0 (en) | 2011-07-26 | 2012-04-11 | Turbulent propulsor |
Country Status (1)
Country | Link |
---|---|
GB (4) | GB201112832D0 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20210309347A1 (en) * | 2020-04-01 | 2021-10-07 | Kwang Moo Lee | Propeller structure in the form of twin mobius blades for aircraft |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB191213128A (en) * | 1912-06-04 | 1913-09-04 | Allan Glenn | Improvements in and relating to the Propulsion of Vessels on and Immersed in Water. |
GB216898A (en) * | 1923-06-01 | 1925-08-31 | Technova Technische Industrie - Und Handels - Gesellschaft M.B.H. | |
AT398189B (en) * | 1993-04-05 | 1994-10-25 | Fraunschiel Josef | Wing flapping mechanism for driving aircraft or surface vessels |
-
2011
- 2011-07-26 GB GBGB1112832.9A patent/GB201112832D0/en not_active Ceased
-
2012
- 2012-03-16 GB GBGB1204628.0A patent/GB201204628D0/en not_active Ceased
- 2012-04-11 GB GBGB1206346.7A patent/GB201206346D0/en not_active Ceased
- 2012-06-07 GB GB1210089.7A patent/GB2493241B/en not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB191213128A (en) * | 1912-06-04 | 1913-09-04 | Allan Glenn | Improvements in and relating to the Propulsion of Vessels on and Immersed in Water. |
GB216898A (en) * | 1923-06-01 | 1925-08-31 | Technova Technische Industrie - Und Handels - Gesellschaft M.B.H. | |
AT398189B (en) * | 1993-04-05 | 1994-10-25 | Fraunschiel Josef | Wing flapping mechanism for driving aircraft or surface vessels |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20210309347A1 (en) * | 2020-04-01 | 2021-10-07 | Kwang Moo Lee | Propeller structure in the form of twin mobius blades for aircraft |
Also Published As
Publication number | Publication date |
---|---|
GB201112832D0 (en) | 2011-09-07 |
GB201206346D0 (en) | 2012-05-23 |
GB2493241B (en) | 2018-10-31 |
GB201204628D0 (en) | 2012-05-02 |
GB201210089D0 (en) | 2012-07-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20190607 |