US20150259058A1 - Shallow draft propeller nozzle - Google Patents
Shallow draft propeller nozzle Download PDFInfo
- Publication number
- US20150259058A1 US20150259058A1 US14/214,068 US201414214068A US2015259058A1 US 20150259058 A1 US20150259058 A1 US 20150259058A1 US 201414214068 A US201414214068 A US 201414214068A US 2015259058 A1 US2015259058 A1 US 2015259058A1
- Authority
- US
- United States
- Prior art keywords
- nozzle
- shroud
- propeller
- truncating
- ship
- 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
- 239000011888 foil Substances 0.000 claims abstract description 9
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 239000000446 fuel Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H5/00—Arrangements on vessels of propulsion elements directly acting on water
- B63H5/07—Arrangements on vessels of propulsion elements directly acting on water of propellers
- B63H5/14—Arrangements on vessels of propulsion elements directly acting on water of propellers characterised by being mounted in non-rotating ducts or rings, e.g. adjustable for steering purpose
- B63H5/15—Nozzles, e.g. Kort-type
Definitions
- the present invention relates to ship propulsion in general and in particular to a method and apparatus for permitting an increased ducted propeller size for a given draft.
- FIG. 1 an illustration of a conventional ducted propeller is shown generally at 10 in which the propeller 12 is rotated about a shaft 14 .
- the shroud or nozzle 16 surrounds the propeller to provide the aforementioned increase of thrust and efficiency, especially at low speeds.
- the nozzle or shroud which surrounds the propeller increases the overall diameter of the propeller assembly.
- the shroud may be substantially larger than the propeller itself so as to catch as much water as possible thereby directing this additional water to the propeller.
- ships fitted with such ducted propellers may have increased draft or may have the size of propellers that may be fitted thereto limited by the depth in which the ship is to operate. Such size of the propeller which may be used thereby limits the thrust that can be provided by the propulsion system for the ship.
- the new truncated nozzle alleviates this problem, by allowing to fit within the same draft limit a larger diameter shroud and propeller, which will produce higher thrust, or conversely, allow for less power and fuel consumption for the same thrust as conventional ducted propeller.
- a nozzle for a ship propeller having an axis of rotation.
- the nozzle comprises an annular shroud having a diameter and is adapted to surround the propeller.
- the shroud extends along the axis of the ship propeller and has inner and outer surfaces forming a foil.
- the outer surface of the shroud has a truncating surface extending along at least one of a top or bottom thereof.
- the truncating surface may be located on a bottom of the shroud.
- the truncating surface may be located a top of the shroud.
- the truncating surface may be substantially planar.
- the truncating surface may be substantially horizontal.
- the truncating surface may be convex having a radius of curvature of at least 10 times the diameter of the shroud.
- the truncating surface may be concave having a radius of curvature of at least 10 times the diameter of the shroud.
- the truncating surface may have a rounded edge with the outer surface of the shroud.
- an apparatus for propelling a ship comprising a screw propeller having an axis of rotation and a nozzle surrounding the screw propeller.
- the nozzle comprises an annular shroud having a diameter and is adapted to surround the propeller.
- the shroud extends along the axis of the ship propeller and has inner and outer surfaces forming a foil.
- the outer surface of the shroud has a truncating substantially horizontal surface extending along at least one of a top or bottom thereof.
- the screw propeller may be rotated by a shaft.
- the shaft may extend from a hull of the ship.
- the shroud may be supported by the hull.
- the shaft may extend from a pod suspended below the ship.
- the pod may be rotatable about a vertical or close to vertical axis.
- the shroud may be supported by the pod.
- FIG. 1 is a cross-sectional view of a conventional ducted propeller.
- FIG. 2 is a bottom perspective view of an apparatus for propelling a ship according to a first embodiment of the present invention.
- FIG. 3 is a partial cross sectional view of the nozzle of FIG. 2 .
- FIG. 4 is a side view of the propulsion system of FIG. 2 supported by a ship's hull.
- FIG. 5 is a side view of the propulsion system of FIG. 2 supported from a rotating pod.
- FIG. 6 is a detailed rear view of the nozzle of FIG. 2 having a concave truncating surface.
- FIG. 7 is a detailed rear view of the nozzle of FIG. 2 having a convex truncating surface.
- FIG. 8 is a detailed front view of a propulsion system according to a further embodiment of the present invention.
- an apparatus for propelling a ship is shown generally at 20 .
- the apparatus comprises a screw propeller 22 surrounded by a nozzle or shroud 30 .
- the propeller 22 may be of any known type and size as desired by a user for the required application.
- the propeller 22 is rotated and supported by a shaft 24 having an axis of rotation 26 .
- the nozzle 30 comprises an annular member extending between leading and trailing edges, 32 and 34 , respectively along an axis 26 of the propeller 22 .
- the nozzle is formed between inner and outer surfaces, 36 and 38 , respectively forming a foil shape therebetween. It will be appreciated that any foil profile may be utilized for the nozzle.
- the nozzle includes a truncating surface 40 extending across one or both of the top and bottom edges of the nozzle 30 .
- the truncating surface 40 is positioned to extend substantially horizontally across the nozzle.
- the truncating surface 40 may be spaced apart from the nominal diameter of the nozzle 30 by a setback distance 42 which may be selected to reduce the height of the nozzle as much as possible while still providing sufficient strength to the nozzle.
- the setback distance may be selected to be between 10 and 100 percent of the nozzle foil profile. As illustrated in FIGS.
- the truncating surface reduces the overall height of the nozzle 30 thereby correspondingly reducing the overall draft required for such a nozzle used with a propeller of a given size.
- the reduced height of the nozzle 30 will permit a larger diameter propeller to be utilized thereby providing greater thrust for a given input power to the propeller.
- the truncating surface 40 will slightly reduce the efficiency of the nozzle in the location of the truncating surface due to the disruption of the flow path over the foil profile.
- the larger nozzle possible for a given permitted draft will also provide an additional thrust exceeding the losses due to the disrupted flow over the truncating surface.
- the truncating surface 40 may be substantially planar although the truncating surface may also be curved as illustrated in FIGS. 6 and 7 .
- the truncating surface 40 may be concave as illustrated in FIG. 6 or convex as illustrated in FIG. 7 with a radius of curvature 44 .
- the radius of curvature is selected to reduce the thickness of the top and bottom of the nozzle 30 while preserving some of the foil profile and should therefore be selected to be large to provide as great a height reduction as possible.
- a radius of curvature of greater than 10 times the diameter of the nozzle has been useful.
- the nozzle 30 may be suspended from and supported by the hull 8 of a ship wherein the propeller 22 is located therein at the end of a propeller shaft 24 .
- the truncating surface 40 may be located at the bottom of the nozzle so as to present a substantially flat surface parallel to a bottom of the ocean, lake, river or the like.
- the top of the nozzle 30 may also include a truncating surface facilitating engagement with the hull 8 and permitting the nozzle and propeller to be located closer thereto.
- FIG. 4 the top of the nozzle 30 may also include a truncating surface facilitating engagement with the hull 8 and permitting the nozzle and propeller to be located closer thereto.
- the nozzle and propeller may be supported by a rotatable pod 50 , such as by way of non-limiting example an azimuth thruster.
- the pod 50 may be suspended from the hull 8 by a rotating member 52 which is rotatable about a vertical axis 54 with respect to the hull as are commonly known.
- the nozzle 30 may include either or both of a truncating surface at the top or bottom thereof.
- the truncating surface 40 may extend across the top or bottom of the nozzle 30 at an angle relative to horizontal indicated generally at 60 . Such an angle will facilitate matching a top truncating surface to the angle of the hull at that location. It will be appreciated that this will be useful in locating the truncating surface and thereby the nozzle as close to the hull as possible.
- the truncating surface may be flared outwardly from the nozzle to prevent debris, for example ice, from jamming between the nozzle and the hull.
- the truncating surface and the outer surface 38 of the nozzle 30 may also have a curved surface 62 having a radius generally indicated at 64 . The radius may be selected to be between 5 and 15% of the nozzle outer diameter.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Toys (AREA)
Abstract
A nozzle for a ship propeller having an axis of rotation comprises an annular shroud having a diameter and is adapted to surround the propeller. The shroud extends along the axis of the ship propeller and has inner and outer surfaces forming a foil. The outer surface of the shroud has a truncating surface extending along at least one of a top or bottom thereof.
Description
- 1. Field of Invention
- The present invention relates to ship propulsion in general and in particular to a method and apparatus for permitting an increased ducted propeller size for a given draft.
- 2. Description of Related Art
- Many ships are propelled by propellers having airfoil shaped blades. Such propellers are typically rotated about an axis of a shaft to create thrust against the surrounding water. Many attempts have been made to increase the efficiency of such propellers and to increase their thrust for a given required input power from a motor or engine. One such attempt has been to provide a shroud or nozzle around the propeller as is commonly known as a ducted propeller or Kort nozzle.
- As illustrated in
FIG. 1 , an illustration of a conventional ducted propeller is shown generally at 10 in which thepropeller 12 is rotated about ashaft 14. The shroud ornozzle 16 surrounds the propeller to provide the aforementioned increase of thrust and efficiency, especially at low speeds. - One difficulty with conventional ducted propellers is that the nozzle or shroud which surrounds the propeller increases the overall diameter of the propeller assembly. In the case of conventional or Kort Nozzle, the shroud may be substantially larger than the propeller itself so as to catch as much water as possible thereby directing this additional water to the propeller. Accordingly ships fitted with such ducted propellers may have increased draft or may have the size of propellers that may be fitted thereto limited by the depth in which the ship is to operate. Such size of the propeller which may be used thereby limits the thrust that can be provided by the propulsion system for the ship.
- The new truncated nozzle alleviates this problem, by allowing to fit within the same draft limit a larger diameter shroud and propeller, which will produce higher thrust, or conversely, allow for less power and fuel consumption for the same thrust as conventional ducted propeller.
- According to a first embodiment of the present invention there is disclosed a nozzle for a ship propeller having an axis of rotation. The nozzle comprises an annular shroud having a diameter and is adapted to surround the propeller. The shroud extends along the axis of the ship propeller and has inner and outer surfaces forming a foil. The outer surface of the shroud has a truncating surface extending along at least one of a top or bottom thereof.
- The truncating surface may be located on a bottom of the shroud. The truncating surface may be located a top of the shroud.
- The truncating surface may be substantially planar. The truncating surface may be substantially horizontal. The truncating surface may be convex having a radius of curvature of at least 10 times the diameter of the shroud. The truncating surface may be concave having a radius of curvature of at least 10 times the diameter of the shroud. The truncating surface may have a rounded edge with the outer surface of the shroud.
- According to a further embodiment of the present invention there is disclosed an apparatus for propelling a ship comprising a screw propeller having an axis of rotation and a nozzle surrounding the screw propeller. The nozzle comprises an annular shroud having a diameter and is adapted to surround the propeller. The shroud extends along the axis of the ship propeller and has inner and outer surfaces forming a foil. The outer surface of the shroud has a truncating substantially horizontal surface extending along at least one of a top or bottom thereof.
- The screw propeller may be rotated by a shaft. The shaft may extend from a hull of the ship. The shroud may be supported by the hull.
- The shaft may extend from a pod suspended below the ship. The pod may be rotatable about a vertical or close to vertical axis. The shroud may be supported by the pod.
- Other aspects and features of the present invention will become apparent to those ordinarily skilled in the art upon review of the following description of specific embodiments of the invention in conjunction with the accompanying figures.
- In drawings which illustrate embodiments of the invention wherein similar characters of reference denote corresponding parts in each view,
-
FIG. 1 is a cross-sectional view of a conventional ducted propeller. -
FIG. 2 is a bottom perspective view of an apparatus for propelling a ship according to a first embodiment of the present invention. -
FIG. 3 is a partial cross sectional view of the nozzle ofFIG. 2 . -
FIG. 4 is a side view of the propulsion system ofFIG. 2 supported by a ship's hull. -
FIG. 5 is a side view of the propulsion system ofFIG. 2 supported from a rotating pod. -
FIG. 6 is a detailed rear view of the nozzle ofFIG. 2 having a concave truncating surface. -
FIG. 7 is a detailed rear view of the nozzle ofFIG. 2 having a convex truncating surface. -
FIG. 8 is a detailed front view of a propulsion system according to a further embodiment of the present invention. - Referring to
FIG. 2 , an apparatus for propelling a ship according to a first embodiment of the invention is shown generally at 20. The apparatus comprises ascrew propeller 22 surrounded by a nozzle orshroud 30. Thepropeller 22 may be of any known type and size as desired by a user for the required application. Thepropeller 22 is rotated and supported by ashaft 24 having an axis ofrotation 26. - The
nozzle 30 comprises an annular member extending between leading and trailing edges, 32 and 34, respectively along anaxis 26 of thepropeller 22. The nozzle is formed between inner and outer surfaces, 36 and 38, respectively forming a foil shape therebetween. It will be appreciated that any foil profile may be utilized for the nozzle. - With reference to
FIGS. 2 and 3 , the nozzle includes atruncating surface 40 extending across one or both of the top and bottom edges of thenozzle 30. The truncatingsurface 40 is positioned to extend substantially horizontally across the nozzle. The truncatingsurface 40 may be spaced apart from the nominal diameter of thenozzle 30 by asetback distance 42 which may be selected to reduce the height of the nozzle as much as possible while still providing sufficient strength to the nozzle. By way of non-limiting example, the setback distance may be selected to be between 10 and 100 percent of the nozzle foil profile. As illustrated inFIGS. 2 and 3 , it will be appreciated that the truncating surface reduces the overall height of thenozzle 30 thereby correspondingly reducing the overall draft required for such a nozzle used with a propeller of a given size. Similarly, it will be appreciated that the reduced height of thenozzle 30 will permit a larger diameter propeller to be utilized thereby providing greater thrust for a given input power to the propeller. It will be appreciated that thetruncating surface 40 will slightly reduce the efficiency of the nozzle in the location of the truncating surface due to the disruption of the flow path over the foil profile. However it will also be appreciated that the larger nozzle possible for a given permitted draft will also provide an additional thrust exceeding the losses due to the disrupted flow over the truncating surface. - With reference to
FIGS. 2 and 3 , in a preferred embodiment, the truncatingsurface 40 may be substantially planar although the truncating surface may also be curved as illustrated inFIGS. 6 and 7 . In particular the truncatingsurface 40 may be concave as illustrated inFIG. 6 or convex as illustrated inFIG. 7 with a radius ofcurvature 44. The radius of curvature is selected to reduce the thickness of the top and bottom of thenozzle 30 while preserving some of the foil profile and should therefore be selected to be large to provide as great a height reduction as possible. In particular, it has been found that a radius of curvature of greater than 10 times the diameter of the nozzle has been useful. - With reference to
FIG. 4 , thenozzle 30 may be suspended from and supported by thehull 8 of a ship wherein thepropeller 22 is located therein at the end of apropeller shaft 24. In such embodiments, the truncatingsurface 40 may be located at the bottom of the nozzle so as to present a substantially flat surface parallel to a bottom of the ocean, lake, river or the like. It will also be appreciated that in such embodiments, the top of thenozzle 30 may also include a truncating surface facilitating engagement with thehull 8 and permitting the nozzle and propeller to be located closer thereto. Optionally, as illustrated inFIG. 5 , the nozzle and propeller may be supported by arotatable pod 50, such as by way of non-limiting example an azimuth thruster. In such embodiments, thepod 50 may be suspended from thehull 8 by a rotatingmember 52 which is rotatable about avertical axis 54 with respect to the hull as are commonly known. Similar to as set out above, for such embodiments, thenozzle 30 may include either or both of a truncating surface at the top or bottom thereof. - With reference to
FIG. 8 , according to a further embodiment the truncatingsurface 40 may extend across the top or bottom of thenozzle 30 at an angle relative to horizontal indicated generally at 60. Such an angle will facilitate matching a top truncating surface to the angle of the hull at that location. It will be appreciated that this will be useful in locating the truncating surface and thereby the nozzle as close to the hull as possible. Optionally, as illustrated inFIG. 8 , the truncating surface may be flared outwardly from the nozzle to prevent debris, for example ice, from jamming between the nozzle and the hull. As illustrated inFIG. 8 , the truncating surface and theouter surface 38 of thenozzle 30 may also have acurved surface 62 having a radius generally indicated at 64. The radius may be selected to be between 5 and 15% of the nozzle outer diameter. - While specific embodiments of the invention have been described and illustrated, such embodiments should be considered illustrative of the invention only and not as limiting the invention as construed in accordance with the accompanying claims.
Claims (15)
1. A nozzle for a ship propeller having an axis of rotation, the nozzle comprising an annular shroud having a diameter and being adapted to surround said propeller, said shroud extending along said axis of the ship propeller and having inner and outer surfaces forming a foil, wherein said outer surface of said shroud has a truncating surface extending along at least one of a top or bottom thereof.
2. The nozzle of claim 1 wherein said truncating surface is located on a bottom of said shroud.
3. The nozzle of claim 1 wherein said truncating surface is located a top of said shroud.
4. The nozzle of claim 1 wherein said truncating surface is substantially planar.
5. The nozzle of claim 1 wherein said truncating surface is substantially horizontal.
6. The nozzle of claim 1 wherein said truncating surface is convex having a radius of curvature of at least 10 times said diameter of said shroud.
7. The nozzle of claim 1 wherein said truncating surface is concave having a radius of curvature of at least 10 times said diameter of said shroud.
8. The nozzle of claim 1 wherein said truncating surface has a rounded edge with said outer surface of said shroud.
9. An apparatus for propelling a ship comprising a screw propeller having an axis of rotation and the nozzle of claim 1 surrounding said screw propeller.
10. The apparatus of claim 9 wherein said screw propeller is rotated by a shaft.
11. The apparatus of claim 10 wherein said shaft extends from a hull of said ship.
12. The apparatus of claim 10 wherein said shaft extends from a pod suspended below said ship.
13. The apparatus of claim 12 wherein said pod is rotatable about an axis.
14. The apparatus of claim 12 wherein said shroud is supported by said pod.
15. The apparatus of claim 9 wherein said shroud is supported by said hull.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US14/214,068 US20150259058A1 (en) | 2014-03-14 | 2014-03-14 | Shallow draft propeller nozzle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US14/214,068 US20150259058A1 (en) | 2014-03-14 | 2014-03-14 | Shallow draft propeller nozzle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20150259058A1 true US20150259058A1 (en) | 2015-09-17 |
Family
ID=54068120
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US14/214,068 Abandoned US20150259058A1 (en) | 2014-03-14 | 2014-03-14 | Shallow draft propeller nozzle |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US20150259058A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117068355A (en) * | 2023-07-31 | 2023-11-17 | 深圳市中天海洋科技有限公司 | Boosting structure of underwater booster |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3457891A (en) * | 1968-08-30 | 1969-07-29 | Hydroconic Ltd | Propulsive systems for vessels |
| US4637801A (en) * | 1984-07-12 | 1987-01-20 | William H. Flood | Thrust enhancing propeller duct assembly for water craft |
| US5389020A (en) * | 1993-02-02 | 1995-02-14 | Clark; James D. | Marine prop housing |
-
2014
- 2014-03-14 US US14/214,068 patent/US20150259058A1/en not_active Abandoned
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3457891A (en) * | 1968-08-30 | 1969-07-29 | Hydroconic Ltd | Propulsive systems for vessels |
| US4637801A (en) * | 1984-07-12 | 1987-01-20 | William H. Flood | Thrust enhancing propeller duct assembly for water craft |
| US5389020A (en) * | 1993-02-02 | 1995-02-14 | Clark; James D. | Marine prop housing |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN117068355A (en) * | 2023-07-31 | 2023-11-17 | 深圳市中天海洋科技有限公司 | Boosting structure of underwater booster |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105829202B (en) | For the ice breaker preferably operated in shallow icing water | |
| US4427393A (en) | Propulsion of ships | |
| EP2338783A1 (en) | Twin skeg ship | |
| EP3150482A1 (en) | Combined propeller cap for reducing rotating flow and hub vortex and enhancing propulsion efficiency | |
| US7452253B2 (en) | Propulsion system of marine vessel | |
| US10040528B2 (en) | Propulsion device for ship | |
| CN103097238B (en) | marine vessel with propulsion unit | |
| US7025642B1 (en) | Boat propeller | |
| US9926059B2 (en) | Ship propulsion arrangement | |
| CA2846137C (en) | Shallow draft propeller nozzle | |
| SE544385C2 (en) | Propeller combination for a marine vessel | |
| KR20140038217A (en) | Propeller system for vessel | |
| US20150259058A1 (en) | Shallow draft propeller nozzle | |
| US9376186B2 (en) | Marine tunnel thruster | |
| CN107539445B (en) | Rudder for ship | |
| US20140273673A1 (en) | All-speed-range propeller having stern fins | |
| WO2011102103A1 (en) | Thruster with duct attached and vessel comprising same | |
| KR200480863Y1 (en) | Propeller for Ship | |
| KR20140131767A (en) | A rudder for a ship | |
| KR102209082B1 (en) | A propulsion apparatus for ship | |
| US10569851B1 (en) | Dual blade assembly propeller | |
| US20150266554A1 (en) | Tractor Mode Marine Propulsion | |
| KR101589124B1 (en) | Propulsion apparatus of vessel | |
| JP2014169017A (en) | Propeller | |
| RU2600958C1 (en) | Screw propeller |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: COLUMBIA INSURANCE COMPANY, NEBRASKA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:SHAW INDUSTRIES GROUP, INC.;REEL/FRAME:034170/0587 Effective date: 20141029 |
|
| AS | Assignment |
Owner name: NAVIFORM CONSULTING & RESEARCH LTD., CANADA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:VAN DIEPEN, PETER;REEL/FRAME:035837/0349 Effective date: 20140313 |
|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |