WO1993009026A1 - An elastomeric propeller having a flexible elastomeric covering - Google Patents
An elastomeric propeller having a flexible elastomeric covering Download PDFInfo
- Publication number
- WO1993009026A1 WO1993009026A1 PCT/DK1992/000312 DK9200312W WO9309026A1 WO 1993009026 A1 WO1993009026 A1 WO 1993009026A1 DK 9200312 W DK9200312 W DK 9200312W WO 9309026 A1 WO9309026 A1 WO 9309026A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- propeller
- blade
- blades
- elastomer
- propeller according
- Prior art date
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
- B63H1/02—Propulsive elements directly acting on water of rotary type
- B63H1/12—Propulsive elements directly acting on water of rotary type with rotation axis substantially in propulsive direction
- B63H1/14—Propellers
- B63H1/26—Blades
Definitions
- the invention concerns a propeller for e.g. a ship and . 5 having a central hub with a plurality of propeller blades.
- Propellers for e.g. ships are extensively moulded either integrally or with hub and blades separately of metals, such as aluminium alloys, bronze and steel. After moulding
- the propeller can no longer work in a quiet and well- balanced manner, but will instead run untrue and transmit shakings and vibrations into the hull.
- Some of the em ⁇ ployed metals are moreover not particularly corrosion resistant to sea water. This applies e.g. to the aluminium
- US Patent 2 473 665 describes a propeller which, within certain limits, is capable of withstanding shocks and im ⁇ pacts from objects which the propeller might strike in the water during rotation.
- the blades of this propeller con- sist of rubber which merely yields elastically if the blade is struck, and immediately again assumes the origi ⁇ nal shape.
- the blades are reinforced with some wires. However, this reinforcement is not sufficient to absorb the loads that occur in operation of the great majority of ships, and the reinforcement type cannot be used either for selectively controlling the deformation of the blades in response to the load.
- the object of the invention is to provide a propeller of the type mentioned in the opening paragraph which can be moulded to finished size with a smooth and even surface that does not require expensive after-treatment.
- Another object of the invention is to provide a propeller of the type mentioned in the opening paragraph which per se is capable of reducing the propeller noise and absorb ⁇ ing and damping shock pulses from the reaction forces of the water, and which can moreover withstand shocks and impacts from objects in the water or on the bottom to a considerable extent without being permanently deformed.
- a third object of the invention is to provide a propeller of the type mentioned in the opening paragraph which is corrosion resistant to e.g. sea water.
- a fourth object of the invention is to provide a propeller of the type mentioned in the opening paragraph which, by simple means, can safely and effectively adjust the pitch of the blades optimally to any state of operation in re ⁇ sponse to the instantaneous load on the propeller.
- a fifth object of the invention is to provide a propeller of the type mentioned in the opening paragraph which, by simple means, can be rapidly and easily adapted to various applications optimally and be adjusted if the blades should have changed their shape or have lost their ba ⁇ lance.
- the blades are composed of a flexible elastomer having a core which extends from the hub over a considerable portion of the area of each blade and consists of a material having a greater coefficient of elasticity than the elastomer, e.g. fibre reinforced plas- tics or metal.
- This core is capable of imparting the ne ⁇ cessary strength and stability to the blades, while the elastomer serves to flexibly control the pitch of the blades in response to the load and to dampen shock pulses as well as to absorb impacts without permanent deforma- tions.
- the propeller obtains a consider ⁇ able corrosion resistance to e.g. sea water and a smooth surface already during the moulding which does not require any form of after-treatment.
- the elastomer may advantageously be a natural or synthetic rubber which is vulcanized firmly on the core so as to provide an intimate and long-lasting connection between the core and the rubber.
- the rubber may moreover be reinforced with fibres and/or a carcass of e.g. canvas, and the core may moreover be perforated so as to provide a direct bond via the per ⁇ forated holes between the rubber layers on both sides of the core.
- the rubber may also be composed of several layers, and when the outermost one of these consists of very soft rubber, the propeller obtains particularly good impact and shock absorbing properties.
- the vulcaniza ⁇ tion or the joints between the core and the rubber and the optional rubber layers, respectively are mutually inter ⁇ rupted by zones without joints, so that these joint-free zones may have the form of sections which are mutually se ⁇ parated by joints or by e.g. a string extending along the leading edge of the blade and having side ribs which sub ⁇ stantially extend in the same direction as the current along the blade in operation.
- a fluid such as air or water
- a fluid can be pressed via one or more fill ⁇ ing valves inwardly between the surfaces in the joint-free zones, thereby providing fluid-filled compartments at these locations which cooperate with the flexible elasto ⁇ mer at the changes in form which the blade undergoes in response to the instantaneous state of load.
- the compartments may be connected individually or groupwise with their respective filling valves, so that the shape of the blade can be changed partially, i.e. in the area in which the respective compartments are located.
- the elastomer covering is composed of e.g. two layers of rubber
- the fluid compart ⁇ ments in one blade is fluid-connected with the correspond ⁇ ing fluid compartment in the other blades, since the blades hereby automatically obtain the same outer geome- trical shape.
- the fluid connections may e.g. extend through channels in the hub.
- the applicant's Danish patent application No. 1392/91, "a folding propeller having at least three blades" and No. 1393/91 "a folding propeller having at least two blades”, both of which are incorporated in the present patent application by reference, describe pivotal propeller blades provided with a rubber covering on the innermost end portion which carries the engagement means for syn ⁇ chronization of the pivotal movements of the blades.
- this rubber covering may ad- vantageously be integral with the flexible elastomer of the rest of the blade, so that fluid compartments may also be provided in the innermost end portion of the blade for controlling the shape of the engagement means at this lo ⁇ cation and their pressure against the engagement means of the other blades.
- fig. 1 is a partially sectional end view of a fraction of a first embodiment of a propeller according to the inven ⁇ tion,
- fig. 2 shows a section along the line II-II in fig. 1,
- figs. 3a-3e show a cross-section through a propeller blade seen in various situations of operation
- figs. 4a-4c show a cross-section through various embodi ⁇ ments of a propeller blade for a propeller during forward rotation
- fig. 5 is a partially sectional end view of a fraction of a second embodiment of a propeller according to the inven ⁇ tion, fig. 6 shows a section along the line VI-VI in fig. 1,
- fig. 7 is a partially sectional end view of a fraction of a third embodiment of a propeller according to the inven- tion,
- fig. 8 shows a section along the line VIII-VIII in fig. 7,
- fig. 9 is a partially sectional end view of a fraction of a fourth embodiment of a propeller according to the inven ⁇ tion,
- fig. 10 shows a section along the line X-X in fig. 9,
- fig. 11 is a partially sectional end view of a folding propeller blade according to the invention.
- fig. 12 shows a section along the line XII-XII in fig. 11,
- fig. 13 is a partially sectional end view of a fraction of a fifth embodiment of a propeller according to the inven ⁇ tion,
- fig. 14 shows a section along the line XIV-XIV in fig. 13,
- fig. 15 shows a section along the line XV-XV in fig. 13, and
- fig. 16 schematically shows the self-adjusting fluid con- nections between identical fluid compartments in propeller blades having two elastomer layers.
- Figs. 1-2 show a typical structure of an elastomer pro ⁇ peller according to the invention for a ship.
- the propeller which is generally designated 1
- the propeller has three propeller blades 3 which are firmly arranged on a hub 2 for the mounting of the propeller on the drive shaft of the ship.
- the blades are composed of a core 4 and a flex ⁇ ible rubber covering 5, which is fixedly adhered or vulca ⁇ nized on the core.
- the blades are screw-shaped with a radially outwardly decreasing pitch, as appears from fig. 2, which moreover shows that the blades have an airfoil profile.
- the core 4 is made of e.g. metal of fibre reinforced plastics having a sufficient strength to impart the required rigidity to the blades 3.
- the core is perforated with holes 7 through which a bond is achieved between the rubber coverings on both sides of the core, and the blade will hereby be better capable of permanently withstanding the quickly varying changes in form which the blade under ⁇ goes in operation.
- Figs. 3a-e show various situations of operation for a pro ⁇ peller blade having a flexible rubber covering 8 which is vulcanized on a firm core 9.
- the arrows at the blade illu ⁇ strate the pressure or negative pressure which occurs when the blade moves through the water at various speeds. These speeds and their orientation are moreover illustrated by the arrows to the right of the profiles.
- the propeller stands still, and its blades are solely loaded by the static pressure of the water.
- the pro ⁇ peller has now begun to rotate, thereby generating a posi- tive pressure on the top side of the blade and a negative pressure on its underside.
- the pressure load on the rubber covering has changed its direction, as shown, but is still so small that it has not been able to deform the rubber covering significantly.
- the propeller rotates full speed astern, so that the rubber covering is compressed on the underside of the blade and expands on the top side of the blade.
- the flexible trailing edge of the blade is simul ⁇ taneously turned on the top side to form a profile which, seen in relation to the direction of rotation, has a rounded leading edge which is hydrodynamically more suit ⁇ able for penetrating through the water than a sharp edge.
- the propeller blades can be arranged in this manner to work with optimum efficiency within a much greater range of operation than is the case with the known propellers.
- Figs. 5 and 6 show a second embodiment of a propeller 10 according to the invention.
- the propeller has three blades 12 which are secured on a hub 11.
- the rubber covering is only vul- canized firmly on the core 13 along a narrow rim area which is provided with holes 15 to effectively ensure attachment of the covering to the core.
- the rest of the core is not connected with the rubber covering, thereby forming a joint-free area or compartment which is con- nected via a channel 17 with a filling valve 18 at the side of the hub 11.
- the compartment 16 can now be filled with air or liquid as desired for affecting the flexible properties of the blade in coaction with the rubber cover ⁇ ing, such that the shape of the blade changes optimally in response to the instantaneous load.
- Figs. 4a-c illustrate the advantages which can be obtained in this manner by means of a fluid filling in the blade over a blade with a rubber covering vulcanized firmly on the core along its overall surface.
- the latter case is shown in fig. 4a, in which a solid, soft rubber covering 20 is vulcanized firmly on a core 21 to the full extent.
- the blade changes its shape as desired in re ⁇ sponse to the instantaneous load, as described before with reference to figs. 3a-e.
- the change in shape that can be achieved in this manner is limited, since the elastic deformation ability of the rubber only permits relatively small changes in the thickness of the rubber coverings.
- the rubber covering 20 is now no longer vulcanized firmly on the core 21 along its overall surface. Therefore, in operation the pressure load will make the rubber covering lift from the core on one or the other side thereof to form air compartments 22.
- the rubber covering can now move considerably more outwardly with respect to the core than in the structure with fully vulcanized rubber shown in fig. 4a.
- the structure shown in fig. 4b it will be ex ⁇ pedient to provide the core with through holes 23 for con ⁇ sistently conveying the air from the pressure side to the negative pressure side to ensure that the rubber covering optimally changes its shape as desired in response to the load.
- the compartment 22 is now filled with li ⁇ quid, e.g. water, instead.
- the fluid compartment does not have to be a single large compartment like in the embodiment shown in figs. 5 and 6, but may also have a more complicated form according to the purpose, where zones with vulcanization between the rubber covering and the core alternate with vulcanization-free zones.
- An example of such a structure is sho n in figs. 7 and 8, which show a propeller having three blades 25 on a hub 26.
- the liquid compart ⁇ ment in this case consists of a string 28 extending along the leading edge of the blade and a plurality of ribs 29 which emanate from the string 28 and extend toward the trailing edge of the blade in the same direction as the water substantially flows over the blade when the propel ⁇ ler works.
- the hub accommodates a filling valve 32 which is connected with the string 28 and serves to fill the compartment 28, 29 with a fluid, such as air or water under pressure.
- the rubber covering 30 is vulca ⁇ nized firmly on the surface of the core 31 at short inter- vals, which gives the propeller blade a considerably more stable shape than in the embodiment shown in figs. 5 and 6 with just a single large compartment.
- Figs. 9 and 10 likewise show a propeller having three blades 33, a hub 34, a core 25 and a rubber covering 36.
- the blade 33 has three separate fluid compartments 37, 38 and 39, each having its own filling valve 40, 41 and 42, respectively.
- the advantage of this arrangement is that the compartments can be pumped independently of each other, so that one and the same pro ⁇ peller can be given a shape which is suited for various purposes. It is noted in this context that the number and the arrangement of the compartments in the structure shown in figs. 9 and 10 are just given by way of example, and that the numbers and the shapes of the compartments can be adapted in any expedient manner as required.
- the propeller blades on the propel- lers described in the applicant's Danish patent applica ⁇ tions No. 1392/91 and No. 1393/91 are provided with a rub ⁇ ber covering on the innermost end part of the blades which is located in the hub and carries the engagement means for synchronization of the pivotal movements of the blades.
- Figs. 11 and 12 show such a folding propeller blade which is generally designated 43.
- the innermost end part 44 of the blade is provided with a rubber covering 45 which is vulcanized firmly on the core 52 integrally with the rub ⁇ ber covering 46 on the actual blade.
- the blade like in the embodiment shown in figs. 5 and 6, includes a single large fluid compartment 47, which is filled with e.g.
- the compartment 47 com ⁇ municates via a fluid channel 50 with a filling valve 49 arranged at the end of the swing axle 48 of the blade.
- a filling valve 49 arranged at the end of the swing axle 48 of the blade.
- the rubber covering 45 on the end part 44 of the blade is solid, but it is readily possible also to provide fluid compartments in the rubber covering 45 so that the engagement means on it can be adjusted by pumping when worn.
- the fluid compartment can be pro ⁇ vided in any other manner, e.g. as shown in figs. 7, 8 and 9, 10.
- the inner layer 57 and the core 56 define between them a single inner fluid compartment 56 extending over most of the area of the core, and the outer layer 58 and the inner layer 57 define between them an outer fluid compartment 60 which likewise extends over most of the area of the core. How ⁇ ever, both compartments may be adapted in any other suit ⁇ able manner, e.g. like in the embodiments shown in figs. 7, 8 and figs. 9, 10, respectively.
- the inner fluid com- partments 59 in each blade are interconnected via an inner annular groove 51 in the hub 55, and the outer fluid com ⁇ partments 60 are correspondingly interconnected via an outer annular groove 62 in the hub 55.
- the hub moreover includes a valve 53 for filling the inner fluid compart- ments 59 and a valve 64 for filling the outer fluid com ⁇ partments 60.
- the inner fluid compartments in the three blades are in fluid communication with each other and are pumped at the same time via the same filling valve.
- the principle of this structure is shown schematically in fig. 16, which symbolically illustrates the three blades A, B and C with inner fluid compartments 65a, b, c and outer fluid compartments 66a, b, c.
- the inner fluid com- partments are interconnected with fluid conduits 68 in which a filling valve 70 is provided, and the outer fluid compartments are interconnected with fluid conduits 67 in which a filling valve 69 is provided.
- Elastomeric mate ⁇ rials such as rubber, have anisotropic properties to a certain extent and therefore tend to stretch disuniformly when loaded. Since the inner fluid compartments are inter ⁇ connected, the pressure in them will always be the same, but since the inner rubber layer does not stretch comple ⁇ tely uniformly in the three compartments owing to the ani- sotropic properties of the material, the first compartment 65a is larger than the two other compartments 65b, c in the shown example.
- the inner compartment 65a dis ⁇ places fluid from the outer compartment 66a via the con ⁇ duits 67 into the outer compartments 66b, c, resulting in the same fluid amount being maintained in each blade, and these will therefore always have the same outer geometri ⁇ cal shape. This structure is thus self-adjusting.
- the above-mentioned self-adjusting properties can be pro- moted by using even more layers of rubber than two, while ensuring the working order of the propeller even if one or more of the layers should puncture. This working order is also ensured by dividing the fluid compartments into seve ⁇ ral mutually independent compartments, as mentioned ear- lier.
- the elastomer propeller of the invention is passively capable of changing the geome ⁇ trical shape of the blades, such that it is optimally adapted to the instantaneous state of operation.
- the pro ⁇ peller can moreover actively be given the shape best suit- able for any purpose and be adjusted if this should be ne ⁇ cessary. This takes place merely by pumping up the blades again in the same simple manner as e.g. a car tyre is pumped up.
- the rubber covering and a possible air filling moreover diminish the propeller noise and dampen the water noise which penetrates into the hull via the propeller.
- the propeller can withstand shocks and im ⁇ pacts from objects in the water or on the sea bottom con ⁇ siderably better than the conventional structures, without receiving permanent deformations.
- the propeller can readily be moulded with an even and smooth surface which does not require expensive after- treatment, and of elastomers, such as rubber, which per se have an extremely good corrosion resistance against attacks from e.g. sea water.
- the elastomer propeller has been described above by way of example in embodiments with three blades. However, the propeller can have any number of blades within the scope of the invention. In some cases, e.g. small propellers, propellers without or with just a small core are moreover conceivable.
- the propeller which is then frequently re ⁇ inforced with a carcass for defining and retaining the geometrical shape of the propeller, then obtains its strength and rigidity by means of the inner positive air pressure like a car tyre.
- the application of the propeller is moreover not restricted to the propulsion of ships, but may equally well be used for many other purposes where the advantageous properties and effects of the propeller can be utilized, e.g. turbines and ventilators.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Diaphragms And Bellows (AREA)
- Sealing Devices (AREA)
Abstract
Description
Claims
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP5508097A JPH07500549A (en) | 1991-10-30 | 1992-10-29 | Elastic propeller with flexible elastic material coating |
EP92923701A EP0609389A1 (en) | 1991-10-30 | 1992-10-29 | An elastomeric propeller having a flexible elastomeric covering |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DK1797/91 | 1991-10-30 | ||
DK179791A DK179791D0 (en) | 1991-10-30 | 1991-10-30 | ELASTOMER PROPELLER WITH FLEXIBLE ELASTOMS COATING |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1993009026A1 true WO1993009026A1 (en) | 1993-05-13 |
Family
ID=8108116
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/DK1992/000312 WO1993009026A1 (en) | 1991-10-30 | 1992-10-29 | An elastomeric propeller having a flexible elastomeric covering |
Country Status (6)
Country | Link |
---|---|
EP (1) | EP0609389A1 (en) |
JP (1) | JPH07500549A (en) |
AU (1) | AU2941392A (en) |
CA (1) | CA2122477A1 (en) |
DK (1) | DK179791D0 (en) |
WO (1) | WO1993009026A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1327579A1 (en) * | 2002-01-09 | 2003-07-16 | Francesco Siri | Propeller blade |
EP1228958A3 (en) * | 2001-02-02 | 2004-01-07 | Howaldtswerke-Deutsche Werft Ag | Method for reducing the noise emission of propellers |
WO2016200282A1 (en) | 2015-06-12 | 2016-12-15 | Preisner Leszek | An aerodynamic element with variable aerodynamics |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5457110B2 (en) * | 2009-09-03 | 2014-04-02 | 住友精密工業株式会社 | Ship propeller |
JP2015180560A (en) * | 2014-03-07 | 2015-10-15 | ナカシマプロペラ株式会社 | marine propeller |
JP2015199483A (en) * | 2014-04-04 | 2015-11-12 | ナカシマプロペラ株式会社 | Propeller for vessel |
JP7365688B2 (en) * | 2019-12-10 | 2023-10-20 | ナカシマプロペラ株式会社 | marine propeller |
RU2768292C1 (en) * | 2020-11-24 | 2022-03-23 | Российская Федерация, От Имени Которой Выступает Министерство Промышленности И Торговли Российской Федерации | Screw propeller with multi-resonant damping device for reducing oscillations and resonant sound emission of screw propeller |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1384308A (en) * | 1917-10-23 | 1921-07-12 | William Hendry Barker | Airplane-screw |
US2107136A (en) * | 1937-09-25 | 1938-02-01 | Zaiger Louis | Fan |
US2251887A (en) * | 1938-06-13 | 1941-08-05 | Master Electric Co | Flexible fan unit |
US2276262A (en) * | 1939-06-27 | 1942-03-10 | United Aircraft Corp | Composite propeller |
US2383342A (en) * | 1941-10-21 | 1945-08-21 | William H Riley | Hollow propeller |
US3256939A (en) * | 1965-01-11 | 1966-06-21 | Matthew J Novak | Marine propeller |
-
1991
- 1991-10-30 DK DK179791A patent/DK179791D0/en unknown
-
1992
- 1992-10-29 JP JP5508097A patent/JPH07500549A/en active Pending
- 1992-10-29 AU AU29413/92A patent/AU2941392A/en not_active Abandoned
- 1992-10-29 EP EP92923701A patent/EP0609389A1/en not_active Withdrawn
- 1992-10-29 WO PCT/DK1992/000312 patent/WO1993009026A1/en not_active Application Discontinuation
- 1992-10-29 CA CA 2122477 patent/CA2122477A1/en not_active Abandoned
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1384308A (en) * | 1917-10-23 | 1921-07-12 | William Hendry Barker | Airplane-screw |
US2107136A (en) * | 1937-09-25 | 1938-02-01 | Zaiger Louis | Fan |
US2251887A (en) * | 1938-06-13 | 1941-08-05 | Master Electric Co | Flexible fan unit |
US2276262A (en) * | 1939-06-27 | 1942-03-10 | United Aircraft Corp | Composite propeller |
US2383342A (en) * | 1941-10-21 | 1945-08-21 | William H Riley | Hollow propeller |
US3256939A (en) * | 1965-01-11 | 1966-06-21 | Matthew J Novak | Marine propeller |
Non-Patent Citations (1)
Title |
---|
PATENT ABSTRACTS OF JAPAN, Vol. 7, No. 116, M-216; & JP,A,58 036 794, 03-03-1983, (ISHIKAWAJIMA HARIMA JUKOGYO K.K.). * |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1228958A3 (en) * | 2001-02-02 | 2004-01-07 | Howaldtswerke-Deutsche Werft Ag | Method for reducing the noise emission of propellers |
EP1327579A1 (en) * | 2002-01-09 | 2003-07-16 | Francesco Siri | Propeller blade |
WO2016200282A1 (en) | 2015-06-12 | 2016-12-15 | Preisner Leszek | An aerodynamic element with variable aerodynamics |
Also Published As
Publication number | Publication date |
---|---|
CA2122477A1 (en) | 1993-05-13 |
DK179791D0 (en) | 1991-10-30 |
AU2941392A (en) | 1993-06-07 |
EP0609389A1 (en) | 1994-08-10 |
JPH07500549A (en) | 1995-01-19 |
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