EP3016855B1 - Assemblage par ajustement serré hélice-moyeu - Google Patents
Assemblage par ajustement serré hélice-moyeu Download PDFInfo
- Publication number
- EP3016855B1 EP3016855B1 EP14739673.3A EP14739673A EP3016855B1 EP 3016855 B1 EP3016855 B1 EP 3016855B1 EP 14739673 A EP14739673 A EP 14739673A EP 3016855 B1 EP3016855 B1 EP 3016855B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- propeller
- propeller hub
- sleeve
- drive shaft
- hub
- 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.)
- Active
Links
- 229910000906 Bronze Inorganic materials 0.000 claims description 4
- 229910000831 Steel Inorganic materials 0.000 claims description 4
- 239000010974 bronze Substances 0.000 claims description 4
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 claims description 4
- 239000010959 steel Substances 0.000 claims description 4
- 239000000463 material Substances 0.000 claims description 3
- 230000005540 biological transmission Effects 0.000 description 3
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 239000004918 carbon fiber reinforced polymer Substances 0.000 description 2
- 230000001419 dependent effect Effects 0.000 description 2
- 238000011161 development Methods 0.000 description 2
- 230000018109 developmental process Effects 0.000 description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 229910000963 austenitic stainless steel Inorganic materials 0.000 description 1
- 238000005452 bending Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 239000011343 solid material Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
Images
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
- B63H1/20—Hubs; Blade connections
-
- 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
- B63H23/32—Other parts
- B63H23/34—Propeller shafts; Paddle-wheel shafts; Attachment of propellers on shafts
Definitions
- the invention relates to a drive device with the features specified in the preamble of claim 1.
- the starting point of the invention are propeller drives in which a propeller hub with individually attached propeller blades is mounted on a drive shaft.
- a press connection of the propeller hub with the drive shaft in this case allows the transmission of comparatively large torques between the propeller hub and the drive shaft. Press connections show the JP S-63180399 U and the DE 12 93056 B ,
- the mostly made of bronze or carbon fiber reinforced plastic propeller blades are bolted from the outside on the outside of the propeller hub.
- the propeller blades usually each have a foot which protrudes transversely to the connecting direction of the propeller blade and propeller hub on the outer contour of the propeller blade, wherein at this projecting beyond the outer contour of the propeller blade portion of the foot, the screwing of the propeller blade with the propeller hub.
- the feet required on the propeller blades result in the propeller hubs having a comparatively large outside diameter, and as the number of propeller blades of the propeller increases, an ever larger propeller hub is required.
- the object of the invention is to provide a drive device of the type described, the propeller compared to the previously conventional propellers with the same number the propeller blades have a smaller propeller hub with regard to their external dimensions or, if the propeller hub has the same size, a larger number of propeller blades may have:
- the drive device according to the invention can in principle be used in any propeller driven vehicle, but is particularly suitable for an underwater vehicle and in particular for a military submarine.
- This drive device is equipped in a conventional manner with a drive shaft and a propeller arranged on the drive shaft.
- the propeller has a propeller hub connected to the drive shaft and at least two propeller blades releasably attached to the propeller hub.
- the underlying idea of the invention is; Starting from one of the drive shaft facing the inside of the propeller hub, the propeller blades are to be screwed to the propeller hub by means of cap screws.
- This type of screw connection has the advantage that the previously required for screwing the propeller blade with the propeller hub on the propeller blades, protruding transversely to the connecting direction of the propeller blade and propeller hub on the outer contour of the propeller blade feet are no longer needed, with the result that in comparison to the previously known propellers of the type in question with the same number of propeller blades
- Propeller hulls can be used with a significantly small outer diameter or the propeller of the drive device according to the invention with the same size propeller hub can have a larger number of propeller blades.
- the propeller hub For screwing the propeller blades with the propeller hub, the propeller hub has through holes; extending in the radial direction through the propeller hub; while the propeller blades, which are expediently formed from a solid material at least in an end region adjoining the propeller hub, have threaded blind holes at their end contacting the propeller hub in the radial direction.
- the cap screws are guided from the inside of the propeller hub through the through holes formed on the propeller hub, and screwed into the blind holes formed on the propeller blades.
- the through holes formed at the propeller hub are provided here at their end adjacent to the inside of the propeller hub, preferably with cylindrical extensions into which the screw heads are countersunk.
- the propeller blades can be brought directly to the outer peripheral surface of the propeller hub to the plant and screwed there with the propeller hub.
- recesses are formed on the outer peripheral surface of the propeller hub, in which engage the ends of the propeller blades.
- depressions extending in the radial direction are provided on the outer circumferential surface of the propeller hub, which are expediently dimensioned such that the propeller blades inserted into the depressions are supported on the side walls of these depressions aligned transversely to the direction of insertion of the propeller blades.
- a particularly secure hold of the propeller blades in the recesses formed on the propeller hub can be realized if, as provided in an advantageous development of the invention, the cross section of the recesses formed on the propeller hub in the direction of a central axis of the propeller hub continuously tapers and the shape the engaging in the recesses ends of the propeller blades corresponds to the shape of the recesses formed on the propeller hub.
- the propeller blades can be fixed in the recesses virtually in the manner of a splined connection, wherein in addition to the positive connection by the engagement of the ends of the propeller blades in the recesses an additional adhesion between the propeller blades and the Propeller hub is generated.
- connection of the propeller hub with the drive shaft takes place in the drive device according to the invention preferably non-positively in the form of a press connection and particularly advantageous via a pressure oil compression bandage; the simple release of the connection of drive shaft and propeller hub, for example, for repair or replacement of the propeller allows:
- the propeller hub of the drive device is preferably arranged over a between the propeller hub and the drive shaft Sleeve connected by means of a Druckölpress saides with the drive shaft, while the propeller hub is preferably connected via a transverse compression bandage with the sleeve.
- the drive shaft in the region of the arrangement of the propeller hub and the sleeve are preferably conically formed on the inside.
- the sleeve On its outer side, the sleeve is preferably cylindrical in this case.
- the outer cylindricity of the sleeve makes it possible to use as a propeller hub an easily manufactured hollow cylindrical ring element.
- the formation of the Querpress claimedes between the sleeve and the propeller hub takes place with appropriate dimensioning of the sleeve and propeller hub by radial expansion of the sleeve in the formation of the pressure oil press fit between the sleeve and the drive shaft.
- the propeller hub has a certain oversize relative to the sleeve.
- a further and preferably additional measure for ensuring a necessary for the required torque transmission joint pressure between the propeller hub and the sleeve is advantageous to form the propeller hub from a Maiterial whose Elastic Discharge is greater than that of the material from which the sleeve is formed. That is, the propeller hub is preferably stiffer than the sleeve.
- the propeller hub made of an austenitic steel and the sleeve are formed of bronze.
- austenitic steel for the propeller hub expediently a stainless steel, for.
- an austenitic stainless steel can be used.
- At least one radially extending through hole is advantageously formed on the propeller hub and the sleeve, the two through holes being aligned with each other and together with an insertion port an oil supply line form.
- two such through holes are provided on the propeller hub and the sleeve, which are formed in the vicinity of the axial ends of propeller hub and sleeve.
- the at least one oil supply line in the contact area of the propeller hub and sleeve is pressure-tight sealed to prevent the oil from entering the joint between the propeller hub and the sleeve.
- a plurality of oil supply lines are provided, which are each sealed pressure-tight in the contact area of the propeller hub and sleeve.
- the through holes formed on the sleeve are formed as threaded holes, in which a connectable with a hydraulic line ⁇ leinGermanstutzen is screwed.
- the screwing of the ⁇ lein gleichstutzen in the threaded holes formed on the sleeve is typically carried out from the outside of the propeller hub, where they are each connected to a hydraulic line.
- the ⁇ lein gleichstutzen are dimensioned so that they are in the radial direction extend beyond the contact area of propeller hub and sleeve and seal this contact area pressure-tight.
- the in Fig. 1 illustrated propeller 2 has a hollow cylindrical propeller hub 4, on whose outside a plurality of propeller blades are arranged, wherein in Fig. 1 For the sake of clarity, only the end portion of a propeller blade 6 adjacent to the propeller hub 4 is shown.
- the propeller hub 4 is made of austenitic steel.
- the propeller blades 6 are made of carbon fiber reinforced plastic, wherein they have a metallic core 8 in one of the propeller hub 4 facing end portion ( Fig. 3 ).
- recesses 10 are formed on the outer peripheral side of the propeller hub, in which the propeller blades 6 with their end portions 12 (see also Fig. 3 ) intervene.
- the recesses 10 delimiting side walls 14 of the recesses 10 are based on the engagement of the end portions 12 in the recesses 10 of the propeller hub 4 slightly bevelled, so that the cross-section of the recesses 10 decreases with increasing depth of the recess 10.
- the shape of the end sections 12 of the propeller blades 6 corresponds to the shape of the recesses 10.
- through holes 16 are formed on the propeller hub 4; which extend from the inside of the propeller hub 4 to the respective recess 10 out. Adjacent to the inside of the propeller hub 4, the through-holes 16 each have a cylindrical extension 18. Corresponding to the position of the through holes 16 formed on the propeller hub 4 are four thread blind holes 20 are formed on the propeller hub 4 radially facing side of the end portions 12 of the propeller blades 6, each hineinerrangen in the metallic core 8 of the propeller blades 6. The through holes 16 formed on the propeller hub 4 and the threaded blind holes 20 formed on the end portions 12 of the propeller blades 6 serve to receive cap screws 22 with which the propeller blades 6 are bolted to the propeller hub 4.
- the propeller 2 is attached to a drive shaft 24 operatively connected to a drive motor.
- the propeller 2 is attached to a portion 26 of the drive shaft, which is conical.
- a sleeve 28 is arranged at the portion 26 of the drive shaft 24, a sleeve 28 is arranged.
- This sleeve 28 is formed of bronze.
- the sleeve 28 has a conical inner volume.
- Radially on the outside, the sleeve 28 is cylindrical, wherein at an in Fig. 3 left end of the sleeve 28 is a radially outwardly projecting Ringkrageh 30 is formed.
- the sleeve 28 is peripherally surrounded by the propeller hub 4, which bears against the annular collar 30.
- the sleeve 28 is rotatably connected by means of a pressure oil press fit with the drive shaft 24.
- a joint 32 between the sleeve 28 and the portion 26 of the drive shaft 24 it is necessary in a joint 32 between the sleeve 28 and the portion 26 of the drive shaft 24 to build up an oil film:
- two ⁇ leinschreibstutzen 32 are provided, each by a radially through the propeller hub 4 extending through hole 34 are guided and screwed in an aligned and radially extending through the sleeve 28 through hole 36.
- the ⁇ leinriostutzen 38 and the through holes 36 are sealed pressure-tight, so that no oil can penetrate into the contact area between the propeller hub 4 and the sleeve 28.
- a pressing device 40 which around a cylindrical portion 42 of the drive shaft 24, the in Fig. 3 is located to the left of the section 26, is arranged around. Out Fig. 3 not visible, the pressing device 40 is secured against axial movement.
- an annular space 44 is formed, which extends around the entire drive shaft 24 around. This annular space 44 is designed to be open in the direction of the sleeve 28 located next to the pressing device 40.
- an oil supply line 46 leads to the annular space 44.
- an annular piston 48 is slidably mounted in the axial direction of the drive shaft 24; If oil is introduced into the annular space 44 via the oil feed line 46, the annular piston 48 is pressed out of the annular chamber 44, wherein the sleeve 28 is displaced in the direction of the increasing slope of the portion 26 of the drive shaft 24.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Claims (10)
- Dispositif d'entraînement, en particulier pour un sous-marin, comprenant un arbre d'entraînement (24) et une hélice (2) disposée sur l'arbre d'entraînement (24), qui présente un moyeu d'hélice (4) connecté à l'arbre d'entraînement (24) et au moins deux pales d'hélice (6) fixées de manière amovible au moyeu d'hélice (4), les pales d'hélice (6) étant vissées au moyen de vis à tête (22) au moyeu d'hélice (4) à partir d'un côté intérieur du moyeu d'hélice (4) tourné vers l'arbre d'entraînement (24), le moyeu d'hélice (4) étant connecté à l'arbre d'entraînement (24) par le biais d'une douille (28) disposée entre le moyeu d'hélice (4) et l'arbre d'entraînement (24) au moyen d'un assemblage par ajustement serré à huile sous pression et un dispositif de pressage (40) étant prévu pour former l'assemblage par ajustement serré à huile sous pression, caractérisé en ce qu'un espace annulaire (44) s'étendant autour de l'arbre d'entraînement (24) est réalisé au niveau du dispositif de pressage (40), un piston annulaire (48) étant supporté de manière déplaçable dans l'espace annulaire (44) dans la direction axiale de l'arbre d'entraînement (24), et de l'huile pouvant être introduite dans l'espace annulaire (44) par le biais d'une conduite d'alimentation en huile (46).
- Dispositif d'entraînement selon la revendication 1, caractérisé en ce que des évidements (10) sont réalisés au niveau de la surface périphérique extérieure du moyeu d'hélice (4), dans lesquels évidements s'engagent des extrémités des pales d'hélice (6).
- Dispositif d'entraînement selon la revendication 2, caractérisé en ce que la section transversale des évidements (10) réalisés au niveau du moyeu d'hélice (4) se rétrécit de manière continue dans la direction d'un axe médian du moyeu d'hélice (4) et la forme des extrémités des pales d'hélice (6) s'engageant dans les évidements (10) correspond à la forme des évidements (10) réalisés au niveau du moyeu d'hélice (4).
- Dispositif d'entraînement selon l'une quelconque des revendications 1 à 3, caractérisé en ce que l'arbre d'entraînement (24) est réalisé sous forme conique dans la région de l'agencement du moyeu d'hélice (4) et la douille (28) est réalisée à l'intérieur de manière conique et sous forme cylindrique au niveau de son côté extérieur.
- Dispositif d'entraînement selon l'une quelconque des revendications 1 à 4, caractérisé en ce que le moyeu d'hélice (4) présente un surdimensionnement par rapport à la douille (28).
- Dispositif d'entraînement selon l'une quelconque des revendications 4 à 5, caractérisé en ce que le moyeu d'hélice (4) est réalisé à partir d'un matériau dont le module d'élasticité est supérieur à celui du matériau constituant la douille (28).
- Dispositif d'entraînement selon la revendication 6, caractérisé en ce que le moyeu d'hélice (4) est réalisé à partir d'un acier austénitique et la douille (28) est réalisée en bronze.
- Dispositif d'entraînement selon l'une quelconque des revendications 5 à 7, caractérisé en ce qu'à chaque fois au moins un trou de passage (34, 36) s'étendant la direction radiale est réalisé au niveau du moyeu d'hélice (4) et de la douille (28), les deux trous de passage (34, 36) étant alignés l'un avec l'autre et formant conjointement avec une tubulure d'introduction d'huile (38) une conduite d'alimentation en huile.
- Dispositif d'entraînement selon la revendication 8, caractérisé en ce que l'au moins une conduite d'alimentation en huile est étanchéifiée de manière étanche à la pression dans la région de contact entre le moyeu d'hélice (4) et la douille (28) .
- Dispositif d'entraînement selon la revendication 9, caractérisé en ce que l'au moins un trou traversant (34, 36) réalisé au niveau de la douille (28) est réalisé sous forme de trou fileté dans lequel est vissée une tubulure d'introduction d'huile (38) pouvant être connectée à une conduite hydraulique.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102013212948.3A DE102013212948A1 (de) | 2013-07-03 | 2013-07-03 | Antriebsvorrichtung |
PCT/EP2014/001767 WO2015000572A1 (fr) | 2013-07-03 | 2014-06-27 | Assemblage par ajustement serré hélice-moyeu |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3016855A1 EP3016855A1 (fr) | 2016-05-11 |
EP3016855B1 true EP3016855B1 (fr) | 2018-02-21 |
Family
ID=51210402
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP14739673.3A Active EP3016855B1 (fr) | 2013-07-03 | 2014-06-27 | Assemblage par ajustement serré hélice-moyeu |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP3016855B1 (fr) |
KR (1) | KR101857890B1 (fr) |
DE (1) | DE102013212948A1 (fr) |
WO (1) | WO2015000572A1 (fr) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102022113278A1 (de) * | 2022-05-25 | 2023-11-30 | KSB SE & Co. KGaA | Rührwerkanordnung |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1293056B (de) * | 1963-02-18 | 1969-04-17 | P & O Res & Dev Co | Keilnutlose Verbindung eines Schiffspropellers mit der Propellerwelle |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1036492A (en) * | 1964-05-04 | 1966-07-20 | John Michael Langham | Improvements in or relating to a marine propeller assembly and a method of mounting same |
US3470843A (en) * | 1966-07-07 | 1969-10-07 | Satterthwaite James G | Torque-journal hub propeller |
GB1209786A (en) * | 1967-12-11 | 1970-10-21 | Glacier Co Ltd | Stern constructions for marine vessels having propellers with detachable blades |
DE2302251A1 (de) * | 1972-01-24 | 1973-08-02 | Kanonerskij Sudoremontnyj Sawo | Schiffsschraube mit abnehmbaren fluegeln |
GB1455504A (en) * | 1974-02-15 | 1976-11-10 | Stone Manganese Marine Ltd | Marine propellers |
DE2535664C3 (de) * | 1975-08-09 | 1978-04-20 | Blohm + Voss Ag, 2000 Hamburg | Vorrichtung zum Montieren einer Schiffsschraube |
DE2550755C2 (de) * | 1975-11-12 | 1984-05-03 | Anton Piller Kg, 3360 Osterode | Laufrad für Axialgebläse |
GB1482375A (en) * | 1976-04-08 | 1977-08-10 | Stone Manganese Marine Ltd | Marine-propeller assemblies |
DE2828257A1 (de) * | 1978-06-28 | 1980-01-03 | Pilgrim Eng Dev | Verfahren zur befestigung einer schiffsschraube und anordnung hierfuer |
JPS63180399U (fr) * | 1987-05-11 | 1988-11-22 | ||
DE4236253C2 (de) * | 1992-10-20 | 1997-05-15 | Sulzer Hydro Gmbh | Vorrichtung zum Verändern der Winkelstellung von Flügeln eines Schiffspropellers |
SE514094C2 (sv) * | 1999-05-19 | 2001-01-08 | Kamewa Ab | Fartygspropeller med löstagbart fastsatta blad |
CN103482047B (zh) * | 2013-10-09 | 2015-10-28 | 中国船舶重工集团公司第七0四研究所 | 桨叶分离螺距微调式四叶螺旋桨 |
-
2013
- 2013-07-03 DE DE102013212948.3A patent/DE102013212948A1/de not_active Withdrawn
-
2014
- 2014-06-27 KR KR1020167002851A patent/KR101857890B1/ko active IP Right Grant
- 2014-06-27 WO PCT/EP2014/001767 patent/WO2015000572A1/fr active Application Filing
- 2014-06-27 EP EP14739673.3A patent/EP3016855B1/fr active Active
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1293056B (de) * | 1963-02-18 | 1969-04-17 | P & O Res & Dev Co | Keilnutlose Verbindung eines Schiffspropellers mit der Propellerwelle |
Also Published As
Publication number | Publication date |
---|---|
KR101857890B1 (ko) | 2018-05-14 |
DE102013212948A1 (de) | 2015-01-08 |
EP3016855A1 (fr) | 2016-05-11 |
KR20160027167A (ko) | 2016-03-09 |
WO2015000572A1 (fr) | 2015-01-08 |
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