EP2627910B1 - Fan comprising fan blades - Google Patents
Fan comprising fan blades Download PDFInfo
- Publication number
- EP2627910B1 EP2627910B1 EP11773440.0A EP11773440A EP2627910B1 EP 2627910 B1 EP2627910 B1 EP 2627910B1 EP 11773440 A EP11773440 A EP 11773440A EP 2627910 B1 EP2627910 B1 EP 2627910B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- fan
- hub
- blade
- fan blade
- region
- 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
- 239000003381 stabilizer Substances 0.000 claims description 18
- 230000005484 gravity Effects 0.000 claims description 4
- 238000004519 manufacturing process Methods 0.000 description 7
- 239000000463 material Substances 0.000 description 6
- 230000035508 accumulation Effects 0.000 description 4
- 238000009825 accumulation Methods 0.000 description 4
- 230000008901 benefit Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 238000005452 bending Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 238000009423 ventilation Methods 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/38—Blades
- F04D29/384—Blades characterised by form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/325—Rotors specially for elastic fluids for axial flow pumps for axial flow fans
- F04D29/329—Details of the hub
Definitions
- the invention relates to a fan with fan blades, in particular for radiators of motor vehicles, wherein the fan blades are mounted on a fan hub.
- a fan with fan blades which has a hub ramp on the pressure side of the fan blades, whereby the flow is stabilized on the pressure side of the fan blades.
- air guide elements Arranged on the suction-side region of the fan blades are air guide elements which form a flow channel and guide the air in a targeted manner from the hub to the suction side of the fan blade, ie in the region of the cylindrical fan hub or in the region of the hub ramp.
- the invention is therefore based on the object of specifying a fan with fan blades, which ensures a reduction of the mass accumulation in the area of the connections of the fan blades, wherein the production box of the fan is reduced and the production time is reduced.
- each fan blade is angled towards a blade root to the rear, wherein an angled portion of the fan blade is at least partially pulled down on the fan hub.
- a curvature and / or a radius of the fan blade in a first region of the fan blade extending outwards from the bend are different from a curvature and / or a radius of the second area extending from the bend towards the fan hub, the second area of the fan blade being pulled down onto the fan hub.
- the second area of the fan blade which is pulled down onto the fan hub, is designed to be angled forward in the direction of rotation on the leading edge.
- This embodiment improves the flow conditions between the two successive fan blades.
- the clogging of the fan blade in the area of the fan hub also serves to improve the acoustic properties of the fan.
- a hub ramp between two fan blades is conical. This hub ramp stabilizes the hub area, which allows a clean and low-loss flow around the blade root in the fan hub.
- the hub ramp starting from the blade root of a fan blade arranged on the fan hub, is guided directly onto the trailing edge of the following fan blade.
- the auxiliary ramp forms an integral part of the fan blade, which is particularly advantageous in terms of flow. As a result, the strength of the fan is guaranteed with a low material usage.
- a stabilizer is arranged on a side of the fan blades facing away from the hub ramp, which stabilizer is formed in particular on the second area of the fan blade in the section of the fan blade that is pulled down onto the fan hub.
- the stabilizer serves as Flow control and prevents vortex structures in the fan hub.
- the stabilizer runs on a smaller radius than the hub ramp on the back of the fan blade.
- the stabilizer is arranged as an injection molded part on the fan blade. The stabilizers in the blade root area of the fan blades on the suction side of the fan blades separate the hub and blade flow and prevent flow separation and harmful vortex formation.
- the center of gravity of the fan blade preferably the first area of the fan blade, is advanced so far forward to the suction side that a centrifugal force acting on the fan blade and an aerodynamic force generated by a pressure increase approximately compensate each other.
- This has the advantage that the reaction force of the fan blade resulting from the centrifugal forces lies in the flow direction in front of the fan hub.
- At least one rib on the pressure side of the fan is arranged radially at the position of the connection of the blade root to the fan hub. This ensures the flow of power from the fan hub to the fan blade.
- the rib has a curved outer edge, wherein the rib extends from the fan hub to preferably to the hub ramp. This tension-optimized swing of the rib trailing edge reduces the material usage.
- the at least one rib are arranged next to the actual connection of the fan blade to the fan hub, so that this connection, which is exposed to the highest load by the pressure building up, is relieved.
- a fan with fan blades which are designed as axial blades, is used in a commercial vehicle, where it is driven by a vehicle engine becomes.
- the fan is connected to an engine end face either directly on a crankshaft or via a belt or gear output with this.
- the regulation of the rotation time of the fan is carried out by a clutch which is arranged within a fan hub. Due to this coupling to the vehicle engine, high mechanical loads act on the fan. On the one hand in the form of vibrations of the vehicle engine or by the bending of the crankshaft. On the other hand by the speed.
- an overspeed of the vehicle engine as a result of a switching error of the clutch is not regulated so fast, so that acts on the fan high speed load.
- Such a fan 1 is in FIG. 1 and consists of a plurality of fan blades 2, which are arranged around a fan hub 3 and secured thereto with a blade root 15.
- Each fan blade 2 is divided into two areas 4, 5.
- the fan blade 2 has a bend 6 between these two areas 4, 5.
- the second, leading to Lüfternabe, inner region 5 is pulled back away from the first, outwardly projecting portion 4 and rests on the fan hub 3.
- the first region 4 of the fan blade 2 in this case has a different arc profile than the second region 5 of the fan blade 2, which is pulled down onto the fan hub 3.
- a smaller radius is set at the first, larger radius of the first area 4 of the fan blade 2, so that the second area 5 of the fan blade 2 forms a different arc than the first area 4 of the fan blade 2.
- the bumps change the first area 4 and the second area 5 of the fan blade 2.
- the leading edge 8 of the pulled-down second region 5 of the fan blade 2 in the direction of rotation of the fan 1 is sown forward.
- the sacculated area of the front edge 8 of the fan blade 2 in the area of the fan hub 3 is identified by the reference numeral 8a. This sickle contributes to an improvement in the acoustics of the fan 1.
- the momentum of the second region 5 of the fan blade 2 is thereby pulled out of the area of the fan hub 3.
- FIG. 3 a cutout on the back (pressure side) of the fan 1 is shown, wherein at each fan blade 2, a hub ramp 9 is arranged.
- This hub ramp 9 is made conical in the area between the fan blade 2 and the subsequent fan blade 2a.
- the ramp leading edge 13 is rounded and pulled toward the fan hub 3 inwards.
- the hub ramp 9 is performed starting from the fan hub 3 directly from the previous fan blade 2 on the trailing edge 10 of the following fan blade 2a.
- the hub ramp 9 and the fan blade 2 form a structural unit and are integrally fused with one another, since the hub ramp 9 extends starting from the connection point of the second region 5 of the fan blade 2.
- the hub ramp 9 ends at the trailing edge 10 of the next fan blade 2a, approximately halfway up the fan blade 2a. With this configuration, the strength of the fan 1 is ensured at a low material usage.
- the hub ramp 9 is stabilized by a plurality of ribs 11 relative to the fan hub 3.
- FIG. 4 a section of the front (storage side) of the fan 1 is shown.
- a stabilizer 7 is arranged at the front of the fan blade 2.
- the hub ramp 9, which is located on the back of the fan blade 2, is shown in phantom for this reason.
- the stabilizer 7 is approximately perpendicular to the fan blade 2 and protrudes out of this, whereby the flow is stabilized.
- the stabilizer 7 serves as a flow guide to prevent vortex structures in the area of the fan hub 3 in their propagation.
- the stabilizer 7 begins on the fan blade 2 in the pulled-down area 5 (second area 5 of the fan blade 2) and ends at the leading edge 8 of the fan blade 2. Opposite the fan hub 3, the stabilizer 7 has a smaller radius than the hub ramp. 9
- FIG. 5 shows a plan view of the back of the fan 1, on which radially extending ribs 11 are arranged, which serve to stiffen the fan 1.
- at least three ribs 11 are provided on each fan blade 2, wherein at least two ribs 11 support the hub ramp 9. These ribs 11 contribute to the fact that the respective fan blades 2 is better relieved when voltage spikes occur. In this case, the power flow is ensured by the fan hub 3 in the fan blade 2 by the ribs 11.
- the ribs 11 are arranged right and left to the connection 14 of the fan blade 2 to the fan hub 3. As a result, this point, which is the point with the highest load, relieved.
- the depth of the ribs 11 at the connection 14 to the fan hub 3 and the hub ramp 9 is minimal for reasons of material savings, but deep enough that the stresses in the hub ramp 9 by the centrifugal force which acts on the fan blade 2, not too large.
- the rib 11 ends about 2 cm in front of the rear edge of the hub ramp 9.
- the ribs 11 in this case have a curved outer edge 12 and extending in their area starting from the fan hub 3 in the direction of the hub ramp 9. This curved rib shape improves the flow conditions at this point.
- This centrifugal force F Z counteracts an aerodynamic force F D.
- This aerodynamic force F D arises on the back (pressure side) of the fan blade 2 by an increase in pressure.
- the aerodynamic force F D acts on the trailing edge of the fan blade 2 and tries to move the fan blade 2 in the direction of the air conveying direction 17.
- the fan blade 2 builds up a pressure.
- the described fan 1 is made of a plastic. Manufacturing technology, the fan 1 is generated with a simple on / off tool without the use of slides, whereby the use of plastic is minimized.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
Die Erfindung betrifft einen Lüfter mit Lüfterschaufeln, insbesondere für Kühler von Kraftfahrzeugen, wobei die Lüfterschaufeln auf einer Lüfternabe befestigt sind.The invention relates to a fan with fan blades, in particular for radiators of motor vehicles, wherein the fan blades are mounted on a fan hub.
Gemäß der
Aus der
Der Erfindung liegt somit die Aufgabe zugrunde, einen Lüfter mit Lüfterschaufeln anzugeben, welcher eine Reduzierung der Massenanhäufung im Bereich der Anbindungen der Lüfterschaufeln gewährleistet, wobei die Herstelfungskasten des Lüfters reduziert und die Herstellungszeit verringert wird.The invention is therefore based on the object of specifying a fan with fan blades, which ensures a reduction of the mass accumulation in the area of the connections of the fan blades, wherein the production box of the fan is reduced and the production time is reduced.
Erfindungsgemäß wird die Aufgabe dadurch gelöst, dass jede Lüfterschaufel in Richtung einer Schaufelwurzel nach hinten abgewinkelt ist, wobei ein abgewinkelter Bereich der Lüfterschaufel mindestens teilweise auf die Lüfternabe heruntergezogen ist.According to the invention the object is achieved in that each fan blade is angled towards a blade root to the rear, wherein an angled portion of the fan blade is at least partially pulled down on the fan hub.
Dies hat den Vorteil, dass die Massenanhäufungen reduziert werden, wodurch sich die Gefahr von fertigungsbedingten Lufteinschlüssen und Lunkern reduziert und eine verkürzte Fertigungszeit gewährleistet wird. Durch die heruntergezogene Vorderkante der Lüfterschaufel wird bei einem wesentlich geringeren Einsatz an Material die Festigkeit des Lüfters verbessert. Erfindungsgemäß sind eine Wölbung und/oder ein Radius der Lüfterschaufel in einem sich von der Abwinklung nach außen erstreckenden ersten Bereich der Lüfterschaufel verschieden zu einer Wölbung und/oder einem Radius des zweiten, sich von der Abwinklung in Richtung Lüfternabe ausdehnenden Bereich, wobei der zweite Bereich der Lüfterschaufel auf die Lüfternabe heruntergezogen ist. Durch eine solche Anbindung der Lüfterschaufel an die Lüfternabe wird ein sehr homogener und spannungsoptimierter Übergang erreicht.This has the advantage that the mass accumulations are reduced, whereby the risk of production-related air pockets and voids is reduced and a shorter production time is ensured. The pulled down leading edge of the fan blade improves the strength of the fan while significantly reducing the amount of material used. According to the invention, a curvature and / or a radius of the fan blade in a first region of the fan blade extending outwards from the bend are different from a curvature and / or a radius of the second area extending from the bend towards the fan hub, the second area of the fan blade being pulled down onto the fan hub. By such a connection of the fan blade to the fan hub a very homogeneous and voltage-optimized transition is achieved.
In einer Ausgestaltung ist die, auf die Vorderkante des auf die Lüfternabe heruntergezogenen zweiten Bereiches der Lüfterschaufel in Drehrichtung nach vorn gesichelt ausgebildet. Durch diese Ausgestaltung werden die Strömungsbedingungen zwischen den zwei aufeinander folgenden Lüfterschaufeln verbessert. Die Sichelung der Lüfterschaufel im Bereich der Lüfternabe dient auch zur Verbesserung der akustischen Eigenschaften des Lüfters. Erfindungsgemäß ist eine Nabenrampe zwischen zwei Lüfterschaufeln konisch ausgebildet. Diese Nabenrampe stabilisiert den Nabenbereich, wodurch eine saubere und verlustarme Umströmung der Schaufelwurzel im Bereich der Lüfternabe ermöglicht wird.In one embodiment, the second area of the fan blade, which is pulled down onto the fan hub, is designed to be angled forward in the direction of rotation on the leading edge. This embodiment improves the flow conditions between the two successive fan blades. The clogging of the fan blade in the area of the fan hub also serves to improve the acoustic properties of the fan. According to the invention, a hub ramp between two fan blades is conical. This hub ramp stabilizes the hub area, which allows a clean and low-loss flow around the blade root in the fan hub.
In einer Ausgestaltung ist die Nabenrampe ausgehend von der an der Lüfternabe angeordneten Schaufelwurzel einer Lüfterschaufel direkt auf die Hinterkante der nachfolgenden Lüfterschaufel geführt. Bei dieser Gestaltung bildet die Nebenrampe einen integralen Bestandteil der Lüfterschaufel, was strömungstechnisch besonders vorteilhaft ist. Hierdurch wird die Festigkeit des Lüfters bei einem geringen Materialeinsatz gewährleistet.In one embodiment, the hub ramp, starting from the blade root of a fan blade arranged on the fan hub, is guided directly onto the trailing edge of the following fan blade. In this design, the auxiliary ramp forms an integral part of the fan blade, which is particularly advantageous in terms of flow. As a result, the strength of the fan is guaranteed with a low material usage.
In einer Weiterbildung ist auf einer, der Nabenrampe abgewandten Seite der Lüfterschaufeln ein Stabilisator angeordnet, welcher insbesondere auf dem zweiten Bereich der Lüfterschaufel in dem auf die Lüfternabe heruntergezogenen Abschnitt der Lüfterschaufel ausgebildet ist. Der Stabilisator dient als Strömungsleitelement und unterbindet Wirbelstrukturen im Bereich der Lüfternabe.In a further development, a stabilizer is arranged on a side of the fan blades facing away from the hub ramp, which stabilizer is formed in particular on the second area of the fan blade in the section of the fan blade that is pulled down onto the fan hub. The stabilizer serves as Flow control and prevents vortex structures in the fan hub.
In einer anderen Ausführungsform verläuft der Stabilisator auf einem kleineren Radius als die Nabenrampe auf der Rückseite der Lüfterschaufel. Dabei ist der Stabilisator als Spritzgussteil an der Lüfterschaufel angeordnet. Die Stabilisatoren im Schaufelwurzelbereich der Lüfterschaufeln bewirken auf der Saugseite der Lüfterschaufeln eine Trennung von Naben- und Schaufelströmung und verhindern eine Ablösung der Strömung sowie eine schädliche Wirbelbildung.In another embodiment, the stabilizer runs on a smaller radius than the hub ramp on the back of the fan blade. The stabilizer is arranged as an injection molded part on the fan blade. The stabilizers in the blade root area of the fan blades on the suction side of the fan blades separate the hub and blade flow and prevent flow separation and harmful vortex formation.
Vorteilhafterweise ist der Schwerpunkt der Lüfterschaufel, vorzugsweise der erste Bereich der Lüfterschaufel, so weit nach vorn zur Saugseite vorgeschoben, dass sich eine, an der Lüfterschaufel wirkende Zentrifugalkraft und eine, durch eine Druckerhöhung erzeugte aerodynamische Kraft annähernd gegenseitig kompensieren. Das hat den Vorteil, dass die aus den Fliehkräften resultierende Reaktionskraft der Lüfterschaufel in Strömungsrichtung vor der Lüfternabe liegt.Advantageously, the center of gravity of the fan blade, preferably the first area of the fan blade, is advanced so far forward to the suction side that a centrifugal force acting on the fan blade and an aerodynamic force generated by a pressure increase approximately compensate each other. This has the advantage that the reaction force of the fan blade resulting from the centrifugal forces lies in the flow direction in front of the fan hub.
In einer Weiterbildung ist an der Position der Anbindung der Schaufelwurzel an die Lüfternabe mindestens eine Rippe auf der Druckseite des Lüfters radial angeordnet. Dadurch wird der Kraftfluss von der Lüfternabe in die Lüfterschaufel gewährleistet.In a further development, at least one rib on the pressure side of the fan is arranged radially at the position of the connection of the blade root to the fan hub. This ensures the flow of power from the fan hub to the fan blade.
In einer Variante weist die Rippe eine geschwungene Außenkante auf, wobei sich die Rippe von der Lüfternabe bis vorzugsweise zur Nabenrampe erstreckt. Durch diesen spannungsoptimierten Schwung der Rippenhinterkante wird der Materialeinsatz reduziert. Darüber hinaus sind die mindestens eine Rippe neben der eigentlichen Anbindung der Lüfterschaufel an der Lüfternabe angeordnet, so dass diese Anbindung, welche der höchsten Belastung durch den sich aufbauenden Druck ausgesetzt ist, entlastet wird.In a variant, the rib has a curved outer edge, wherein the rib extends from the fan hub to preferably to the hub ramp. This tension-optimized swing of the rib trailing edge reduces the material usage. In addition, the at least one rib are arranged next to the actual connection of the fan blade to the fan hub, so that this connection, which is exposed to the highest load by the pressure building up, is relieved.
Der Erfindung liegen zahlreiche Ausführungsformen zugrunde. Eine davon soll anhand der in der Zeichnung dargestellten Figuren näher erläutert werden.The invention is based on numerous embodiments. One of them will be explained in more detail with reference to the figures shown in the drawing.
Es zeigt:
- Figur 1:
- perspektivische Ansicht einer Ausführungsform eines erfindungsgemäßen Lüfters
- Figur 2:
- Ausschnitt auf eine Vorderseite des Lüfters gemäß
Figur 1 - Figur 3:
- Ausschnitt auf eine Rückseite des Lüfters gemäß
Figur 1 - Figur 4:
- Darstellung des Stabilisators und einer Rampe an einer Lüfterschaufel
- Figur 5:
- radial angeordnete Rippen auf der Rückseite des Lüfters
- Figur 6:
- vergrößerte Darstellung der radial angeordneten Rippen gemäß
Figur 5 - Figur 7:
- Anbindung der Lüfterschaufel an die Lüfternabe
- Figur 8:
- Prinzipdarstellung der Kräfteverhältnisse, die an der Lüfterschaufel angreifen
- FIG. 1:
- perspective view of an embodiment of a fan according to the invention
- FIG. 2:
- Section on a front of the fan according to
FIG. 1 - FIG. 3:
- Section on a back of the fan according to
FIG. 1 - FIG. 4:
- Illustration of the stabilizer and a ramp on a fan blade
- FIG. 5:
- radially arranged ribs on the back of the fan
- FIG. 6:
- enlarged view of the radially arranged ribs according to
FIG. 5 - FIG. 7:
- Connection of the fan blade to the fan hub
- FIG. 8:
- Schematic representation of the balance of power acting on the fan blade
Gleiche Merkmale sind mit gleichen Bezugszeichen gekennzeichnet.Identical features are identified by the same reference numerals.
Ein Lüfter mit Lüfterschaufeln, welche als Axialschaufeln ausgebildet sind, wird in einem Nutzfahrzeug eingesetzt, wo er von einem Fahrzeugmotor angetrieben wird. Der Lüfter ist dabei an einer Motorstirnfläche entweder direkt auf einer Kurbelwelle oder über einen Riemen- bzw. Zahnradabtrieb mit dieser verbunden. Die Regelung der Drehzeit des Lüfters wird dabei von einer Kupplung vorgenommen, welche innerhalb einer Lüfternabe angeordnet ist. Durch diese Ankopplung an den Fahrzeugmotor wirken hohe mechanische Belastungen auf den Lüfter. Zum einen in Form von Vibrationen des Fahrzeugmotors bzw. durch die Biegung der Kurbelwelle. Zum anderen durch die Drehzahl. So wird beispielsweise eine Überdrehzahl des Fahrzeugmotors infolge eines Schaltfehlers von der Kupplung nicht so schnell ausgeregelt, so dass auf den Lüfter eine hohe Drehzahlbelastung wirkt.A fan with fan blades, which are designed as axial blades, is used in a commercial vehicle, where it is driven by a vehicle engine becomes. The fan is connected to an engine end face either directly on a crankshaft or via a belt or gear output with this. The regulation of the rotation time of the fan is carried out by a clutch which is arranged within a fan hub. Due to this coupling to the vehicle engine, high mechanical loads act on the fan. On the one hand in the form of vibrations of the vehicle engine or by the bending of the crankshaft. On the other hand by the speed. Thus, for example, an overspeed of the vehicle engine as a result of a switching error of the clutch is not regulated so fast, so that acts on the fan high speed load.
Ein solcher Lüfter 1 ist in
Wie aus der
In
In
Wie aus der
auf. Beim Drehen des Lüfters 1 wird eine Zentrifugalkraft FZ der Lüfterschaufel 2 erzeugt, die an der Vorderkante der Lüfterschaufel 2 auftritt. Das bedeutet, dass die aus den Zentrifugalkräften FZ resultierende Reaktionskraft FR der Lüfterschaufel 2, welche aus
- ω
- Drehgeschwindigkeit des Lüfters,
- ρ
- Dichte
- V
- verdrängtes Luftvolumen
- r
- Radius des Lüfters,
on. When rotating the
- ω
- Rotational speed of the fan,
- ρ
- density
- V
- displaced air volume
- r
- Radius of the fan,
Dieser Zentrifugalkraft FZ wirkt eine aerodynamische Kraft FD entgegen. Diese aerodynamische Kraft FD entsteht auf der Rückseite (Druckseite) der Lüfterschaufel 2 durch eine Druckerhöhung. Die aerodynamische Kraft FD wirkt auf die Hinterkante der Lüfterschaufel 2 und versucht die Lüfterschaufel 2 in Richtung der Luftförderrichtung 17 zu bewegen. Die Lüfterschaufel 2 baut dabei einen Druck auf.This centrifugal force F Z counteracts an aerodynamic force F D. This aerodynamic force F D arises on the back (pressure side) of the
Diese aerodynamischen Kräfte sind bei gleichbleibender Drehzahl des Lüfters 1 abhängig vom Arbeitspunkt, so dass für die Auslegung des Lüfters 1 eine Annahme bezüglich des Arbeitspunktes gemacht werden muss. In die Lüfternabe 3 wird kein Moment eingeleitet. Die aerodynamischen Kräfte und die Fliehkräfte steigen dabei quadratisch mit der Drehzahl.These aerodynamic forces are at constant speed of the
Aufgrund der seitlichen Verschiebung des Schwerpunktes der Lüfterschaufel 2 um den Abstand a von der Lüfternabe 3 in Richtung Luftförderrichtung 17, greift die Zentrifugalkraft FZ nicht an der Lüfternabe 3 an, sondern versucht die Lüfterschaufel 2 nach hinten zu kippen. Dies wird durch die angreifenden aerodynamischen Kräfte FD aufgrund des besonderen Abstandes der Lüfterschaufel 2 von der Lüfternabe kompensiert.Due to the lateral displacement of the center of gravity of the
Der beschriebene Lüfter 1 ist aus einem Kunststoff hergestellt. Fertigungstechnisch wird der Lüfter 1 mit einem einfachen Auf/Zu-Werkzeug ohne den Einsatz von Schiebern erzeugt, wobei der Einsatz von Kunststoff minimiert wird.The described
Claims (8)
- A fan comprising fan blades, in particular for radiators of motor vehicles, wherein the fan blades (2) are attached to a fan hub (3), characterised in that each fan blade (2) is angled rearward in the direction of a blade root (15), wherein an angled region (5) of the fan blade (2) is bent down towards the fan hub (3), wherein a curvature and/or a radius of the fan blade (2) in a first region (4) extending outward from the angle (6) is different to a curvature and/or a radius of the second region (5) extending from the angle (6) in the direction of the fan hub (3), wherein the second region (5) of the fan blade (2) is bent down towards the fan hub (3), and wherein a hub ramp (9) is formed conically in the region between the blade front edge of one and the blade rear edge of the following fan blades (2, 2a).
- The fan as claimed in claim 1, characterised in that the front edge (8) of the second region (5) of the fan blade (2) which is bent down towards the fan hub (3) is formed in a sickle-shaped manner (8a) in the direction of rotation.
- The fan as claimed in claim 1 or 2, characterised in that the hub ramp (9), starting from the blade root (15) of the fan blade (2) arranged on the fan hub (3), is guided directly onto the rear edge (10) of the following fan blade (2a).
- The fan as claimed in at least one of the preceding claims, characterised in that a stabiliser (7) is arranged on a side of the fan blade (2) facing away from the hub ramp (9) and is formed in particular on the second region (5) of the fan blade (2) in the segment bent down towards the fan hub (3).
- The fan as claimed in claim 4, characterised in that the stabiliser (7) on the front edge of the fan blade (2) runs on a smaller radius than the radial extension of the hub ramp (9) on the back of the fan blade (2).
- The fan as claimed in at least one of the preceding claims, characterised in that the centre of gravity (16) of the fan blade (2) is displaced so far forward towards the suction side that a centrifugal force (FZ) acting on the fan blade (2) and an aerodynamic force (FD) generated by a pressure increase on the fan blade approximately compensate for each other.
- The fan as claimed in at least one of the preceding claims, characterised in that at least one rib (11) is arranged radially on the pressure side of the fan (1) approximately at the attachment (14) of the blade root (15) to the fan hub (3).
- The fan as claimed in claim 7, characterised in that the rib (11) has a curved outer edge (12), wherein the rib (11) extends from the fan hub (3) preferably up to the hub ramp (9).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102010042325A DE102010042325A1 (en) | 2010-10-12 | 2010-10-12 | Fan with fan blades |
PCT/EP2011/067835 WO2012049220A1 (en) | 2010-10-12 | 2011-10-12 | Fan comprising fan blades |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2627910A1 EP2627910A1 (en) | 2013-08-21 |
EP2627910B1 true EP2627910B1 (en) | 2017-06-21 |
Family
ID=44862963
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP11773440.0A Active EP2627910B1 (en) | 2010-10-12 | 2011-10-12 | Fan comprising fan blades |
Country Status (8)
Country | Link |
---|---|
US (1) | US9447791B2 (en) |
EP (1) | EP2627910B1 (en) |
JP (1) | JP6045498B2 (en) |
CN (1) | CN203476797U (en) |
BR (1) | BR112013009031A2 (en) |
DE (1) | DE102010042325A1 (en) |
RU (1) | RU2579800C2 (en) |
WO (1) | WO2012049220A1 (en) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102010062301A1 (en) * | 2010-12-01 | 2012-06-06 | Behr Gmbh & Co. Kg | Axial |
WO2014080494A1 (en) * | 2012-11-22 | 2014-05-30 | 三菱電機株式会社 | Air conditioner |
KR102200395B1 (en) * | 2013-12-12 | 2021-01-08 | 엘지전자 주식회사 | An axial fan and an air conditioner including the same |
DE102014204043A1 (en) * | 2014-03-05 | 2015-09-10 | MAHLE Behr GmbH & Co. KG | Fan wheel of an axial fan |
BR112016026558B1 (en) * | 2014-05-13 | 2022-03-03 | R.E.M. Holding S.R.L | BLADE FOR INDUSTRIAL AXIAL FAN AND INDUSTRIAL AXIAL FAN INCLUDING SUCH BLADE |
US9869190B2 (en) | 2014-05-30 | 2018-01-16 | General Electric Company | Variable-pitch rotor with remote counterweights |
RU2658442C1 (en) * | 2014-08-07 | 2018-06-21 | Мицубиси Электрик Корпорейшн | Axial fan and air conditioning unit with its own axial fan |
DE102014219046A1 (en) | 2014-09-22 | 2016-03-24 | Mahle International Gmbh | fan |
US20160146088A1 (en) * | 2014-11-20 | 2016-05-26 | Jeff Richardson | Cooling Fan Assembly |
US10072510B2 (en) | 2014-11-21 | 2018-09-11 | General Electric Company | Variable pitch fan for gas turbine engine and method of assembling the same |
EP3354904B1 (en) | 2015-04-08 | 2020-09-16 | Horton, Inc. | Fan blade surface features |
USD782639S1 (en) | 2015-06-24 | 2017-03-28 | Mitsubishi Electric Corporation | Propeller fan |
USD797917S1 (en) * | 2015-08-17 | 2017-09-19 | Delta T Corporation | Fan with light |
US10100653B2 (en) | 2015-10-08 | 2018-10-16 | General Electric Company | Variable pitch fan blade retention system |
USD859630S1 (en) * | 2015-11-20 | 2019-09-10 | Kichler Lighting Llc | Ceiling fan |
DE102015224096A1 (en) | 2015-12-02 | 2017-06-08 | Mahle International Gmbh | Fan wheel for an axial fan |
CN105485045A (en) * | 2015-12-24 | 2016-04-13 | 浙江亿利达风机股份有限公司 | Plastic axial impeller |
KR101745904B1 (en) * | 2016-10-19 | 2017-06-13 | 주식회사 한미마이크로닉스 | Cooler fan having double blade |
JP6615379B2 (en) * | 2016-10-27 | 2019-12-04 | 三菱電機株式会社 | Propeller fan, outdoor unit and refrigeration cycle equipment |
CN106640321A (en) * | 2016-12-09 | 2017-05-10 | 重庆道同动力机械设备有限公司 | Heat exchange wind wheel structure of engine |
CN110945250B (en) * | 2017-08-09 | 2021-09-28 | 三菱电机株式会社 | Propeller fan, air supply device, and refrigeration cycle device |
USD860427S1 (en) | 2017-09-18 | 2019-09-17 | Horton, Inc. | Ring fan |
JP6583397B2 (en) * | 2017-12-05 | 2019-10-02 | 株式会社富士通ゼネラル | Propeller fan |
US11767761B2 (en) | 2018-08-02 | 2023-09-26 | Horton, Inc. | Low solidity vehicle cooling fan |
DE102019108676A1 (en) * | 2019-04-03 | 2020-10-08 | Mahle International Gmbh | Fan wheel |
DE102020200652A1 (en) | 2020-01-21 | 2021-07-22 | Mahle International Gmbh | Fan wheel |
US11674435B2 (en) | 2021-06-29 | 2023-06-13 | General Electric Company | Levered counterweight feathering system |
US11795964B2 (en) | 2021-07-16 | 2023-10-24 | General Electric Company | Levered counterweight feathering system |
CN115596706A (en) * | 2022-10-31 | 2023-01-13 | 东风马勒热***有限公司(Cn) | Axial flow fan |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE355646B (en) | 1971-03-30 | 1973-04-30 | Svenska Flaektfabriken Ab | |
US4671739A (en) * | 1980-07-11 | 1987-06-09 | Robert W. Read | One piece molded fan |
DE4020742A1 (en) | 1990-06-29 | 1992-01-02 | Behr Gmbh & Co | IMPELLER FOR A FAN |
RU2124654C1 (en) | 1998-02-06 | 1999-01-10 | Открытое акционерное общество Московский вентиляторный завод | Axial fan impeller |
DE19929978B4 (en) | 1999-06-30 | 2006-02-09 | Behr Gmbh & Co. Kg | Fan with axial blades |
US6375427B1 (en) * | 2000-04-14 | 2002-04-23 | Borgwarner Inc. | Engine cooling fan having supporting vanes |
DE50110684D1 (en) | 2001-01-02 | 2006-09-21 | Behr Gmbh & Co Kg | Fan with axial loops |
WO2002063172A1 (en) * | 2001-02-07 | 2002-08-15 | Denso Corporation | Axial fan for vehicle |
JP4679074B2 (en) | 2004-05-19 | 2011-04-27 | アイシン化工株式会社 | cooling fan |
CN101657619B (en) * | 2007-05-10 | 2012-06-13 | 博格华纳公司 | Synergistic blade and hub structure for cooling fans |
CN201636038U (en) * | 2010-01-12 | 2010-11-17 | 雪龙集团有限公司 | Fan with high efficiency, energy saving and cost lowering |
-
2010
- 2010-10-12 DE DE102010042325A patent/DE102010042325A1/en not_active Withdrawn
-
2011
- 2011-10-12 WO PCT/EP2011/067835 patent/WO2012049220A1/en active Application Filing
- 2011-10-12 BR BR112013009031A patent/BR112013009031A2/en not_active Application Discontinuation
- 2011-10-12 JP JP2013533205A patent/JP6045498B2/en active Active
- 2011-10-12 RU RU2013121573/06A patent/RU2579800C2/en not_active IP Right Cessation
- 2011-10-12 CN CN201190000906.3U patent/CN203476797U/en not_active Expired - Lifetime
- 2011-10-12 EP EP11773440.0A patent/EP2627910B1/en active Active
- 2011-10-12 US US13/879,121 patent/US9447791B2/en active Active
Non-Patent Citations (1)
Title |
---|
None * |
Also Published As
Publication number | Publication date |
---|---|
WO2012049220A1 (en) | 2012-04-19 |
BR112013009031A2 (en) | 2017-10-31 |
CN203476797U (en) | 2014-03-12 |
JP2013539840A (en) | 2013-10-28 |
DE102010042325A1 (en) | 2012-04-12 |
RU2013121573A (en) | 2014-11-20 |
US20130287581A1 (en) | 2013-10-31 |
EP2627910A1 (en) | 2013-08-21 |
US9447791B2 (en) | 2016-09-20 |
RU2579800C2 (en) | 2016-04-10 |
JP6045498B2 (en) | 2016-12-14 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2627910B1 (en) | Fan comprising fan blades | |
EP2646695B1 (en) | Axial fan | |
DE602005003797T2 (en) | axial fan | |
DE60128435T2 (en) | COOLING FAN | |
DE69919970T2 (en) | Axial | |
DE69309180T2 (en) | Fan | |
EP1607573B2 (en) | Compressor blade with reduced aerodynamic vibration induction | |
DE60313147T2 (en) | FAN | |
DE60122323T2 (en) | COOLING FAN WITH FUNNY COAT AND CORRESPONDING SHEET | |
DE112009000367T5 (en) | Cooling fan with partial ring | |
EP1219837B1 (en) | Fan with axial blades | |
DE102011118844B3 (en) | Vertical wind turbine and rotor blade for this | |
DE3137114A1 (en) | AXIAL BLOWERS, ESPECIALLY FOR MOTOR VEHICLES | |
EP2886874A1 (en) | Radial impeller for a drum type ventilator and fan assembly having such a radial impeller | |
DE202004010088U1 (en) | Impeller, in particular for an axial fan | |
EP2466150B1 (en) | Method for manufacturing an impeller for a ventilator | |
WO2017017264A1 (en) | Fan impeller and radiator fan module | |
EP3034886A1 (en) | Blade and fan impeller therewith | |
EP2746534B1 (en) | Stator and/or rotor stage of a turbomachine and corresponding gas turbine | |
EP3067519B1 (en) | Fan blade for a flight drive | |
DE4434598A1 (en) | Radial ventilator for air cooling of small electrical motor for domestic machines and small operating equipment, | |
EP3114354B1 (en) | Fan wheel of an axial fan | |
EP3181911A1 (en) | Kantenberandung eines rotationselements und gebläserad | |
EP2478226B1 (en) | Fan for an internal combustion engine | |
DE102008040698A1 (en) | Fan i.e. axial flow fan, for use as ventilator for cooling electronic device i.e. personal computer, has fan blades whose front edges point in rotational direction of fan wheel, and slat separated from front edge of fan blade by air gap |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
17P | Request for examination filed |
Effective date: 20130513 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
DAX | Request for extension of the european patent (deleted) | ||
RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: MAHLE BEHR GMBH & CO. KG |
|
17Q | First examination report despatched |
Effective date: 20160623 |
|
GRAP | Despatch of communication of intention to grant a patent |
Free format text: ORIGINAL CODE: EPIDOSNIGR1 |
|
INTG | Intention to grant announced |
Effective date: 20170301 |
|
GRAS | Grant fee paid |
Free format text: ORIGINAL CODE: EPIDOSNIGR3 |
|
GRAA | (expected) grant |
Free format text: ORIGINAL CODE: 0009210 |
|
AK | Designated contracting states |
Kind code of ref document: B1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
REG | Reference to a national code |
Ref country code: GB Ref legal event code: FG4D Free format text: NOT ENGLISH |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: EP |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: FG4D Free format text: LANGUAGE OF EP DOCUMENT: GERMAN |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: REF Ref document number: 903230 Country of ref document: AT Kind code of ref document: T Effective date: 20170715 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R096 Ref document number: 502011012491 Country of ref document: DE |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 7 |
|
REG | Reference to a national code |
Ref country code: NL Ref legal event code: MP Effective date: 20170621 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 Ref country code: GR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170922 Ref country code: FI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 Ref country code: NO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170921 Ref country code: HR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 |
|
REG | Reference to a national code |
Ref country code: LT Ref legal event code: MG4D |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: BG Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170921 Ref country code: SE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 Ref country code: RS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 Ref country code: NL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 Ref country code: LV Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 Ref country code: EE Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 Ref country code: RO Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 Ref country code: CZ Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: ES Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 Ref country code: PL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 Ref country code: IT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 Ref country code: IS Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20171021 Ref country code: SM Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 |
|
REG | Reference to a national code |
Ref country code: DE Ref legal event code: R097 Ref document number: 502011012491 Country of ref document: DE |
|
PLBE | No opposition filed within time limit |
Free format text: ORIGINAL CODE: 0009261 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: DK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 |
|
26N | No opposition filed |
Effective date: 20180322 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MC Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 |
|
REG | Reference to a national code |
Ref country code: CH Ref legal event code: PL |
|
GBPC | Gb: european patent ceased through non-payment of renewal fee |
Effective date: 20171012 |
|
REG | Reference to a national code |
Ref country code: IE Ref legal event code: MM4A |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: LU Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171012 Ref country code: CH Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171031 Ref country code: LI Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171031 Ref country code: GB Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171012 |
|
REG | Reference to a national code |
Ref country code: BE Ref legal event code: MM Effective date: 20171031 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: SI Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 Ref country code: BE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171031 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 |
|
REG | Reference to a national code |
Ref country code: FR Ref legal event code: PLFP Year of fee payment: 8 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: IE Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171012 |
|
REG | Reference to a national code |
Ref country code: AT Ref legal event code: MM01 Ref document number: 903230 Country of ref document: AT Kind code of ref document: T Effective date: 20171012 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AT Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20171012 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: FR Payment date: 20181026 Year of fee payment: 8 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: HU Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT; INVALID AB INITIO Effective date: 20111012 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: CY Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20170621 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: MK Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: TR Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: PT Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: AL Free format text: LAPSE BECAUSE OF FAILURE TO SUBMIT A TRANSLATION OF THE DESCRIPTION OR TO PAY THE FEE WITHIN THE PRESCRIBED TIME-LIMIT Effective date: 20170621 |
|
PG25 | Lapsed in a contracting state [announced via postgrant information from national office to epo] |
Ref country code: FR Free format text: LAPSE BECAUSE OF NON-PAYMENT OF DUE FEES Effective date: 20191031 |
|
PGFP | Annual fee paid to national office [announced via postgrant information from national office to epo] |
Ref country code: DE Payment date: 20231020 Year of fee payment: 13 |
|
P01 | Opt-out of the competence of the unified patent court (upc) registered |
Free format text: CASE NUMBER: Effective date: 20240521 |