EP2411311B1 - Device for inputting banknotes into a container, and paddle wheel - Google Patents
Device for inputting banknotes into a container, and paddle wheel Download PDFInfo
- Publication number
- EP2411311B1 EP2411311B1 EP10717071.4A EP10717071A EP2411311B1 EP 2411311 B1 EP2411311 B1 EP 2411311B1 EP 10717071 A EP10717071 A EP 10717071A EP 2411311 B1 EP2411311 B1 EP 2411311B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- paddle
- main body
- wing
- region
- curvature
- 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.)
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- 229920001971 elastomer Polymers 0.000 claims description 6
- 239000000806 elastomer Substances 0.000 claims description 5
- 239000000463 material Substances 0.000 description 7
- 230000015556 catabolic process Effects 0.000 description 3
- 238000006731 degradation reaction Methods 0.000 description 3
- 238000005452 bending Methods 0.000 description 2
- 238000001746 injection moulding Methods 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 229920002725 thermoplastic elastomer Polymers 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 229920006311 Urethane elastomer Polymers 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000018109 developmental process Effects 0.000 description 1
- 230000014759 maintenance of location Effects 0.000 description 1
- 239000004814 polyurethane Substances 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H29/00—Delivering or advancing articles from machines; Advancing articles to or into piles
- B65H29/38—Delivering or advancing articles from machines; Advancing articles to or into piles by movable piling or advancing arms, frames, plates, or like members with which the articles are maintained in face contact
- B65H29/40—Members rotated about an axis perpendicular to direction of article movement, e.g. star-wheels formed by S-shaped members
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H29/00—Delivering or advancing articles from machines; Advancing articles to or into piles
- B65H29/20—Delivering or advancing articles from machines; Advancing articles to or into piles by contact with rotating friction members, e.g. rollers, brushes, or cylinders
- B65H29/22—Delivering or advancing articles from machines; Advancing articles to or into piles by contact with rotating friction members, e.g. rollers, brushes, or cylinders and introducing into a pile
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H31/00—Pile receivers
- B65H31/26—Auxiliary devices for retaining articles in the pile
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H2404/00—Parts for transporting or guiding the handled material
- B65H2404/10—Rollers
- B65H2404/11—Details of cross-section or profile
- B65H2404/111—Details of cross-section or profile shape
- B65H2404/1114—Paddle wheel
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H2404/00—Parts for transporting or guiding the handled material
- B65H2404/10—Rollers
- B65H2404/14—Roller pairs
- B65H2404/141—Roller pairs with particular shape of cross profile
- B65H2404/1413—Paddle / cylindrical
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B65—CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
- B65H—HANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
- B65H2701/00—Handled material; Storage means
- B65H2701/10—Handled articles or webs
- B65H2701/19—Specific article or web
- B65H2701/1912—Banknotes, bills and cheques or the like
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S902/00—Electronic funds transfer
- Y10S902/08—Terminal* with means permitting deposit or withdrawal, e.g. ATM
- Y10S902/17—Terminal* with means permitting deposit or withdrawal, e.g. ATM with particular feeder or counter feature
Definitions
- the invention relates to a device for entering notes of value in a container.
- the apparatus comprises a feed unit for feeding the notes of value and a stack unit for stacking the supplied notes of value.
- the device has at least one impeller for handling the notes of value.
- the impeller comprises a rotatably mounted base body and at least one wing fixedly connected to a first end of a connecting region with the main body.
- the wing has a pressure area for applying a force to at least one banknote.
- the invention can be used in particular in connection with ATMs, automatic cash deposits and / or automatic cash register systems, into which banknotes, preferably banknotes, are paid.
- the deposited banknotes are stored in a receiving area of the container in the form of a stack.
- the notes of value are fed to the receiving area individually and stacked in the receiving area in such a way that a note of value to be supplied is fed to an already existing stack on its end face.
- the front or back side of the banknote to be supplied and the front or back side of the banknote immediately before the banknote supplied note of value are arranged opposite one another.
- the impeller presses the last-added note against the stack.
- the device is constructed such that the blades of the impeller at a rotation of the impeller are strongly curved by the contact with adjacent elements.
- a banknote deposit and bill dispenser with a top holding unit for banknotes and a bottom holding unit for banknotes for holding and transporting the banknotes in a banknote stacking direction or in the counterstacking direction.
- the upper portion of an upright banknote is held by the upper holding unit.
- the lower portion of the upright banknote is held by the lower holding unit.
- the holding units are, in particular, impellers with a base body and vanes arranged radially relative to the base body. Due to the radial connection of the wings to the base body, the wings are bent comparatively strongly by the contact with adjacent elements, ie the curvature of the wing has a small radius of curvature.
- the wings are stressed due to the strong curvature and the high stiffness required for holding the notes of value with high voltages. This can lead to material fatigue, in particular to a reduction in rigidity and stress relaxation. This, in turn, the proper function of the impeller is no longer guaranteed.
- each wing comprises a pressure area and a support area. It is an object of the invention to provide a device for entering notes of value in a container with an impeller for handling bank notes, in which the wing of the impeller is claimed with a low uniform voltage.
- the impeller for handling banknotes comprises a rotatably mounted base body and at least one at a first end of a connecting portion fixedly connected to the main body wings.
- the wing has a pressure area for applying a force to at least one bank note and a support area.
- the support area contacts the lateral surface of the base body when the wing exerts a force on a bank note. It is advantageous if the wing essentially only exerts a force on the note of value if at least part of the support area of the wing contacts the base body.
- the wing does not contact the base body, at least in one region, when the wing exerts a force on the security note and the support region contacts the lateral surface of the base body. It is particularly advantageous if the support region of the wing, when it exerts no force on a banknote, runs substantially parallel to a tangent to the base body in a first position.
- the connection point at which the wing is connected to the base body is arranged at a preset angle of ⁇ 45 ° before the first point.
- the joint is in particular arranged at an angle in the range between 10 ° and 30 ° before the first point. Such an arrangement of the wing is also referred to as the previous connection of the wing.
- the connection region is placed radially on the lateral surface of the base body.
- the impeller is produced in particular by means of an injection molding process. As a result, a cost-effective production of the impeller is achieved.
- the main body is preferably a hub rotatably mounted about its longitudinal axis.
- the impeller can be easily mounted rotatably on a shaft and rotated by a rotation of the shaft.
- the impeller comprises two wings.
- the wings are arranged offset by 180 °. This ensures that a value-added stack accommodated in a receiving area of a container is reliably pressed into the receiving area with the aid of the impeller, so that a free supply area is produced for positioning a further banknote to be supplied and stacked.
- the impeller may also comprise more than two wings, in particular three or four wings.
- the wing when exerting a force on a value note on a curvature counter to the direction of rotation of the impeller.
- the wing is sufficiently elastic. In this way, it is achieved that the wing can be bent non-destructively in contact with arranged in the radius of the wing elements.
- the impeller is for this purpose in particular made of an elastomer, preferably a non-crosslinked elastomer.
- the center of curvature of the curvature of the wing lies in a through the lateral surface of the basic body limited space. The center of curvature of the curvature is preferably on the axis of rotation of the body.
- the support region of the wing rests optimally on the lateral surface of the main body, and, on the other hand, that the curvature of the wing has a large radius of curvature. Due to the large radius of curvature in turn, the wing is stressed with a lower voltage.
- the wing at the end facing away from the main body has a counter curvature, so that compensated by the contact of the support area with the lateral surface of the body resulting backward inclination of the wing against the direction of rotation of the body or at least reduced. This ensures that the wing can exert a sufficiently large force on the banknote over the contact area.
- the wing preferably has an S-shaped area.
- Fig. 1 is a schematic representation of a known embodiment of an impeller 10a shown.
- the impeller 10a is used in particular in ATMs, automatic cash register systems and / or automatic cash deposits, into which banknotes are deposited and stacked in banknote acceptor areas.
- the notes of value are fed to the Wertscheinreawitz individually and stored in this standing on one of its long sides in a stacked form.
- the notes of value of the value note stack already received in the value acceptance area are pressed by means of the impeller 10a against a pressure wall limiting the value acceptance area, so that a free supply area is formed, in which the value note to be deposited next in the value acceptance area can be supplied to the value acceptance area. This avoids that an added value note canted during feeding with the notes of the value note stack and thus a correct stacking of the notes of value can not be guaranteed.
- the impeller 10a comprises a hollow cylindrical main body 12a and two wings 14a, 16a fixedly connected to the main body 12a.
- the main body 12a is designed in particular as a hub.
- the wings 14a, 16a are also referred to as paddles.
- the main body 12a is rotatable and stationary with an in Fig. 1 connected shaft shown connected 18, that the longitudinal axis of the main body 12a and the longitudinal axis of the shaft 18 coincide.
- the impeller 10a rotates in the direction of rotation P1.
- the vanes 14a, 16a are connected at a first end of a connecting region 20a, 22a to the main body 12a such that the longitudinal axis of the respective connecting region 20a, 22a is arranged in each case radially to the main body 12a.
- This radial arrangement of the wings 14a, 16a is also referred to as a radial connection.
- each wing 14a, 16a at least one pressure area 24a, 26a, with which the wing 14a, 16a presses against the stacked in the Wertscheinarea Scheme Wertscheinstapel last fed value note and thus exerts a force on this note and thus on the existing stack to to produce the feed opening for supplying another note of value.
- the wings 14a, 16a In order to exert sufficient force on the last note of the value note stack, the wings 14a, 16a must have a high rigidity. Furthermore, the drive unit with which the shaft 18 and thus also the impeller 10 a are driven, must generate a sufficiently high torque. At the in Fig. 1 Not The drive unit shown is in particular a stepper motor.
- Fig. 1 two adjacent elements 28, 30 are shown.
- the adjoining elements 28, 30 are, in particular, shafts or rods which are in Fig. 1 are also shown cut.
- the vanes 14a, 16a of the impeller 10a are strongly bent in rotation of the impeller 10a in the direction of rotation P1 by the contact with the adjacent elements 28, 30.
- the wing 16a is in Fig. 1 shown in a position in which it is bent by the contact with the first adjacent element 28.
- a strong curvature of the wing 16a is generated.
- a strong curvature is a curvature with a small radius of curvature or with small radii of curvature.
- the drive unit for driving the shaft 18 In order to apply the least necessary force even with decreasing stiffness, the drive unit for driving the shaft 18 must drive it at a higher speed.
- the uneven curvature of the wing 16a causes a likewise uneven stress distribution over the wing 16a. As a result, voltage peaks can result, which can lead to damage to the wing 16a.
- the impeller 10a after Fig. 1 is the enveloping circle of the curved wings 14, 16 represented by the circles 34, 36.
- the outer circle 34 indicates the enveloping circle of that surface of the wing 16a, which is seen in the direction of rotation P1, arranged at the front.
- the circle 36 indicates the envelope of the rear surface of the wing 16a.
- FIG. 2 is a schematic representation of a further developed embodiment of an impeller 10b shown. Elements with the same structure or the same function have the same reference numerals.
- the longitudinal axes of the connecting portions 20b, 22b of the wings 14b, 16b are neither orthogonal nor parallel to a tangent to a main body 12b in the respective connection points at which the wings 14b, 16b are connected to the main body 12b.
- the wings 14b, 16b are thus connected neither radially nor tangentially to the main body 12b.
- each wing 14b, 16b comprises at least one pressure region 24b, 26b.
- the curvature region of the wing 16b is designated by the reference numeral 32b. Due to the lower curvature, ie by a curvature having a larger radius of curvature, the stresses occurring in the vanes 14b, 16b are lower than the stresses which occur in the vanes 14a, 16a in the radial connection of the vanes 14a, 16a.
- the enveloping circle resulting in connection of the wings 14b, 16b has a radius which is approximately 90% of the radius of the enveloping circle, which is determined by the radial connection of the wings 14a, 16a Fig. 1 results.
- FIG. 3 is a schematic representation of an embodiment according to the invention of an impeller 10c shown.
- Fig. 4 is a schematic perspective view of the impeller 10c after Fig. 3 shown.
- the impeller 10c includes two blades 14c, 16c.
- the force exerted by the last note of value of the note stack on the wing 14c when the note is pressed by means of the wing 14c is in Figure 3 represented by the arrow P2.
- the wings 14c, 16c each include a support portion 38, 40, which contacts the lateral surface of a base body 12c, when the respective wing 14c, 16c exerts a force on the last note of the value note stack via a contact area 24c, 26c.
- the wing 14c, 16c thus bears against the base body 12c and is supported by the base body 12c.
- the force P2 exerted by the note of value on the wings 14c, 16 is transferred over a larger area from the wing 14c, 16c to the base body 12c, so that the occurring stresses are lower.
- the wing 14c, 16c is in particular on an even larger area on the base body 12c, the greater the force P2 exerted on the wing 14c, 16c.
- the wing 14c is designed in such a way that the wing 14c does not contact the base body 12c in at least one area 42 when the wing 14c exerts a force on the last value note of the value note stack.
- the vane 16c is analogous to the vane 14c, so the embodiments described for the vane 14c corresponding to the vane 16c and the vices described for the vane 16c apply mutatis mutandis to the vane 14c.
- the gap which is present in the unloaded state between the wing 14c, 16c and the base body 12c, should be as small as possible, so that the wing 14c, 16c rests quickly on contact with a banknote on the base body 12c.
- the unloaded state is the state in which the wing 14c, 16c exerts no force on a bank note and the wing 14c, 16c is not bent by adjacent elements 28, 30.
- the wing 14 c is formed such that the support portion 38 extends parallel to a tangent to the base body 12 c at a first location 44.
- the connection point 46 between the wing 14c and the main body 12c is seen in the direction of rotation P1 of the main body 12c at an angle in front of the first location 44.
- this angle has a value in the range between 0 ° and 45 °, preferably in the range between 10 ° and 30 °. This ensures that the wing 14c is longer and thus softer compared to a wing that is tangentially connected to the base body 12c at the first location 44.
- Such a soft wing 14c is stressed during the stress with an equal force with lower mechanical stresses than the shorter tangentially connected wing.
- connection point 46 Between the longitudinal axis of a connecting region 20c of the wing 14c and a tangent to the base body 12c at the connection point 46 is an angle in the range between 70 ° and 110 °. In a preferred embodiment of the invention, the angle is about 90 °, so that the connecting portion 20c of the wing 14c is radially connected to the main body 12c.
- the wing 14c is formed such that between the support portion 38 and the connecting portion 20c in the unloaded state of the wing 14c an angle in the range between 70 ° and 110 °, preferably an angle of about 90 °. This ensures that the connecting portion 20c of the wing 14c protrudes radially from the main body 12c and the support portion 38 of the wing 14c nevertheless runs parallel to a tangent to the main body 12c in the first position 44.
- a transition region between the support region 38 and the connection region 20c is preferably opposed the direction of rotation P1 curved, in particular formed in the form of a radius.
- Fig. 3 and 4 shown and previously described shape and connection of the wings 14c, 16c is also referred to as the previous connection of the wings 14c, 16c. Due to the previous connection of the wings 14c, 16c it is achieved that the enveloping circle resulting from the contact with the adjacent elements 28, 30 is substantially smaller than the enveloping circle 34, 36 at the radial connection of the wings 14a, 16a.
- the resulting envelope is in Fig. 3 not shown and in particular has a radius which is only about 70% of the radius, which results in the radial connection of the wings 14a, 16a.
- the enveloping circles 34, 36 which result in the radial connection of the wings 14a, 16a, shown. Due to the much smaller enveloping circle, a more compact design of the device in which the impeller 10c is used is possible with the same load on the impeller 10c.
- the engagement of the wings 14c, 16c is achieved by the wing 16c being less curved by contact with the adjacent element 28, so that the radius of curvature compared to the radii of curvature in the embodiments of the vanes 10a, 10b after the Fig. 1 and 2 is larger.
- the center of the radius of curvature is disposed near the longitudinal axis of the main body 12c.
- the center of curvature lies on the longitudinal axis of the main body 12c. This in turn ensures that the stresses with which the wings 14c, 16c are claimed, lower are, and thus the material fatigue, in particular the degradation of the rigidity of the wings 14c, 16c, are reduced.
- a uniform voltage curve over the wing 14c, 16c is achieved by the uniform curvature and thus the occurrence of local stress peaks and possible damage to the impeller 10c avoided or reduced.
- a connecting portion 20c, 22c of the wing 14c, 16c, at the end of which the wing 14c, 16c is connected to the base body 12c is relieved by supporting the wing 14c, 16c with the support portion 38, 40 on the base body 12c.
- the wings 14c, 16c are in particular designed in such a way that the wing 14c, 16c only exerts a force on a security note when the support area 38, 40 at least partially rests against the base body 12c.
- the wing 14c comprises a counterbending area 48, which is curved in such a way that the end of the wing 14c, which is not connected to the main body 12c, points in the direction of rotation P1.
- a counterbending area 48 which is curved in such a way that the end of the wing 14c, which is not connected to the main body 12c, points in the direction of rotation P1.
- the wings 14c, 16c and the main body 12c are in particular formed in one piece.
- the impeller 10c is advantageously made of an uncrosslinked elastomer, in particular of polyurethane (PU), of a thermoplastic elastomer (TPE) or of polyester-urethane rubber (Vulkollan®), and is produced, for example, by injection molding.
- the impeller 10c may also be made of crosslinked elastomers.
- the wings 14c, 16c of the impeller 10c are arranged offset by 180 °.
- the wings 14c, 16c may also be offset from each other by an angle other than 180 °.
- less than two wings 14c, 16c may be provided.
- the impeller 10c may have only one blade 14c, 16c, which embodiment is not covered by the claims, or four blades 14c, 16c which are offset by 90 °.
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Description
Die Erfindung betrifft eine Vorrichtung zur Eingabe von Wertscheinen in einen Behälter. Die Vorrichtung umfasst eine Zuführeinheit zum Zuführen der Wertscheine und eine Stapeleinheit zum Stapeln der zugeführten Wertscheine. Ferner hat die Vorrichtung mindestens ein Flügelrad zur Handhabung der Wertscheine. Das Flügelrad wiederum umfasst einen drehbar gelagerten Grundkörper und mindestens einen mit einem ersten Ende eines Verbindungsbereiches fest mit dem Grundkörper verbundenen Flügel. Der Flügel hat einen Andruckbereich zum Ausüben einer Kraft auf mindestens einen Wertschein.The invention relates to a device for entering notes of value in a container. The apparatus comprises a feed unit for feeding the notes of value and a stack unit for stacking the supplied notes of value. Furthermore, the device has at least one impeller for handling the notes of value. In turn, the impeller comprises a rotatably mounted base body and at least one wing fixedly connected to a first end of a connecting region with the main body. The wing has a pressure area for applying a force to at least one banknote.
Die Erfindung kann insbesondere in Verbindung mit Geldautomaten, automatischen Tresorkassen und/oder automatischen Kassensystemen eingesetzt werden, in die Wertscheine, vorzugsweise Banknoten, eingezahlt werden. Die eingezahlten Wertscheine werden in einem Aufnahmebereich des Behälters in Form eines Stapels abgelegt. Die Wertscheine werden dem Aufnahmebereich einzeln zugeführt und in dem Aufnahmebereich derart gestapelt, dass ein zuzuführender Wertschein einem bereits vorhandenen Stapel an seiner Stirnseite zugeführt wird. Die Vorder- oder Rückseite des zuzuführenden Wertscheins und die Vorder- oder Rückseite des dem Stapel unmittelbar zuvor zugeführten Wertscheins sind gegenüberliegend angeordnet. Das Flügelrad drückt den als letztes zugeführten Wertschein gegen den Stapel. Um eine kompakte Bauweise der Vorrichtung zu gewährleisten, ist die Vorrichtung derart aufgebaut, dass die Flügel des Flügelrades bei einer Drehung des Flügelrades durch den Kontakt mit angrenzenden Elementen stark gekrümmt werden.The invention can be used in particular in connection with ATMs, automatic cash deposits and / or automatic cash register systems, into which banknotes, preferably banknotes, are paid. The deposited banknotes are stored in a receiving area of the container in the form of a stack. The notes of value are fed to the receiving area individually and stacked in the receiving area in such a way that a note of value to be supplied is fed to an already existing stack on its end face. The front or back side of the banknote to be supplied and the front or back side of the banknote immediately before the banknote supplied note of value are arranged opposite one another. The impeller presses the last-added note against the stack. In order to ensure a compact design of the device, the device is constructed such that the blades of the impeller at a rotation of the impeller are strongly curved by the contact with adjacent elements.
Aus dem Dokument
Aus dem Dokument
Diese Aufgabe wird durch eine Vorrichtung mit den Merkmalen des Patentanspruchs 1 gelöst. Vorteilhafte Weiterbildungen der Erfindung sind in den abhängigen Patentansprüchen angegeben.This object is achieved by a device having the features of patent claim 1. Advantageous developments of the invention are specified in the dependent claims.
Durch den Kontakt zwischen dem Stützbereich des Flügels und der Mantelfläche des Grundkörpers beim Ausüben einer Kraft auf einen Wertschein durch den Flügel wird erreicht, dass zumindest ein Teil des Stützbereiches an dem Grundkörper anliegt und somit der Flügel durch den Grundkörper gestützt wird. Dies bewirkt, dass die Kraft, die der Flügel auf den Wertschein ausübt, über eine große Fläche vom Flügel auf den Grundkörper übertragen wird. Ferner wird durch das Anliegen des Stützbereiches des Flügels am Grundkörper erreicht, dass der Flügel mit nur einer geringen Krümmung, d. h. einer Krümmung mit einem großen Krümmungsradius, elastisch verformt wird. Dies bewirkt, dass der Flügel, verglichen mit einer radialen Anordnung des Flügels an den Grundkörper, mit einer wesentlich geringeren mechanischen Spannung beansprucht und eine gleichmäßige Spannungsverteilung erreicht wird. Insbesondere wird das Auftreten von Spannungsspitzen, insbesondere im Verbindungsbereich, vermieden oder zumindest reduziert. Hierdurch wiederum wird eine Materialermüdung verhindert bzw. abgeschwächt, so dass die Reduzierung der Steifigkeit und der Spannungsabbau des Flügels im Laufe der Lebensdauer des Flügels reduziert wird und somit eine ausreichend hohe Kraft, die von dem Flügel auf den Wertschein ausgeübt wird, gewährleistet ist. Das Flügelrad zur Handhabung von Wertscheinen umfasst einen drehbar gelagerten Grundkörper und mindestens einen an einem ersten Ende eines Verbindungsbereiches fest mit dem Grundkörper verbundenen Flügel. Der Flügel hat einen Andruckbereich zum Ausüben einer Kraft auf mindestens einen Wertschein und einen Stützbereich. Der Stützbereich kontaktiert die Mantelfläche des Grundkörpers, wenn der Flügel eine Kraft auf einen Wertschein ausübt. Es ist vorteilhaft, wenn der Flügel im Wesentlichen erst dann eine Kraft auf den Wertschein ausübt, wenn zumindest ein Teil des Stützbereiches des Flügels den Grundkörper kontaktiert.By the contact between the support region of the wing and the lateral surface of the base body when exerting a force on a note of value by the wing is achieved that at least a part of the support region bears against the base body and thus the wing is supported by the base body. This causes the force exerted by the wing on the banknote to be transferred over a large area from the wing to the base body. Furthermore, it is achieved by the concern of the support region of the wing on the base body, that the wing with only a slight curvature, ie a curvature with a large radius of curvature, is elastically deformed. This causes the wing, compared with a radial arrangement of the wing to the body, claimed with a much lower mechanical stress and a uniform stress distribution is achieved. In particular, the occurrence of voltage peaks, in particular in the connection region, is avoided or at least reduced. This, in turn, prevents or mitigates material fatigue so that the reduction in stiffness and stress relief of the blade is reduced over the life of the blade, thus ensuring a sufficiently high force exerted by the blade on the banknote. The impeller for handling banknotes comprises a rotatably mounted base body and at least one at a first end of a connecting portion fixedly connected to the main body wings. The wing has a pressure area for applying a force to at least one bank note and a support area. The support area contacts the lateral surface of the base body when the wing exerts a force on a bank note. It is advantageous if the wing essentially only exerts a force on the note of value if at least part of the support area of the wing contacts the base body.
Des Weiteren ist es vorteilhaft, wenn zwischen dem Verbindungsbereich und dem Stützbereich der Flügel den Grundkörper zumindest in einem Bereich nicht kontaktiert, wenn der Flügel eine Kraft auf den Wertschein ausübt und der Stützbereich die Mantelfläche des Grundkörpers kontaktiert. Es ist besonders vorteilhaft, wenn der Stützbereich des Flügels, wenn dieser keine Kraft auf einen Wertschein ausübt, im Wesentlichen parallel zu einer Tangente an den Grundkörper in einer ersten Stelle verläuft. Die Verbindungsstelle, an der der Flügel mit dem Grundkörper verbunden ist, ist um einen voreingestellten Winkel von <45° vor der ersten Stelle angeordnet. Die Verbindungsstelle ist insbesondere um einen Winkel im Bereich zwischen 10° und 30° vor der ersten Stelle angeordnet. Eine solche Anordnung des Flügels wird auch als zurückliegende Anbindung des Flügels bezeichnet. Durch die zurückliegende Anbindung des Flügels an den Grundkörper wird erreicht, dass der Flügel verglichen mit einer tangentialen Anbindung des Flügels an der ersten Stelle länger ist und somit bei gleichem Querschnitt weicher ist. Somit treten bei einer Krümmung des Flügels nur relativ geringe mechanische Spannungen auf, so dass einer Materialermüdung vorgebeugt wird. Durch das Anliegen des Flügels an dem Grundkörper, wenn der Flügel eine Kraft auf einen Wertschein ausübt, wird trotz des weicheren Flügels sichergestellt, dass eine ausreichend große Kraft auf den Wertschein ausgeübt wird.Furthermore, it is advantageous if, between the connection region and the support region, the wing does not contact the base body, at least in one region, when the wing exerts a force on the security note and the support region contacts the lateral surface of the base body. It is particularly advantageous if the support region of the wing, when it exerts no force on a banknote, runs substantially parallel to a tangent to the base body in a first position. The connection point at which the wing is connected to the base body is arranged at a preset angle of <45 ° before the first point. The joint is in particular arranged at an angle in the range between 10 ° and 30 ° before the first point. Such an arrangement of the wing is also referred to as the previous connection of the wing. By the previous connection of the wing to the base body is achieved that the wing is longer compared to a tangential connection of the wing at the first point and thus softer with the same cross-section. Thus, with a curvature of the wing only Relatively low mechanical stresses, so that a material fatigue is prevented. Due to the wing's presence on the base body, when the wing exerts a force on a security note, it is ensured, despite the softer wing, that a sufficiently large force is exerted on the security note.
Bei einer bevorzugten Ausführungsform der Erfindung ist zwischen der Längsachse des Verbindungsbereiches des Flügels und einer Tangente an den Grundkörper in der Verbindungsstelle ein Winkel im Bereich zwischen 70° und 100°. Bei einer besonders bevorzugten Ausführungsform der Erfindung ist der Verbindungsbereich radial auf der Mantelfläche des Grundkörpers aufgesetzt. Ferner ist es vorteilhaft, wenn in einem unbelasteten Zustand des Flügels zwischen dem Verbindungsbereich und dem Stützbereich ein Winkel zwischen 70° und 110°, insbesondere ein Winkel von etwa 90°, ist. Der unbelastete Zustand des Flügels ist derjenige Zustand, in dem der Flügel keine Kraft auf einen Wertschein ausübt und nicht durch den Kontakt mit einem angrenzenden Element verformt wird. Ein Übergangbereich zwischen dem Stützbereich und dem ist vorzugsweise gekrümmt, insbesondere in Form eines Radius ausgebildet.In a preferred embodiment of the invention, an angle in the range between 70 ° and 100 ° between the longitudinal axis of the connecting portion of the wing and a tangent to the body in the joint. In a particularly preferred embodiment of the invention, the connection region is placed radially on the lateral surface of the base body. Furthermore, it is advantageous if in an unloaded state of the wing between the connection region and the support region an angle between 70 ° and 110 °, in particular an angle of about 90 °, is. The unloaded state of the wing is that state in which the wing exerts no force on a note and is not deformed by contact with an adjacent element. A transition region between the support region and that is preferably curved, in particular in the form of a radius.
Auf diese Weise ist die zurückliegende Anbindung des Flügels an den Grundkörper auf einfache Weise herstellbar und das Flügelrad ist einfach und kostengünstig zu fertigen.In this way, the past connection of the wing to the body in a simple manner and the impeller is easy and inexpensive to manufacture.
Ferner ist es vorteilhaft, den Grundkörper und den Flügel einteilig auszubilden. Das Flügelrad wird insbesondere mittels eines Spritzgussverfahrens hergestellt. Hierdurch wird eine kostengünstige Fertigung des Flügelrades erreicht.Furthermore, it is advantageous to form the main body and the wing in one piece. The impeller is produced in particular by means of an injection molding process. As a result, a cost-effective production of the impeller is achieved.
Der Grundkörper ist vorzugsweise ein um ihre Längsachse drehbar gelagerte Nabe. Hierdurch kann das Flügelrad einfach auf einer Welle drehfest gelagert werden und durch eine Rotation der Welle in Rotation versetzt werden. Gemäß der Erfindung umfasst das Flügelrad zwei Flügel. Die Flügel sind um 180° versetzt angeordnet. Hierdurch wird sichergestellt, dass ein in einem Aufnahmebereich eines Behälters aufgenommener Wertscheinstapel zuverlässig mit Hilfe des Flügelrades in den Aufnahmebereich hineingedrückt wird, so dass ein freier Zuführbereich zum Positionieren eines weiteren zuzuführenden und zu stapelnden Wertscheins erzeugt wird. Bei einer alternativen Ausführungsform der Erfindung kann das Flügelrad auch mehr als zwei Flügel, insbesondere drei oder vier Flügel, umfassen. Erfindungsgemäß weist zumindest ein Teil des Flügels beim Ausüben einer Kraft auf einen Wertschein eine Krümmung entgegen der Drehrichtung des Flügelrades auf. Hierzu ist der Flügel ausreichend elastisch ausgebildet. Auf diese Weise wird erreicht, dass der Flügel bei dem Kontakt mit im Radius des Flügels angeordneten Elementen zerstörungsfrei umgebogen werden kann. Das Flügelrad ist hierzu insbesondere aus einem Elastomer, vorzugsweise einem unvernetzten Elastomer, hergestellt. Erfindungsgemäß liegt der Krümmungsmittelpunkt der Krümmung des Flügels in einem durch die Mantelfläche des Grundkörpers begrenzten Raum. Der Krümmungsmittelpunkt der Krümmung liegt vorzugsweise auf der Drehachse des Grundkörpers. Hierdurch wird zum einen erreicht, dass der Stützbereich des Flügels optimal auf der Mantelfläche des Grundkörpers aufliegt, und zum anderen, dass die Krümmung des Flügels einen großen Krümmungsradius hat. Durch den großen Krümmungsradius wiederum wird der Flügel mit einer geringeren Spannung beansprucht.The main body is preferably a hub rotatably mounted about its longitudinal axis. As a result, the impeller can be easily mounted rotatably on a shaft and rotated by a rotation of the shaft. According to the invention, the impeller comprises two wings. The wings are arranged offset by 180 °. This ensures that a value-added stack accommodated in a receiving area of a container is reliably pressed into the receiving area with the aid of the impeller, so that a free supply area is produced for positioning a further banknote to be supplied and stacked. In an alternative embodiment of the invention, the impeller may also comprise more than two wings, in particular three or four wings. According to the invention, at least a part of the wing when exerting a force on a value note on a curvature counter to the direction of rotation of the impeller. For this purpose, the wing is sufficiently elastic. In this way, it is achieved that the wing can be bent non-destructively in contact with arranged in the radius of the wing elements. The impeller is for this purpose in particular made of an elastomer, preferably a non-crosslinked elastomer. According to the invention, the center of curvature of the curvature of the wing lies in a through the lateral surface of the basic body limited space. The center of curvature of the curvature is preferably on the axis of rotation of the body. This achieves, on the one hand, that the support region of the wing rests optimally on the lateral surface of the main body, and, on the other hand, that the curvature of the wing has a large radius of curvature. Due to the large radius of curvature in turn, the wing is stressed with a lower voltage.
Darüber hinaus ist es vorteilhaft, wenn der Flügel an dem dem Grundkörper abgewandten Ende eine Gegenkrümmung aufweist, so dass sich die durch den Kontakt des Stützbereiches mit der Mantelfläche des Grundkörpers ergebende Rückwärtsneigung des Flügels entgegen der Drehrichtung des Grundkörpers ausgeglichen oder zumindest reduziert wird. Hierdurch wird sichergestellt, dass der Flügel über den Andruckbereich eine ausreichend große Kraft auf den Wertschein ausüben kann. Hierzu hat der Flügel vorzugsweise einen S-förmig ausgebildeten Bereich.Moreover, it is advantageous if the wing at the end facing away from the main body has a counter curvature, so that compensated by the contact of the support area with the lateral surface of the body resulting backward inclination of the wing against the direction of rotation of the body or at least reduced. This ensures that the wing can exert a sufficiently large force on the banknote over the contact area. For this purpose, the wing preferably has an S-shaped area.
Weitere Merkmale und Vorteile der Erfindung ergeben sich aus der folgenden Beschreibung, welche in Verbindung mit den beigefügten Figuren die Erfindung anhand von Ausführungsbeispielen näher erläutert.Further features and advantages of the invention will become apparent from the following description which, in conjunction with the accompanying figures, the invention with reference to embodiments explained in more detail.
Es zeigen:
- Fig. 1
- eine schematische Darstellung einer bekannten Ausführungsform eines Flügelrades;
- Fig. 2
- eine schematische Darstellung einer weiterentwickelten Ausführungsform eines Flügelrades;
- Fig. 3
- eine schematische Darstellung einer erfindungsgemäßen Ausführungsform eines Flügelrades; und
- Fig. 4
- eine schematische perspektivische Darstellung des Flügelrades nach
Fig. 3 .
- Fig. 1
- a schematic representation of a known embodiment of an impeller;
- Fig. 2
- a schematic representation of a further developed embodiment of an impeller;
- Fig. 3
- a schematic representation of an embodiment of an impeller according to the invention; and
- Fig. 4
- a schematic perspective view of the impeller after
Fig. 3 ,
In
Das Flügelrad 10a umfasst einen hohlzylindrischen Grundkörper 12a und zwei fest mit dem Grundkörper 12a verbundene Flügel 14a, 16a. Der Grundkörper 12a ist insbesondere als Nabe ausgebildet. Die Flügel 14a, 16a werden auch als Paddel bezeichnet.The
Der Grundkörper 12a ist derart dreh- und ortsfest mit einer in
Die Flügel 14a, 16a sind an einem ersten Ende eines Verbindungsbereiches 20a, 22a derart mit dem Grundkörper 12a verbunden, dass die Längsachse des jeweiligen Verbindungsbereiches 20a, 22a jeweils radial zum Grundkörper 12a angeordnet ist. Diese radiale Anordnung der Flügel 14a, 16a wird auch als radiale Anbindung bezeichnet. Ferner umfasst jeder Flügel 14a, 16a mindestens einen Andruckbereich 24a, 26a, mit dem der Flügel 14a, 16a gegen den den im Wertscheinaufnahmebereich gestapelten Wertscheinstapel als letztes zugeführten Wertschein drückt und somit eine Kraft auf diesen Wertschein und somit auch auf den vorhandenen Stapel ausübt, um die Zuführöffnung zum Zuführen eines weiteren Wertscheins zu erzeugen. Um eine ausreichende Kraft auf den letzten Wertschein des Wertscheinstapels auszuüben, müssen die Flügel 14a, 16a eine hohe Steifigkeit haben. Ferner muss die Antriebseinheit, mit der die Welle 18 und somit auch das Flügelrad 10a angetrieben werden, ein ausreichend hohes Drehmoment erzeugen. Bei der in
Ferner sind in
Durch die starke Krümmung des Flügels 16a treten in dem Flügel 16a, insbesondere in dem Verbindungsbereich 22a große Spannungen, insbesondere große Randspannungen, auf. Durch die hohe Steifigkeit des Flügels 16a sind die auftretenden Spannungen besonders groß. Die hohen auftretenden Spannungen führen im Laufe des Betriebes des Flügelrades 10a zu einer Materialermüdung. Insbesondere bewirken die hohen auftretenden Spannungen einen starken Abbau der Steifigkeit der Flügel 14a, 16a und somit einem starken Spannungsabbau. Dies wiederum kann dazu führen, dass durch die Flügel 14a, 16a nicht mehr die mindestens notwendige Kraft auf den letzten Wertschein des Wertscheinstapels ausgeübt wird und somit ein sicheres Zurückhalten der Wertscheine des Wertscheinstapels nicht mehr gewährleistet ist. Ferner kann die Materialermüdung zum Versagen des Flügelrades 10a führen. Um auch bei nachlassender Steifigkeit die mindestens notwendige Kraft aufzubringen, muss die Antriebseinheit zum Antrieb der Welle 18 diese mit einer höheren Drehzahl antreiben. Die ungleichmäßige Krümmung des Flügels 16a bewirkt eine ebenfalls ungleichmäßige Spannungsverteilung über den Flügel 16a. Hierdurch können sich Spannungsspitzen ergeben, die zu Schädigungen des Flügels 16a führen können.Due to the strong curvature of the
Bei der Ausführungsform des Flügelrades 10a nach
In
Durch die nicht radiale Anbindung der Flügel 14b, 16b an den Grundkörper 12b des Flügelrades 10b werden die Flügel 14b, 16b durch den Kontakt mit den angrenzenden Elementen 28, 30 weniger stark umgebogen als die Flügel 14a, 16a des Flügelrades 10a nach
In
Die Flügel 14c, 16c umfassen jeweils einen Stützbereich 38, 40, der die Mantelfläche eines Grundkörpers 12c kontaktiert, wenn der jeweilige Flügel 14c, 16c über einen Andruckbereich 24c, 26c eine Kraft auf den letzten Wertschein des Wertscheinstapels ausübt. Der Flügel 14c, 16c liegt somit an dem Grundkörper 12c an und wird vom Grundkörper 12c abgestützt. Hierdurch wird die von dem Wertschein auf den Flügel 14c, 16 ausgeübte Kraft P2 über eine größere Fläche von dem Flügel 14c, 16c auf den Grundkörper 12c übertragen, so dass die auftretenden Spannungen geringer sind. Der Flügel 14c, 16c liegt insbesondere auf einer umso größeren Fläche auf dem Grundkörper 12c auf, je größer die auf den Flügel 14c, 16c ausgeübte Kraft P2 ist. Der Flügel 14c ist insbesondere derart ausgebildet, dass der Flügel 14c den Grundkörper 12c in mindestens einem Bereich 42 nicht kontaktiert, wenn der Flügel 14c eine Kraft auf den letzten Wertschein des Wertscheinstapels ausübt. Der Flügel 16c ist analog zum Flügel 14c ausgebildet, so dass die Ausführungen, die für den Flügel 14c beschrieben sind, entsprechend für den Flügel 16c und die Ausführungen, die für den Flügel 16c beschrieben sind, entsprechend für den Flügel 14c gelten. Der Spalt, der im unbelasteten Zustand zwischen dem Flügel 14c, 16c und dem Grundkörper 12c vorhanden ist, sollte möglichst gering sein, so dass der Flügel 14c, 16c bei dem Kontakt mit einem Wertschein schnell auf den Grundkörper 12c aufliegt. Der unbelastete Zustand ist derjenige Zustand, in dem der Flügel 14c, 16c keine Kraft auf einen Wertschein ausübt und der Flügel 14c, 16c nicht durch angrenzende Elemente 28, 30 umgebogen wird.The
Der Flügel 14c ist derart ausgebildet, dass der Stützbereich 38 parallel zu einer Tangente an den Grundkörper 12c an einer ersten Stelle 44 verläuft. Die Verbindungsstelle 46 zwischen dem Flügel 14c und dem Grundkörper 12c ist in Drehrichtung P1 des Grundkörpers 12c gesehen um einen Winkel vor der ersten Stelle 44 angeordnet. Dieser Winkel hat insbesondere einen Wert im Bereich zwischen 0° und 45°, vorzugsweise im Bereich zwischen 10° und 30°. Hierdurch wird erreicht, dass der Flügel 14c verglichen mit einem Flügel, der tangential an der ersten Stelle 44 an den Grundkörper 12c angebunden ist, länger und somit auch weicher ist. Ein solcher weicher Flügel 14c wird bei der Beanspruchung mit einer gleich großen Kraft mit geringeren mechanischen Spannungen beansprucht als der kürzere tangential angebundene Flügel.The
Zwischen der Längsachse eines Verbindungsbereiches 20c des Flügels 14c und einer Tangente an den Grundkörper 12c an der Verbindungsstelle 46 ist ein Winkel im Bereich zwischen 70° und 110°. Bei einer bevorzugten Ausführungsform der Erfindung beträgt der Winkel etwa 90°, so dass der Verbindungsbereich 20c des Flügels 14c radial an den Grundkörper 12c angebunden ist.Between the longitudinal axis of a connecting
Ferner ist der Flügel 14c derart ausgebildet, dass zwischen dem Stützbereich 38 und dem Verbindungsbereich 20c im unbelasteten Zustand des Flügels 14c ein Winkel im Bereich zwischen 70° und 110°, vorzugsweise ein Winkel von etwa 90°, ist. Hierdurch wird erreicht, dass der Verbindungsbereich 20c des Flügels 14c radial vom Grundkörper 12c absteht und der Stützbereich 38 des Flügels 14c trotzdem parallel zu einer Tangente an den Grundkörper 12c in der ersten Stelle 44 verläuft. Ein Übergangbereich zwischen dem Stützbereich 38 und dem Verbindungsbereich 20c ist vorzugsweise entgegen der Drehrichtung P1 gekrümmt, insbesondere in Form eines Radius ausgebildet.Further, the
Die in
Ferner wird durch die zurückliegende Anbindung der Flügel 14c, 16c erreicht, dass der Flügel 16c durch den Kontakt mit dem angrenzenden Element 28 weniger stark gekrümmt wird, so dass der Krümmungsradius verglichen mit den Krümmungsradien bei den Ausführungsformen der Flügelräder 10a, 10b nach den
Ferner umfasst der Flügel 14c einen Gegenkrümmungsbereich 48, der derart gekrümmt ist, dass das nicht mit dem Grundkörper 12c verbundene Ende des Flügels 14c in Drehrichtung P1 weist. Durch diese Gegenkrümmung des Flügels 14c wird erreicht, dass das Zurückbiegen des Flügels 14c entgegen der Drehrichtung P1 durch das Abstützen des Flügels 14c auf dem Grundkörper 12c zumindest teilweise kompensiert wird. Auf diese Weise wird sichergestellt, dass die zum Zurückhalten des letzten Wertscheins des Wertscheinstapels notwendige Kraft durch den Andruckbereich 24c, insbesondere durch das dem Grundkörper 12c abgewandte Ende des Andruckbereiches 14c, sichergestellt ist. Insgesamt ist der Flügel 14c somit S-förmig.Furthermore, the
Die Flügel 14c, 16c und der Grundkörper 12c sind insbesondere einteilig ausgebildet. Das Flügelrad 10c ist vorteilhafterweise aus einem unvernetzten Elastomer, insbesondere aus Polyurethan (PU), aus einem thermoplastischen Elastomer (TPE) oder aus Polyester-Urethan-Kautschuk (Vulkollan®), hergestellt und wird beispielsweise im Spritzgussverfahren hergestellt. Alternativ kann das Flügelrad 10c auch aus vernetzten Elastomeren hergestellt werden.The
Die Flügel 14c, 16c des Flügelrades 10c sind um 180° versetzt angeordnet. Bei einer alternativen von den Patentansprüchen nicht abgedeckten Ausführungsform können die Flügel 14c, 16c auch um einen anderen von 180° abweichenden Winkel zueinander versetzt sein. Ferner können auch mehr oder in einer von den Patentansprüchen nicht abgedeckten Ausführungsform, weniger als zwei Flügel 14c, 16c vorgesehen sein. Insbesondere kann bei anderen Ausführungsformen das Flügelrad 10c nur einen Flügel 14c, 16c, welche Ausführungsform nicht von den Patentansprüchen abgedeckt ist, oder vier Flügel 14c, 16c, die um 90° versetzt angeordnet sind, haben.The
- 10a, 10b, 10c10a, 10b, 10c
- Flügelradimpeller
- 12a, 12b, 12c12a, 12b, 12c
- Grundkörperbody
- 14a, 14b, 14c14a, 14b, 14c
- Flügelwing
- 16a, 16b, 16c16a, 16b, 16c
- Flügelwing
- 1818
- Wellewave
- 20a, 20b, 20c20a, 20b, 20c
- Verbindungsbereichconnecting area
- 22a, 22b, 22c22a, 22b, 22c
- Verbindungsbereichconnecting area
- 24a, 24b, 24c24a, 24b, 24c
- Andruckbereichpressure region
- 26a, 26b, 26c26a, 26b, 26c
- Andruckbereichpressure region
- 28, 3028, 30
- angrenzendes Elementadjacent element
- 32a, 32b32a, 32b
- Krümmungsbereichcurvature region
- 34, 3634, 36
- Hüllkreisenveloping circle
- 38, 4038, 40
- Stützbereichsupport area
- 4242
- BereichArea
- 4444
- erste Stellefirst place
- 4646
- Verbindungsstellejunction
- 4848
- GegenkrümmungsbereichAgainst bending area
- P1P1
- Drehrichtungdirection of rotation
- P2P2
- Kraftforce
Claims (11)
- Device for inputting banknotes into a container, having a feed unit for feeding the banknotes,
having a stacking unit for stacking the fed banknotes, and
having at least one paddle wheel (10c) for handling the banknotes, comprising a rotatably mounted main body (12c) and a paddle (14c, 16c) which, at a first end of a connection region (20c, 22c), is fixedly connected to the main body (12c), wherein the paddle (14c, 16c) comprises a pressure-exerting region (24c, 26c) for exerting a force on at least one banknote and comprises a support region (38, 40),
wherein the support region (38, 40) makes contact with the shell surface of the main body (12c) when the paddle (14c, 16c) exerts a force on a banknote, and
wherein at least a part of the paddle (14c, 16c), when exerting a force on a banknote, exhibits a curvature counter to the direction of rotation (P1) of the paddle wheel (10c),
wherein the paddle wheel (10c) has two paddles (14c, 16c) arranged offset by 180°,
characterized in that the curvature central point of the curvature of the paddle (14c, 16c) lies within a space delimited by the shell surface of the hollow cylindrical main body (12c). - Device according to Claim 1, characterized in that, between the connection region (20, 22) and the support region (38, 40), the paddle (14c, 16c) does not make contact with the main body (12c) at least in one region (42) when the paddle (14c, 16c) exerts a force on a banknote and the support region (38, 40) makes contact with the shell surface of the main body (12c).
- Device according to either of Claims 1 and 2, characterized in that the support region (38, 40) of the paddle (14c, 16c), when said paddle is not exerting a force on a banknote, runs substantially parallel to a tangent to the main body (12c) at a first point (44), and in that the connection point (46) at which the paddle (14c, 16c) is connected to the main body (12c) is, as viewed in the direction of rotation (P1) of the main body (12c), arranged in front of the first point (44) by an angle of less than 45°, in particular an angle in the range between 10° and 30°.
- Device according to one of Claims 1 to 3, characterized in that, between the longitudinal axis of the connection region (20c, 22c) of the paddle (14c, 16c) and a tangent to the main body (12c) at the connection point (46) at which the paddle (14c, 16c) is connected to the main body (12c), there is an angle in the range between 70° and 110°.
- Device according to one of Claims 1 to 4, characterized in that the connection region (20c, 22c) of the paddle (14c, 16c) is attached radially onto the shell surface of the main body (12c).
- Device according to one of Claims 1 to 5, characterized in that, in an unloaded state of the paddle (14c, 16c), between the connection region (20c, 22c) and the support region (38, 40), there is an angle in the range between 70° and 110°, in particular an angle of approximately 90°.
- Device according to one of Claims 1 to 6, characterized in that the main body (12c) and the paddle (14c, 16c) are formed in one piece.
- Device according to one of Claims 1 to 7, characterized in that the main body (12c) is a hub which is mounted so as to be rotatable about its longitudinal axis.
- Device according to one of Claims 1 to 8, characterized in that the curvature central point of the curvature of the paddle (14c, 16c) lies on the axis of rotation of the main body (12c).
- Device according to one of Claims 1 to 9, characterized in that the paddle (14c, 16c) has a region of S-shaped form.
- Device according to one of Claims 1 to 10, characterized in that the paddle wheel (10c) is produced from a non-crosslinked elastomer.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102009015383A DE102009015383A1 (en) | 2009-03-27 | 2009-03-27 | Device for entering notes of value in a container |
PCT/EP2010/053612 WO2010108864A1 (en) | 2009-03-27 | 2010-03-19 | Device for inputting securities into a container |
Publications (2)
Publication Number | Publication Date |
---|---|
EP2411311A1 EP2411311A1 (en) | 2012-02-01 |
EP2411311B1 true EP2411311B1 (en) | 2018-07-18 |
Family
ID=42312980
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP10717071.4A Active EP2411311B1 (en) | 2009-03-27 | 2010-03-19 | Device for inputting banknotes into a container, and paddle wheel |
Country Status (5)
Country | Link |
---|---|
US (1) | US8720672B2 (en) |
EP (1) | EP2411311B1 (en) |
CN (1) | CN102387975B (en) |
DE (1) | DE102009015383A1 (en) |
WO (1) | WO2010108864A1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8777222B2 (en) * | 2011-11-30 | 2014-07-15 | Ncr Corporation | Document stacking |
CN110335408B (en) * | 2018-03-13 | 2024-10-29 | 山东新北洋信息技术股份有限公司 | Impeller assembly, banknote collection and separation device and cash recycling equipment |
CN111252480A (en) * | 2020-03-17 | 2020-06-09 | 上海克硫环保科技股份有限公司 | Double-valve-core discharging device |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62150451U (en) * | 1986-03-17 | 1987-09-24 | ||
JP2007091437A (en) * | 2005-09-30 | 2007-04-12 | Hitachi Omron Terminal Solutions Corp | Paper sheet stacking device |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3649003A (en) * | 1970-06-29 | 1972-03-14 | Baeuerle Gmbh Mathias | Sheet feeding mechanism for a small duplicating machine |
US4043549A (en) * | 1975-11-24 | 1977-08-23 | Xerox Corporation | Impact feeder |
SE413007B (en) * | 1977-04-12 | 1980-03-31 | Wifag Maschf | DEVICE FOR CREATING A CURRENT OF OVERLAPPED FALSE PRINTED PRODUCTS |
US4475733A (en) * | 1982-08-02 | 1984-10-09 | Xerox Corporation | Enhanced paddle wheel inertial separator and transporter |
US4585226A (en) * | 1984-07-12 | 1986-04-29 | Pitney Bowes Inc. | Resilient document feeding member |
DE3826348A1 (en) * | 1988-08-03 | 1990-02-08 | Roland Man Druckmasch | SHOVEL WHEEL BOOM |
US5098080A (en) * | 1990-12-19 | 1992-03-24 | Xerox Corporation | Ski jump stack height sensor |
US5415390A (en) | 1994-05-23 | 1995-05-16 | Hewlett-Packard Company | Double surface registration mechanism for a stack of sheets |
KR100330326B1 (en) | 1998-10-12 | 2002-04-01 | 가나이 쓰토무 | A Paper Money Paying-in and Paying-out Device |
JP4042304B2 (en) * | 2000-06-14 | 2008-02-06 | 富士電機リテイルシステムズ株式会社 | Paper sheet storage device |
JP3929762B2 (en) | 2001-12-03 | 2007-06-13 | 日立オムロンターミナルソリューションズ株式会社 | Paper sheet stacking and feeding device |
JP3880503B2 (en) * | 2002-10-16 | 2007-02-14 | 日立オムロンターミナルソリューションズ株式会社 | Paper sheet stacking and feeding device |
JP4292012B2 (en) * | 2003-02-10 | 2009-07-08 | 日立オムロンターミナルソリューションズ株式会社 | Banknote deposit and withdrawal device |
JP4257705B2 (en) * | 2004-03-04 | 2009-04-22 | 日立オムロンターミナルソリューションズ株式会社 | Paper sheet stacking and feeding device, rotating member, and guide member |
EP1873726A4 (en) * | 2005-03-29 | 2010-07-07 | Glory Kogyo Kk | Banknote handling device |
JP4495645B2 (en) * | 2005-07-19 | 2010-07-07 | グローリー株式会社 | Banknote transfer device |
JP4715656B2 (en) * | 2006-07-05 | 2011-07-06 | 沖電気工業株式会社 | Media processing device |
US7571904B2 (en) * | 2006-12-07 | 2009-08-11 | Xerox Corporation | Control system for indexing compiler drive shaft that senses drive torque to initiate indexing |
DE102008018961A1 (en) * | 2008-04-15 | 2009-10-29 | Wincor Nixdorf International Gmbh | Single-sheet handling device for entering rectangular single sheets into a container |
-
2009
- 2009-03-27 DE DE102009015383A patent/DE102009015383A1/en not_active Ceased
-
2010
- 2010-03-19 US US13/260,044 patent/US8720672B2/en active Active
- 2010-03-19 EP EP10717071.4A patent/EP2411311B1/en active Active
- 2010-03-19 CN CN201080015251.7A patent/CN102387975B/en active Active
- 2010-03-19 WO PCT/EP2010/053612 patent/WO2010108864A1/en active Application Filing
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62150451U (en) * | 1986-03-17 | 1987-09-24 | ||
JP2007091437A (en) * | 2005-09-30 | 2007-04-12 | Hitachi Omron Terminal Solutions Corp | Paper sheet stacking device |
Also Published As
Publication number | Publication date |
---|---|
US20120085625A1 (en) | 2012-04-12 |
DE102009015383A1 (en) | 2010-09-30 |
WO2010108864A1 (en) | 2010-09-30 |
EP2411311A1 (en) | 2012-02-01 |
CN102387975B (en) | 2015-10-07 |
CN102387975A (en) | 2012-03-21 |
US8720672B2 (en) | 2014-05-13 |
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