EP0771753A1 - Système de régulation de phase pour les roues à aubes de plieuses - Google Patents

Système de régulation de phase pour les roues à aubes de plieuses Download PDF

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Publication number
EP0771753A1
EP0771753A1 EP96115359A EP96115359A EP0771753A1 EP 0771753 A1 EP0771753 A1 EP 0771753A1 EP 96115359 A EP96115359 A EP 96115359A EP 96115359 A EP96115359 A EP 96115359A EP 0771753 A1 EP0771753 A1 EP 0771753A1
Authority
EP
European Patent Office
Prior art keywords
airfoil
phase angle
phase
impeller
product
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.)
Granted
Application number
EP96115359A
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German (de)
English (en)
Other versions
EP0771753B1 (fr
Inventor
Charles Henry Dufour
Paul Raymond Bolduc
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Heidelberger Druckmaschinen AG
Original Assignee
Heidelberger Druckmaschinen AG
Priority date (The priority date 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 date listed.)
Filing date
Publication date
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Publication of EP0771753A1 publication Critical patent/EP0771753A1/fr
Application granted granted Critical
Publication of EP0771753B1 publication Critical patent/EP0771753B1/fr
Anticipated expiration legal-status Critical
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H29/00Delivering or advancing articles from machines; Advancing articles to or into piles
    • B65H29/38Delivering 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
    • B65H29/40Members rotated about an axis perpendicular to direction of article movement, e.g. star-wheels formed by S-shaped members
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2511/00Dimensions; Position; Numbers; Identification; Occurrences
    • B65H2511/20Location in space
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2511/00Dimensions; Position; Numbers; Identification; Occurrences
    • B65H2511/20Location in space
    • B65H2511/21Angle
    • B65H2511/212Rotary position
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2511/00Dimensions; Position; Numbers; Identification; Occurrences
    • B65H2511/40Identification
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2511/00Dimensions; Position; Numbers; Identification; Occurrences
    • B65H2511/50Occurence
    • B65H2511/51Presence
    • B65H2511/514Particular portion of element
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2513/00Dynamic entities; Timing aspects
    • B65H2513/10Speed
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B65CONVEYING; PACKING; STORING; HANDLING THIN OR FILAMENTARY MATERIAL
    • B65HHANDLING THIN OR FILAMENTARY MATERIAL, e.g. SHEETS, WEBS, CABLES
    • B65H2701/00Handled material; Storage means
    • B65H2701/10Handled articles or webs
    • B65H2701/19Specific article or web
    • B65H2701/1912Banknotes, bills and cheques or the like

Definitions

  • the present invention relates to a folder for folding printed products and, in particular, to a system for monitoring and regulating the phase of airfoils in such a folder.
  • a paper web fed through a web-fed rotary printing machine After a paper web fed through a web-fed rotary printing machine has been printed, it is fed to a folder for further processing.
  • the web is usually cut in the folder and folded into signatures.
  • the signatures are then divided into several product streams and laid out for further processing.
  • the division of the signatures into several product streams can be achieved by arranging a pair of rotating paddle wheels in the signature path.
  • U.S. 5,112,033 discloses e.g. B. a folder with a first and a second paddle wheel, which rotate in opposite directions. Cut and folded printed products (ie signatures) are transported in the immediate vicinity of the rotating paddle wheels using high-speed conveyor belts.
  • Each of the bucket wheels has a plurality of bucket blades, the tips of which define the circumference of a respective bucket wheel.
  • the bucket blades arranged one next to the other form pockets for receiving the cut and folded printed products.
  • the circumference of the first impeller overlaps the circumference of the second impeller and vice versa.
  • each blade has a recess in its outer radial area which serves to receive the tips of the blades of the respective other blade wheel.
  • US-5,123,638 shows a product delivery with a flywheel arrangement for use in a folder of a printing press
  • US-4,881,731 shows a device for feeding sheets, in particular bank notes.
  • the object of the invention is to provide an apparatus and a method for regulating the phase of an impeller arrangement in the folder of a printing press, in which the release of the folded products from a transport system (e.g. high-speed conveyor belts) with the phase of the impeller blades is regulated and it is ensured that the folded products are picked up and transported by the airfoils without damage.
  • a transport system e.g. high-speed conveyor belts
  • the present invention comprises a phase control system for the paddle wheel arrangement in the folder of a printing press, which first includes a rotating paddle wheel with a first plurality of paddle blades, a second rotating paddle wheel with a second plurality of paddle blades and a transport system for feeding the folded products into a product receiving area, as seen in the transport direction, in front of the paddle wheels, the paddle wheels being arranged in such a way as to each other, that the circumferential lines described by the blade tips of the first and second blade wheels partially overlap, and the blade wheel arrangement has a first sensor which detects a first edge of a folded product when it passes a first position and which, depending on this, generates a corresponding first signal, one second sensor, which detects a respective first airfoil when it passes a second position and which generates a corresponding second signal in dependence thereon, a processor which generates a he based on the first signal Calculated most point in time when the folded product reaches a predetermined reference position lying in the product receiving area, which determines the phase
  • the impeller assembly includes a first rotating impeller with a plurality of first blades, the tips of which define the circumference of the first impeller.
  • a second rotating vane wheel includes a plurality of second vane blades, the tips of which define the circumference of the second vane wheel.
  • a product receiving area is located on an intersection of the first and second paddle wheel circumferences. The product receiving area is designed such that only one of the first and second airfoils came to occupy the product receiving area at any given time.
  • the folded product transport system is intended for the conveyance of the folded products into the product receiving area; it can e.g. B. include a pair of high speed belts and / or a cutting cylinder assembly.
  • the phase control system includes a processor, a first sensor, a second sensor and a paddle wheel motor control switch.
  • the first sensor detects an edge of a respective folded product passing a first position and generates a corresponding first signal.
  • the first position is defined as the point at which a knife of the cutting cylinder arrangement cuts the folded product.
  • this first position can be determined at any point along the high-speed belts, in the product receiving area, or at any suitable location in the folder.
  • the processor of the control system calculates a first point in time at which a respective folded product will reach a target position in the product receiving area.
  • the second sensor detects each first airfoil when it passes a second position and generates a corresponding second signal.
  • the processor of the control system calculates the phase angle of the first or of the second airfoil, whichever occupies the product receiving area first.
  • the processor of the control system then calculates the phase difference between the current airfoil phase angle and the desired airfoil phase angle.
  • a display device can be provided, on which the phase angle or phase difference is displayed to the operator.
  • the speed of rotation of the impeller assembly is controlled by an impeller motor control switch.
  • the control system changes the speed of rotation of the impeller assembly based on the phase difference by sending control signals from the processor to the impeller motor control switch. By repeatedly changing the speed of rotation of the impeller assembly in this manner, the control system adjusts the current impeller phase angle to the desired impeller phase angle.
  • various factors can be used to set the desired phase angle. If e.g., if the products (i.e., the folded signatures) get from the high-speed conveyor belts to the impeller rotation too early, the rear end of the products can wrap around the airfoils and cause a jam in the impeller assembly. On the other hand, if the products are late in the paddle wheel rotation, there is not enough time for the products to slow down and they "crash" into the rear end of the pockets formed between the blades, damaging them. The degree of slowing of the products after their release by the conveyor belts depends on the inertia of the products and the friction between the products and the blades. Another problem is the damage to the pressure due to excessive friction between the signature and the airfoils. Based on these factors, a desired airfoil phase can be determined experimentally to avoid jams, crashes and pressure damage to the products.
  • the desired airfoil phase is changed based on usage and environmental parameters.
  • the friction between the products and the airfoils depends on various other factors, such as the weight and width of the paper used, the silicone content in the paper and the associated adhesion of the products in the machine.
  • the inertia of the products also depends on the web speed of the machine and the weight of the paper.
  • the degree of pressure-damaging friction changes with temperature and humidity. Consequently, it is advantageous to set the desired phase angle based on the values of one or more of these environmental and application parameters.
  • These parameters can either be entered manually on a control panel or measured automatically by sensors.
  • the desired phase angle corresponding to the various combinations of parameters can e.g. B. determined empirically or stored in a memory as an NxN matrix, where N is the number of parameters.
  • the suitable desired phase angles can then be read directly from the matrix by entering the current values of the parameters.
  • control system can be programmed to mimic the process steps performed by the human operator. For example, the manner in which an operator manually adjusts the impeller phase based on a number of different factors, such as web speed, temperature, paper type, or other environmental or usage parameters, can be monitored by the control system and automatically stored in a table in memory. The desired phase angle can then be read from the table based on the current environmental and usage parameters in the subsequent printing process.
  • a folder 1 for cutting and folding printed products is shown.
  • a paper web is folded over a former 24 and then cut into signatures in a cutting cylinder arrangement 20.
  • the signatures are then transported from a pair of high speed belts 13 to a pair of paddle wheels 100, 200.
  • the paddle wheels 100, 200 rotate in opposite directions and are synchronized with one another so as not to collide.
  • FIG. 2 shows the blade wheel arrangement 100, 200 in detail.
  • the signatures leaving the high-speed bands 13 are shown in the blades 102, 103; 201, 202; 202, 203 of the respective paddle wheels 100, 200 formed pockets 111, 211 added.
  • FIG. 2 shows a signature 14 leaving the high-speed belts 13, which enters the pocket 211 formed by adjoining airfoils 201, 202.
  • Each airfoil has an airfoil tip 6 and an airfoil recess 5 which cooperate to prevent a collision under the airfoils. It is shown how the corresponding airfoil tip 6.12 is received in the airfoil recess 5.22.
  • FIGS. 3a-3h show the position of the vane wheels 100, 200 at eight separate times.
  • a signature 14.1 is in a "zero position", i. H. at a point immediately before it hits the tip 6.22 of the airfoil 202 of the impeller 200.
  • Part of the signature 14.1 remains in contact with the high-speed belts 13 at this time, and while the signature 14.1 leaves the latter, it moves along a center line 15 at a conveying speed W.
  • the tip 6.22 of the airfoil 202 extends over the Center line 15 to record the signature 14.1, the tip 6.12 of the airfoil 103 is received in the recess 5.22 of the airfoil 202 and the tip 6.11 of the airfoil 102 is at a distance from the center line 15.
  • 3b shows the signature 14.1 in position 1, namely at the point where it first contacts the tip 6.22 of the airfoil 202.
  • the tip 6.12 of the airfoil 102 is still away from the center line 15, and part of the signature 14.1 remains in contact with the high-speed bands 13. Since the signature 14.1 is still in contact with the high-speed bands 13, it moves continues with (approximately) the conveying speed W despite the friction caused by contact with the tip 6.22.
  • signature 14.1 bends slightly as it slides along the surface of airfoil 202, but travels at conveyor speed W due to its continued contact with high speed belts 13. In this position, position 2, the tip 6.12 of the airfoil 102 approaches the center line 15, but has not yet crossed the center line 15.
  • FIG. 3d shows the paddle wheels 100, 200 in the position 3.
  • the signature 14.1 moves under the control of the high-speed belts 13 at the conveying speed W.
  • the tip 6.12 of the airfoil 102 has now crossed the center line 15 and is in contact with the signature 14.1.
  • a second signature 14.2 is moved in the high-speed belts 13, namely at a distance d behind the signature 14.1 and at the conveying speed W.
  • 3e, 3f 3g illustrate how the signature 14.1 leaves the high-speed belts 13 and comes into contact with the airfoil 202.
  • the friction resulting from contact with the airfoil 202 slows down the signature 14.1 as it moves to the rear end of the pocket 211.
  • the tip 6.12 of the airfoil 102 pushes the signature 14.1 away from the center line 15.
  • the paddle wheels 100, 200 are shown in the position 0 '.
  • the signature 14.1 has left the airfoil 102 and is moving along the airfoil 202 to the rear end of the pocket 211, which is formed by the airfoils 201, 202 lying against one another.
  • the second signature 14.2 approaches the tip 6.12 of the airfoil 102.
  • the second signature 14.2 will also come into contact with the tip 6.12 of the airfoil 102 and move into the rear end of the pocket 111 formed by the airfoil 101, 102 lying against one another.
  • the signatures 14 released by the conveyor belts 13 too early and included in the impeller rotation it can happen that the rear end of the signature winds around the airfoil (e.g. airfoil 202), which leads to a jam in the impeller wheels 100, 200 can result.
  • the signatures 14 are released from the conveyor belts 13 too late and are included in the paddle wheel rotation, then there is not enough time for the signatures 14 to slow down and they "crash" into the rear end of the pockets 111 and 211, whereby they can be damaged.
  • the degree of slowdown of the signatures after their release by the conveyor belts 13 depends on the inertia of the signatures and the friction between the signatures and the airfoils.
  • Another problem that arises is the pressure damage caused by excessive friction between the signature and the airfoil.
  • the moisture in the print shop can affect the degree to which the ink on the signatures 14 has dried when they leave the high-speed belts 13. This in turn can be done in one Relate to pressure damage caused by a given impeller phase.
  • the type of product, type of paper, adhesiveness and silicone content of the paper can also influence the desired impeller phase.
  • the tack which is defined as the amount of static electricity in the signatures, is a parameter that is conventionally regulated by a "stapler".
  • the amount of silicone added to the web can vary in conventional printing presses. The values chosen for the adhesiveness and the silicone also have an influence on the friction and inertia properties of the signatures when they enter the paddle wheel pockets 111 and 211.
  • the phase of rolling the belts 13 with respect to the paddlewheels 100, 200 was manually adjusted by monitoring the position of the signature upon entry into the paddlewheels with a measurement mark (or with the naked eye) and then the speed of the High-speed belts 13 was regulated accordingly.
  • This method of impeller phase adjustment has several disadvantages.
  • First, the manual adjustment of the speed of the conveyor belts 13 based on measuring marks is in itself imprecise, and it is therefore not possible to optimize the phase control in this way.
  • Another problem arises from the fact that it must be possible to change the speed of the folder in accordance with the change in the web speed of the printing press. because the web speed of the printing press can vary to a great extent.
  • This inventive vane wheel phase control system 300 shown in FIG. 4 includes an airfoil position sensor 310, a vane wheel motor 320, a web speed sensor 330, a signature position sensor 360, a processor 340 and a vane wheel motor control switch 350.
  • the airfoil position sensor 310 may e.g. B. respective markings 311, which are attached to each pocket 111, 211 on one of the paddle wheels 100, 200, and a correspondingly attached, the markings 311 detecting marking sensor 312.
  • the marks 311 can e.g. B. on the blades next to the pockets 111, 211 attached metal strips.
  • the marking sensor 312 can e.g. B. be a proximity switch, which reacts to the metal strips.
  • the signature position sensor 360 determines the position of the signature 14 and can be installed in various ways. It can e.g. B. a sensor relative to the cutting cylinder assembly 20 of the folder 1 can be attached. Since the folded web is cut by the cutting cylinder arrangement 20 into signatures 14, a sensor attached to this arrangement 20 can definitely determine the point in time at which the cutting cylinder generates a signature 14. Since the distance between the cutting cylinder and the high-speed belts 13 is known, and since the The speed at which the signature 14 moves after leaving the cutting cylinder must be substantially equal to the web speed of the printing press (which is sensed by the sensor 330) is the point in time at which the leading or trailing edge of a signature 14 the conveyor belts 13 leaves, determinable. Alternatively, the speed of the signature 14 leaving the cutting cylinder can be measured by the rotational speed of the cutting cylinder 20.
  • the signature position sensor 360 could be designed such that a marking is made next to each knife 401 of the cutting cylinder 20 and a sensor is placed next to the point at which the knife 401 contacts the recess 400 of the cutting cylinder 20.
  • the position of the front and rear edges of the signature 14 is known.
  • the speed at which the signature 14 will move from the cutting cylinders 20 through the high-speed belts 13 is equal to the web speed of the printing press, since any substantial deviation from the web speed would cause a paper jam.
  • the speed of movement of the signature 14 can be calculated more directly by monitoring the speed of rotation of the cutting cylinders 20 and the drive rollers of the high-speed belts.
  • the position of the rear edge of the signature 14 could be determined in the same way.
  • a sensor ie an optical sensor
  • a period of time between the leading edges of the signatures could be from the pulse signals emitted by the sensor and the time t 1 could then be estimated as the time of the last pulse plus the time period.
  • the illustrated method of determining airfoil position is described below with respect to airfoil position sensor 310, including markers 311 and mark sensor 312. As the impeller wheels 100, 200 rotate, the markers 311 activate the mark sensor 312. Since the shape of the airfoil is known, the position of the airfoil tip (or other part of the airfoil blade that is connected to the mark 311 that activates or triggers the mark sensor) can be easily determined at the point in time at which the sensor 312 is activated or triggered. Furthermore, the position of the airfoils at any time between pulse signals can be easily extrapolated from a set of two or more pulse signals. As a result, the position of the airfoil tip in the product receiving area 110 at time t 1 can be easily determined. Since, as shown in FIGS. 3a to 3h, only one blade tip occupies the product receiving area 110 at a given time, the signatures 14 are alternately output into the pockets of the blade wheels 100 and 200.
  • step 510 and 520 the signature position and the airfoil position are determined.
  • the signature and airfoil position can e.g. B. in the processor 340 based on the information received from the sensors 310, 330 and 360 as described above.
  • one or more environmental and application parameters are evaluated in step 530 in order to determine a desired phase angle of the airfoils relative to a nominal signature position (ie the zero position).
  • a nominal signature position ie the zero position
  • the parameters can either be on a control panel entered manually or measured automatically with sensors.
  • the desired phase angles corresponding to the various combinations of parameters can e.g. B. determined empirically and stored in a memory as an N x N matrix, where N is the number of parameters.
  • the suitable desired phase angle can then be read directly from the matrix by entering the current values of the parameters. If the data for the airfoil position, the signature position and the desired phase angle are known, the processor 340 determines in step 540 whether the airfoil wheels should be accelerated or decelerated for the desired airfoil phase angle. If a change in the phase angle is required, a signal is sent to the impeller motor control switch 350 to make the desired phase angle change.
  • step 600 processor 340 determines a desired airfoil phase angle P desired at a signature reference or target position, ie the desired phase angle for an airfoil in the product receiving area at the point in time at which a signature reaches the reference position.
  • the signature reference position is defined as the zero position.
  • the desired airfoil phase angle can be determined based on the various environmental and application parameters.
  • processor 340 monitors the output of signature position sensor 360, web speed sensor 330, and airfoil position sensor 310.
  • step 630 the processor 340 calculates the time t 1 at which the front edge of the next signature 14 will reach the signature target position. As mentioned above, this time can be determined as a function of the output of the signature position sensor 360 and the web speed (W) of the printing press, since the distance (D) from the cutting cylinder arrangement 20 to the zero position is known and the time (t 0 ) at which the signature is formed in the cutting cylinder assembly 20, is detected by the signature position sensor 360.
  • the phase angle P thus becomes next of the next airfoil is determined at time t 1 .
  • the phase angle of the airfoils can be determined at any time based on the output of the airfoil position sensor 310.
  • the phase angle P is defined as the angular position of the airfoil tip in the product delivery area 110 relative to the reference plane that extends perpendicularly along the axis of rotation of the airfoil assembly. 7, this reference plane is defined as a vertical plane 760 extending upwards from the axis 750.
  • processor 340 sends a command to impeller motor control switch 350 to increase the speed of rotation of the impeller assembly.
  • processor 340 sends a command to impeller motor control switch 350 to reduce the speed of rotation of the impeller assembly.
  • the value by which the speed of rotation is to be increased or decreased can be determined in various ways. It can the rotational speed z. B. can be increased or decreased by a fixed deviation value, regardless of the difference between P next and P desired . This fixed deviation value could be determined empirically. Alternatively, the value by which the rotational speed should be increased or decreased could be changed depending on the difference between P next and P desired . The value could also be determined by an algorithm or read from a table based on the phase deviation.
  • Fig. 7a it is shown that if the airfoil position 720 is designated P next and the airfoil position 700 is designated P desired , and thus P next ⁇ P desired , the processor 340 will increase the speed of rotation of the impeller assembly 100, 200. On the other hand, if the airfoil position 710 corresponds to P next and the airfoil position 700 corresponds to P desired , and thus P next > P desired , then the Processor 340 reduce the speed of rotation of paddle wheel assembly 100, 200.
  • processor 340 can be programmed to imitate the work steps of the human operator. It can e.g. For example, the manner in which an operator manually sets the airfoil phase based on various conditions such as web speed, temperature, paper type, or other operating parameters is monitored by processor 340 and automatically stored in a table in memory. Then, in a subsequent print job, the desired phase angle P desired would be read from the table based on the current environmental and application parameters.
  • the above steps can e.g. For example, step 530 in the flowchart of FIG. 5 or step 600 in the flowchart of FIG.
  • an airfoil phase display system which has a display device 370 connected to the processor 340 described above.
  • Processor 340 determines the airfoil phase described above with reference to FIGS. 5 and 6 and then transfers it to display device 370 for display.
  • processor 340 and display device 370 may be used to display other useful information, such as. B. the display of the absolute phase position relative to the reference or target position, the current deviation from the desired phase angle, etc., can be programmed.
  • the processor 340 can be programmed to display a historical example of the phase position over a period of time. This historical example could also be displayed graphically so that the operator can follow the trend in phase deviation.
  • the airfoil phase control can be carried out separately or together with the phase control system described above.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Discharge By Other Means (AREA)
EP96115359A 1995-10-30 1996-09-25 Système de régulation de phase pour les roues à aubes de plieuses Expired - Lifetime EP0771753B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/550,430 US5653428A (en) 1995-10-30 1995-10-30 Phase control system for a folder fan
US550430 1995-10-30

Publications (2)

Publication Number Publication Date
EP0771753A1 true EP0771753A1 (fr) 1997-05-07
EP0771753B1 EP0771753B1 (fr) 2001-11-28

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US (1) US5653428A (fr)
EP (1) EP0771753B1 (fr)
JP (1) JPH09169460A (fr)
DE (2) DE19639138A1 (fr)

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DE102004029170B4 (de) * 2004-06-16 2007-05-03 Man Roland Druckmaschinen Ag Auslegermodul für eine Druckmaschine
WO2006104830A2 (fr) 2005-03-30 2006-10-05 Goss International Americas, Inc. Presse a imprimer offset sur papier sans fin pourvue d'une lame plieuse articulee
EP2441584B1 (fr) * 2005-03-30 2014-04-30 Goss International Americas, Inc. Presse rotative d'ompression offset avec calage automatique
CN101495313B (zh) * 2005-03-30 2011-11-09 高斯国际美洲公司 具有胶印滚筒脱开支撑表面的印刷单元
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EP1868812A4 (fr) * 2005-04-11 2012-01-04 Goss Int Americas Inc Unite d'impression a entrainement a moteur unique permettant de fixer automatiquement une plaque
DE102010028350B4 (de) 2010-04-29 2014-05-22 Koenig & Bauer Aktiengesellschaft Verfahren zur Regelung einer Drehwinkellage und gegebenenfalls einer Rotationsgeschwindigkeit zumindest eines lagegeregelten Antriebsmotors zumindest einer Vorrichtung eines Falzapparats
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US5653428A (en) 1997-08-05
DE19639138A1 (de) 1997-05-07
JPH09169460A (ja) 1997-06-30
DE59608312D1 (de) 2002-01-10
EP0771753B1 (fr) 2001-11-28

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