EP2477820B1 - Traganordnung für eine tintenstrahl-druckvorrichtung - Google Patents

Traganordnung für eine tintenstrahl-druckvorrichtung Download PDF

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Publication number
EP2477820B1
EP2477820B1 EP10770942.0A EP10770942A EP2477820B1 EP 2477820 B1 EP2477820 B1 EP 2477820B1 EP 10770942 A EP10770942 A EP 10770942A EP 2477820 B1 EP2477820 B1 EP 2477820B1
Authority
EP
European Patent Office
Prior art keywords
support
support assembly
carrier
assembly
supporting element
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
Application number
EP10770942.0A
Other languages
German (de)
English (en)
French (fr)
Other versions
EP2477820A2 (de
Inventor
Peter Weingartner
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.)
Durst Phototechnik Digital Technology GmbH
Original Assignee
Durst Phototechnik Digital Technology GmbH
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
Application filed by Durst Phototechnik Digital Technology GmbH filed Critical Durst Phototechnik Digital Technology GmbH
Publication of EP2477820A2 publication Critical patent/EP2477820A2/de
Application granted granted Critical
Publication of EP2477820B1 publication Critical patent/EP2477820B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B41—PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
    • B41J—TYPEWRITERS; SELECTIVE PRINTING MECHANISMS, i.e. MECHANISMS PRINTING OTHERWISE THAN FROM A FORME; CORRECTION OF TYPOGRAPHICAL ERRORS
    • B41J19/00—Character- or line-spacing mechanisms
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B41—PRINTING; LINING MACHINES; TYPEWRITERS; STAMPS
    • B41J—TYPEWRITERS; SELECTIVE PRINTING MECHANISMS, i.e. MECHANISMS PRINTING OTHERWISE THAN FROM A FORME; CORRECTION OF TYPOGRAPHICAL ERRORS
    • B41J19/00—Character- or line-spacing mechanisms
    • B41J19/18—Character-spacing or back-spacing mechanisms; Carriage return or release devices therefor
    • B41J19/20—Positive-feed character-spacing mechanisms

Definitions

  • the invention relates to a support arrangement for an ink jet printing apparatus, as described in claim 1.
  • a method for producing such a carrier and such a carrier is known from EP 2 000 316 A1 become known to the same applicant.
  • the walls of the carrier are formed by joining each in the longitudinal direction of the carrier successively arranged Obergurtmodulen, lower chord modules, front wall modules and backplane modules.
  • transverse webs are arranged at intervals.
  • at least one guide track extending in its longitudinal direction is arranged on the carrier for a module which is movable along the guide track.
  • they are formed in such a way that areas of the modules are machined after joining the modules and transverse webs.
  • the present invention has for its object to provide a support assembly for guiding a printhead carriage of an inkjet printing device, which at a small size during printing a nearly constant distance between the mostly planar surface of the object to be printed and the front end of the printhead arranged there Nozzles over the entire longitudinal extent of the support assembly allows.
  • the advantage resulting from the features of claim 1 lies in the fact that the possibility is created, the additional support element with respect to the support to be deformed relative to the carrier so that this in its mostly horizontal position even at a load through along the Guideway movable assembly, such as the printhead carriage, is rectilinear and thus aligned without deflection.
  • the support element is supported at its two ends against the carrier load-bearing, can be increased by means of the adjusting element, the mutually desired bias so far that even at the highest load the straightness over the entire longitudinal extension of the carrier can be maintained.
  • a further advantage is an embodiment according to claim 3, as this can easily be adapted to different conditions of use to guide the print head carriage can be created.
  • the possibility is created to respond automatically to different deflections quickly and thus be able to compensate for them by the shortest route.
  • vibrations occurring of the support assembly could be reduced or compensated by changing the mutual bias between the support and the support element.
  • a support assembly 1 is shown for an ink jet printing device not shown here, wherein the support assembly 1 in the longitudinal direction or longitudinal extent at least one guideway 2 has.
  • a movable assembly not shown here, such as a printhead carriage, with the pressure devices, nozzles, etc. arranged thereon is moved.
  • the liquid pressure medium between the medium emitting nozzles and a mostly planar surface of the object to be printed a nearly constant distance is necessary, this could so far only be achieved by massive additional reinforcements of the support assembly 1 on the outside. This leads in many cases to space problems with regard to the not shown and movable adjustable adjustable assembly.
  • the carrying arrangement 1 comprises at least one carrier 3 having a longitudinal extent and at least one rod-shaped supporting element 4 likewise extending in the longitudinal direction thereof.
  • the carrier 3 is in the region of its longitudinally spaced-apart ends 5, 6 via bearings 7 shown schematically here supported on the base of the ink jet printing apparatus.
  • the support or storage of the carrier 3 can be done for example by a floating bearing in the region of the end 5 and a fixed bearing in the region of the end 6. This is in the sense of statics or in engineering a mostly horizontally extending, in relation to its length narrow and slender beam, which derives the loads resting on it on walls or vertical supports.
  • the two bearings 7 thus support the beam or support 3 at two spaced locations, whereby a support is present on two supports.
  • a bending line 8 which represents the deflection of the carrier 3 greatly exaggerated.
  • This bending line 8 comes not only the weight of the carrier 3, but also by the previously movably guided assembly to conditions.
  • the carrier 3 is shown between its two bearings 7 in a theoretically ideal position or position, wherein between the two bearings 7, a rectilinear or planar reference plane 9 is clamped. Normally, this is aligned horizontally. Due to the deflection of the carrier 3 is formed on average between the two bearings 7, the largest deflection and thus deviation of the carrier 3 from the reference plane 9 from.
  • the support member 4 for forming the support assembly 1 also extends in the longitudinal direction of the carrier 3 and has in the longitudinal extension of the same likewise mutually distanced ends 10, 11. In this embodiment shown here, the two ends 10, 11 in approximately equidistant from each other as the ends 5, 6 of the carrier 3. Thus, the carrier 3 and the support member 4 at least approximately the same longitudinal extent.
  • the carrier 3 and the support member 4 is additionally clamped over its longitudinal extent by means of at least one control element 13 against each other.
  • the one or more adjusting element 13 may also be referred to as adjusting means.
  • This mutually braced position of the carrier 3 with respect to the support member 4 is best from the Fig. 2 refer to.
  • the weight generated by the movable assembly and the net mass or the weight of the carrier 3 is shown in simplified form with an arrow "F". The deflection of the carrier 3 caused by the total weight F is minimized or completely eliminated by the adjusting element or elements 13.
  • the support member 4 seen at least in the direction of action of gravity away from the wall portion of the carrier 3 is arranged.
  • the one or more adjusting elements 13 may be selected from the group of components such as setscrews, compression springs, tension springs, cylinder-piston assemblies, etc. It is also possible any combination of different control elements 13 possible. It may be advantageous if individual adjusting elements 13 build a compressive force and further of the adjusting elements 13, a tensile force between the carrier 3 and the support member 4 and these are used together. Likewise, the one or more adjusting elements 13 may be arranged at any position both in the longitudinal direction of the support assembly 1 and between the support 3 and the support member 4.
  • a first adjusting element 13 approximately in the middle between the two bearings 7 on the side above the support member 4 and the wall part of the carrier. 3 arranged. Further adjusting elements 13 are arranged distanced towards in the direction of the two ends 5, 6 and formed for example as screws.
  • the two adjusting elements 13 configured as screws act here from the underside of the carrier 3 in the direction of the support element 4.
  • a control element 13 corresponding threaded arrangement is provided here in the lower wall portion of the support, wherein in the support member 4, a control element 13 corresponding threaded arrangement is provided.
  • additional thread extensions in the region of the support member 4 has been omitted for the sake of clarity, but can be used or provided especially in rather thin-walled hollow sections.
  • nuts or threaded blocks can be used.
  • the entire support 3 can be raised by the relative deformation of the support element 4 so far that the support 3 is aligned at least planar to the reference plane 9.
  • This planar alignment with respect to the reference plane 9 should then be adjusted or pre-adjusted, even if the largest weight is introduced or applied by the movable assembly on the support assembly 1 on the support assembly 1. It can also happen that the carrier 3 against removal of the moving assembly, such as the printhead carriage, introduced weight contrary to the direction of action of gravity - ie upwards - before deformed. Only with a corresponding load by the weight of the movable assembly is the planar or rectilinear orientation of the carrier 3 with respect to the reference plane 9 a. Thus, a constant distance is maintained even during the reciprocation of the printhead carriage between the ends of the nozzle openings and the surface to be printed. The caused by the mutual tension deformation of the support member 4 should still be in the elastic region of the material used.
  • actuator 13 may be formed, for example, as a resilient pressure element and in cooperation with the screws designed as actuating elements 13 which cause mutual tension between the carrier 3 and the support member 4.
  • Fig. 2 is again provided in the middle of the longitudinal extent between the two bearings 7, the spring-acting actuator 13.
  • the two as Screws formed adjusting elements 13 also designed to build a pressure effect against each other bracing the carrier 3 with the support member 4. Due to the spatial distancing of the support member 4 with respect to the wall portion of the support 3, this can be seen deformed without problems in the direction of gravity, that the previously described straightness or flatness of the support 3 with respect to the reference plane 9 can be adjusted.
  • the carrier 3 can be composed of various modules, for example, as already in their own EP 2 000 316 A1 has been described. In order to avoid unnecessary repetition, attention is drawn to the detailed disclosure of the module-like carrier 3 on the disclosure made there, or taken by reference and incorporated this disclosure content in the present application.
  • the carrier 3 may be formed from Obergurtmodulen, Untergurtmodulen, front and rear wall modules.
  • the trained here as a floating bearing 12 for supporting the support member 4 on the support 3 is realized here for example by a rib or web.
  • the rib 12 formed as a web or bearing 12 may have a recess 14.
  • the mutual tension between the support 3 and the support member 4 is to be selected accordingly.
  • the carrier 3 and the support member 4 is seen at least in the direction of action of gravity, clamped by the one or more adjusting elements 13 against each other.
  • a normal installation case can also be spoken of a mutual, vertical support. Additionally or independently of this, however, it would also be possible to brace the carrier 3 against one another relative to the support element 4, even in a direction oriented at an angle with respect to the direction of action of the gravitational force.
  • the carrier 3 is designed, for example, as a prismatic hollow body.
  • the support member 4 may for example also be formed as a prismatic hollow body.
  • As preferred cross sections have here rectangular Tube cross sections proved. But it can also find differently shaped support elements 4 application. It would thus be possible to use heavily prestressed ropes which are connected to the carrier 3 via holding elements. This could take the form of a support arrangement, as these are used for the overhead line in the railway or for supporting structures in bridge construction.
  • the support element 4 is arranged with its cross section within an outer boundary line of the carrier 3.
  • the support 3 is designed as a hollow profile body, the rod-shaped support element 4 can be arranged within the free space of the support 3.
  • On appropriate mutual dimensional coordination is to take care to provide enough adjustment between an inner wall of the support 3 and an outer wall of the support member 4 ready or create.
  • a in the Fig. 1 Simplified illustrated detection device 16 to transmit or forward.
  • This detected measured value can then be forwarded, for example, from the detection device 16 to a control device 17 during a line connection.
  • control device 17 is connected to the one or more adjusting elements 13 in line connection and causes a corresponding adjustment of the actuating element 13 in order to achieve the straightness or flatness of the carrier 3 with respect to the reference plane 9. It can be spoken of an active, acting as a function of the introduced weight setting of the mutually braced components, namely the carrier 3 and the support member 4.
  • Fig. 4 is a further and possibly independent embodiment of the support assembly 1 is shown, again for like parts, the same reference numerals or component designations as in the preceding Fig. 1 to 3 be used. In order to avoid unnecessary repetition, the detailed description in the previous ones will be used Fig. 1 to 3 referred or referred.
  • the carrier 3 is shown here, wherein this has an I-shaped cross section.
  • a separate support element 4 on both sides of the web of the carrier 3.
  • the supporting element 4 relative to the carrier 3 supporting bearing 12 are arranged on the support 3.
  • These are formed in the present embodiment by ribs which may have a corresponding receiving opening for the support member 4.
  • the support elements 4 are in turn associated with the adjusting elements 13, seen here in the direction of gravity, above the support elements 4, the adjusting elements 13 are designed as pressure elements and arranged below the support elements 4 adjusting elements 13 are formed as screws which between the flange of the support and the support member 4 can build a tensile force. Instead of trained as tension elements screws but also springs or the like can apply.

Landscapes

  • Ink Jet (AREA)
  • Character Spaces And Line Spaces In Printers (AREA)
  • Handling Of Sheets (AREA)
EP10770942.0A 2009-09-15 2010-09-14 Traganordnung für eine tintenstrahl-druckvorrichtung Active EP2477820B1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ATA1456/2009A AT508825B1 (de) 2009-09-15 2009-09-15 Traganordnung für eine tintenstrahl-druckvorrichtung
PCT/AT2010/000334 WO2011032194A2 (de) 2009-09-15 2010-09-14 Traganordnung für eine tintenstrahl-druckvorrichtung

Publications (2)

Publication Number Publication Date
EP2477820A2 EP2477820A2 (de) 2012-07-25
EP2477820B1 true EP2477820B1 (de) 2014-01-22

Family

ID=43589609

Family Applications (1)

Application Number Title Priority Date Filing Date
EP10770942.0A Active EP2477820B1 (de) 2009-09-15 2010-09-14 Traganordnung für eine tintenstrahl-druckvorrichtung

Country Status (6)

Country Link
US (1) US8925394B2 (es)
EP (1) EP2477820B1 (es)
AT (1) AT508825B1 (es)
ES (1) ES2450143T3 (es)
IL (1) IL218630A (es)
WO (1) WO2011032194A2 (es)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6512675B2 (ja) 2015-10-29 2019-05-15 富士フイルム株式会社 液体吐出ヘッド、及び液体吐出装置
US11479704B2 (en) 2018-08-10 2022-10-25 Halliburton Energy Services, Inc. Potassium salt treatment fluids for clay stabilization

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4392757A (en) * 1980-05-22 1983-07-12 International Business Machines Corporation Backlash and runout compensator for lead screw drives
FR2623902B1 (fr) * 1987-11-26 1990-05-04 Schlumberger Ind Sa Traceur ayant un plateau de support de feuille a profil angulaire
ES2244146T3 (es) 1999-02-17 2005-12-01 Hewlett-Packard Company, A Delaware Corporation Chasis de impresora.
US6595615B2 (en) * 2001-01-02 2003-07-22 3M Innovative Properties Company Method and apparatus for selection of inkjet printing parameters
US6565272B2 (en) * 2001-08-27 2003-05-20 Hewlett-Packard Development Company, L.P. Compliant carriage adjustment method and apparatus for setting default printhead-to-media- spacing in a printer
JP2005096379A (ja) * 2003-09-26 2005-04-14 Brother Ind Ltd インクジェット記録装置
DE602005002613T2 (de) 2004-12-22 2008-07-24 Océ-Technologies B.V. Druckgerät mit hin- und hergehendem Wagen und zweiteiliger Rahmenstruktur
DE602005026369D1 (de) 2005-05-09 2011-03-31 Agfa Graphics Nv Segmentierte Fördervorrichtung für ein Aufzeichnungsmedium und Kalibrierung des Strahlabstandes in einem digitalen Drucker
AT505426B1 (de) * 2007-06-04 2013-04-15 Durst Phototech Digital Tech Verfahren zur herstellung eines trägers und träger

Also Published As

Publication number Publication date
AT508825A2 (de) 2011-04-15
AT508825B1 (de) 2012-06-15
ES2450143T3 (es) 2014-03-24
IL218630A (en) 2015-05-31
IL218630A0 (en) 2012-05-31
US20120227516A1 (en) 2012-09-13
WO2011032194A2 (de) 2011-03-24
US8925394B2 (en) 2015-01-06
AT508825A3 (de) 2012-01-15
WO2011032194A3 (de) 2011-05-12
EP2477820A2 (de) 2012-07-25

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