(19)
(11) EP 0 229 751 B1

(12) EUROPEAN PATENT SPECIFICATION

(45) Mention of the grant of the patent:
18.04.1990 Bulletin 1990/16

(21) Application number: 87890002.6

(22) Date of filing: 12.01.1987
(51) International Patent Classification (IPC)5B28B 1/29, B28B 7/18

(54)

Slipforming extruder for hollow-core concrete elements

Gleitfertiger für Hohldielen aus Beton

Machine à coffrages glissants pour la fabrication éléments creux en béton


(84) Designated Contracting States:
AT BE CH DE FR GB IT LI NL SE

(30) Priority: 17.01.1986 FI 860235

(43) Date of publication of application:
22.07.1987 Bulletin 1987/30

(73) Proprietor: KT-SUUNNITTELU OY
SF-37600 Valkeakoski (FI)

(72) Inventors:
  • Seppänen, Aimo
    FI-37600 Valkeakoski (FI)
  • Järvinen, Lassi
    FI-37600 Valkeakoski (FI)

(74) Representative: Wolfram, Gustav, Dipl.-Ing. 
Patentanwälte Sonn, Pawloy, Weinzinger & Wolfram, Riemergasse 14
1010 Wien
1010 Wien (AT)


(56) References cited: : 
EP-A- 0 174 923
EP-A- 0 175 930
   
       
    Note: Within nine months from the publication of the mention of the grant of the European patent, any person may give notice to the European Patent Office of opposition to the European patent granted. Notice of opposition shall be filed in a written reasoned statement. It shall not be deemed to have been filed until the opposition fee has been paid. (Art. 99(1) European Patent Convention).


    Description


    [0001] The present invention relates to a slipforming extruder in accordance with the preamble of claim 1.

    [0002] Casting of hollow-core concrete elements with sliding molds, especially hollow-core slabs, is based on extruding the concrete mix onto the casting bed by using one or several chloroforming members, e.g. a core-forming mandrel and/or a trowel tube. The concrete mix is compacted by utilizing the pressure generated by the auger flight.

    [0003] In the prior art there exist several basically similar constructions of slipforming extruders for hollow-core elements in which the concrete mix is extruded by means of auger flights. The extruder moves on rails on a bed. The auger flights are conical by their flight sections so as to make the flight expand towards the end of the flight. This kind of a construction achieves an effective compaction of the concrete. A forming member extension is provided immediately next to the auger flight, e.g., a core- forming mandrel, which is vibrated by means of a vibrator mounted inside the mandrel. In addition, a vibrator beam atop the cover part of the machine is vibrated, which combines with the vibration of the coreforming mandrels to effect the final compaction of the concrete. The core-forming mandrel is accompanied with a trowel tube, whose duty is to support the shell walls of the hollow-core slab at the final end of the extruder machinery.

    [0004] Due to the high vibration frequency, however, the drawbacks of the extruder construction of the hollow-core forming mandrel type include a high noise level, high energy consumption, and a low efficiency of vibration power used for compaction.

    [0005] From EP-A 0 125 084 a slipforming extruder of the initially defined kind is known, in which the mandrels perform an eccentric rotational movement causing a deviation in the transversal direction with respect to the axial direction of the auger flights.

    [0006] The present invention aims to overcome the disadvantages found in prior-art constructions and to present a completely new type of extruder which is especially applicable for the compaction of a soil- wet concrete mix.

    [0007] The invention is based on that the core-forming mandrel extensions of the adjacent auger flights are arranged by means of the secondary drive and power train system to move in a synchronized and counterphased manner in the axial direction with respect to each other so that an annular slot remaining between the final end of auger flights and corresponding coreforming mandrels alternately widens and narrows due to the relative movement between the auger flight and the corresponding counterphased moving core-forming mandrel. Thus, the concrete contained in this space is mixed. The auger flights in accordance with the invention, and especially their core parts, have an approximately constant diameter, thus deviating from the conventional constructions of conical shape.

    [0008] In addition, the difference between the outside diameter of auger flights and the diameter of the auger core is small as compared to the conventional auger construction, which allows a relatively large diameter for the auger core. The auger length is also preferably relatively long.

    [0009] A special feature of the invention proposes a decreasing pitch of flights towards the final end of the auger flight. This decrease of pitch is preferably constant, which makes the pitch progressively smaller towards the final end of the auger. Consequently, the pitch of auger flights is essentially smaller at the final end of the auger than at the initial end of the auger. In addition to the increasing compaction of concrete at the final end of the auger flight, the compaction is furthermore amplified by the axially reciprocating movement of the auger flights.

    [0010] More specifically, the slipforming extruder in accordance with the invention is characterized by what is stated in the characterizing part of claim 1.

    [0011] The invention provides remarkable advantages. Thus, the noise level generated by an extruder machine in accordance with the invention is essentially lower than in hollow-core extruders based on vibration compaction with a vibration frequency in the range of 150...250 Hz. In addition, the slipforming extruder in accordance with the invention is especially applicable to both the production of prestressed hollow-core slabs of the aforementioned type and production of steel-reinforced hollow-core concrete slabs.

    [0012] In the following, the invention will be examined in more detail by means of exemplifying embodiments.

    Figure 1 shows a partly schematic cross-sectioned side view of a slipforming extruder in accordance with the invention.

    Figure 2 shows a partly schematic top view of a slipforming extruder with a slightly different construction from that shown in Figure 1.

    Figure 3 shows a cross-sectional view with expanded scale an auger flight with the core-forming mandrel withdrawn.

    Figure 4 shows an auger flight depicted in Figure 3 with the core-forming mandrel expulsed.



    [0013] In the following, the constructions shown in Figures 1 and 2 are examined in parallel using an analogous reference numbering system.

    [0014] The slipforming machine shown in Figure 1 is adapted movable on a casting bed 4. The machine comprises a frame 18, which is supported on wheels 19 and movable on rails 20. With bearings rotatably secured to the frame 18, it has five parallel auger flights 2, 25 with relatively low-profile flights 5. Consequently, a core member 26 of the auger flights 2 has an appreciably large and approximately constant diameter in the axial direction. The flights 5 have a constant pitch over the entire length of the auger 2. Each final end of the augers 2 carries a core-forming mandrel 3 and/or a trowel tube, both mounted axially movable and rotatable in respect to the auger.

    [0015] The drive and power train system 7, 15, 16, 17, which is provided for rotating the auger flights 2, is arranged on the movable frame 18. This drive and power train system comprises an electric motor 17, which drives the auger flights 2, 25 via a chain sprocket 16 and a chain 15 by chain sprockets 7, which are mounted onto shafts 6 of auger flights 2, 25.

    [0016] The concrete poured from a hopper 1 is adapted to flow to the initial end of the auger flights 2. A hollow-core slab 33 to be cast is bordered from below by a bed 4, from the sides by side members which are not shown, and from above by vibrating top beams 21 and 22. As the slipforming extruder machine moves from left to right during the casting operation in accordance with Figure 1, a core-forming mandrel 3 forms a void 24.

    [0017] The frame 18 also carries a secondary drive and power train system 8...14. It comprises an electric motor 14 together with a crankshaft assembly 10, which is driven by the motor and is effectual on shafts 6 of the adjacent auger flights 2, 25. The assembly is connected via connection rods 9 to ends of bars 8 passing through hollow shafts 6 of the auger flights 2 so as to make the adjacent core-forming mandrel 3 and 30 move in a synchronized and counterphased reciprocating manner in the axial direction with respect to the corresponding auger flights 2 and 25 during the operation of the slipforming extruder machine.

    [0018] The frequency of the reciprocating movement of core-forming mandrels 3 and 30 is 0.3...100 Hz, preferably 5...10 Hz. The amplitude of the reciprocating movement (stroke length) is 0.5...50 mm, preferably about 10 mm.

    [0019] The reciprocating movement at the final end of the extrusion phase performs an extremely effective compaction of concrete. The reciprocating movement of core-forming mandrels 3, 30 creates pressure variations in the concrete by achieving in- temal mixing of concrete by means of an alternately increasing and decreasing annular space 29 between the final end of auger flights 2, 25 and corresponding core-forming mandrels 3, 30. This also forces the concrete aggregates to perform a shearing flow in the direction transverse to the axial flow. The core-forming mandrel 3 gives the void 24 a desired form. If the core-forming mandrel 3 has a cross-section of circular shape or rotates with the auger flight 2, the void 24 will have a cylindrical shape.

    [0020] In the exemplifying embodiment shown in Figures 3 and 4, the core-forming mandrel 3 may also be nonrotational. Then, the bar 8 passing through the hollow shaft 6 of the auger flight 2 moves only the core-forming mandrel 3 in respect to the auger flight 2. In order to implement this axial movement, the intruding portion of the mandrel 3 outer surface is provided with axial splines 27 and the envelope portion inner surface of the final end of the auger flight 2 is provided with corresponding key members 28. When a nonrotational mandrel 3 is used, core voids, different from a cylindrical shape, are also possible.

    [0021] The aforementioned progressively decreasing pitch is exemplified in the upper auger 2' of Figure 2. In this embodiment, the pitch of a flight 5' is decreased in the feed direction so as to achieve at the final end of the auger 2' a pitch of 30...70 % , preferably about 50 %, of the pitch at the initial end of the auger 2'. The auger 2 has a flight profile 5 with a height of, for instance, 3...10 % of the diameter of the auger 2.

    [0022] The scope of the invention entails constructions different from the exemplified embodiment. Thus, in addition to the reciprocating movement of the core- forming mandrels 3, the corresponding auger flights 2 may also move simultaneously in a counterphased manner in respect to the mandrels. In this case, too, the relative mutual movement of the auger flights 2 and the core-forming mandrels 3, is implemented. The core-forming mandrels 3 may also be actuated by a rotational movement, e.g. a oscillating rotational movement, which is different from that of the corresponding auger flights 2.


    Claims

    1. A slipforming extruder applicable to the production of hollow-core concrete elements (23) with a movable construction in respect to a casting bed (4) and comprising

    - a frame (18), which is movable and, for instance, supported by wheels (19),

    - at least two augers (2, 25) with flights (5), parallel mounted on bearings in the frame (18),

    - a primary drive and power train system (7, 15, 16, 17) for rotating the auger flights (2),

    - a core-forming mandrel (3) attached to the final end of each auger flight (2) and connected to a secondary drive and power train system, and

    - a feeder apparatus attached to the frame (18), e.g. a hopper (1), for feeding the concrete mix to be cast onto the auger flights (2),
    characterized in that the core-forming mandrel extensions (3, 30) of the adjacent auger flights (2, 25) are arranged by mean of the secondary drive and power train system (8...14) to move in a synchronized and counterphased manner in the axial direction with respect to each other so that an annular slot (29) remaining between the final end of auger flights (2, 25) and corresponding core-forming mandrels (3, 30) alternately widens and narrows due to the relative movement between the auger flight (2, 25) and the corresponding counterphased moving core-forming mandrel (3, 30).


     
    2. A slipforming extruder as claimed in claim 1, characterized in that the secondary drive and power train system comprises a power actuator (14), an electric motor, together with a crankshaft assembly (10), driven by the motor and effectual on rod shafts (8) connected to adjacent core-forming mandrels (e.g. 3 and 30) and passing through the corresponding auger flights (2 and 25).
     
    3. A slipforming extruder as claimed in claim 1, characterized in that the frequency of the reciprocating movement of core-forming mandrels (3) is 0.3...100 Hz, preferably 5...10 Hz.
     
    4. A slipforming extruder as claimed in claim 1, characterized in that the amplitude of the reciprocating movement (stroke length) of the core-forming mandrels (3) is 0.5...50 mm, preferably about 10 mm.
     
    5. A slipforming extruder as claimed in claim 1, characterized by a progressively decreasing pitch of the flight (5') of each auger flight (') in the feed direction.
     
    6. A slipforming extruder as claimed in claim 5, characterized in that the pitch of the flight (5') at the final end of the auger flight (2') is 30...70 %, preferably about 50 %, of the pitch of the flight (5') at the initial end of the auger flight (2').
     
    7. A slipforming extruder as claimed in claim 1, characterized in that each auger flight (2) and its core member (26) have a construction of an approximately constant diameter.
     
    8. A slipforming extruder as claimed in claim 1, characterized in that the profile height of the flight (5) is 3...10 % of the diameter of the auger flight (2).
     
    9. A slipforming extruder as claimed in claim 1, characterized in that the auger flights (2, 25) are adapted to move in a syncronized and counterphased reciprocating manner with respect to their corresponding core-forming mandrels (3, 30).
     
    10. A slipforming extruder as claimed in claim 1, characterized in that the core-forming mandrels (3, 30) are adapted to move in an oscillating rotational movement, unrelated to the movement of the corresponding auger flights (2, 25).
     


    Ansprüche

    1. Gleitschalungsextruder für die Herstellung von Hohlkern-Betonelementen (23) mit in bezug auf ein Gießbett (4) beweglicher Konstruktion und umfassend

    - einen beweglichen und beispielsweise auf Rädern (19) abgestützten Rahmen (18),

    - mindestens zwei Gewindegänge (5) aufweisende Schnecken (2, 25), die in Lagern im Rahmen (18) parallel angeordnet sind,

    - ein Primärantriebs- und Kraftübertragungssystem (7, 15, 16, 17) zur Drehung der Schneckengänge (2),

    - einen kernbildenden Dorn (3), der am hinteren Ende jedes Schneckenganges (2) befestigt und mit einem Sekundärantriebs- und Kraftübertragungssystem verbunden ist, und

    - eine am Rahmen (18) befestigte Zufuhrvorrichtung, z.B. einen Trichter (1) zum Zuführen einer auf die Schneckengänge (2) zu gießenden Betonmischung, dadurch gekennzeichnet, daß die kernbildenden Dornverlängerungen (3, 30) der benachbarten Schneckengänge (2, 25) so angeordnet sind, daß sie sich mittels des Sekundärantriebs- und Kraftübertragungssystems (8....4) synchron und gegenphasig in Axialrichtung in bezug auf einander bewegen, so daß sich ein zwischen dem hinteren Ende der Schneckengänge (2, 25) und den zugehörigen kernbildenden Dornen (3, 30) verbleibender ringförmiger Schlitz (29) aufgrund der Relativbewegung zwischen dem Schneckengang (2, 25) und dem entsprechenden, sich gegenphasig bewegenden kembildenden Dorn (3, 30) abwechselnd verbreitert und verengt.


     
    2. Gleitschalungsextruder nach Anspruch 1, dadurch gekennzeichnet, daß das Sekundärantriebs-und Kraftübertragungssystem einen Kraftantrieb (14), einen Elektromotor, zusammen mit einer Kurbelwellenanordnung (10) umfaßt, die vom Motor betrieben wird und auf Stangenschäfte (8) wirkt, welche mit angrenzenden kernbildenden Dornen (z.B. 3 und 30) verbunden sind und durch die entsprechenden Schneckengänge (2 und 25) hindurchgehen.
     
    3. Gleitschalungsextruder, wie in Anspruch 1 beansprucht, dadurch gekennzeichnet, daß die Frequenz der Oszillationsbewegung der kernbildenden Dorne (3) 0,3...100 Hz, vorzugsweise 5...10 Hz beträgt.
     
    4. Gleitschalungsextruder, wie in Anspruch 1 beansprucht, dadurch gekennzeichnet, daß die Amplitude der Oszillationsbewegung (Hublänge) der kernbildenden Dorne (3) 0,5...50 mm, vorzugsweise etwa 10 mm beträgt.
     
    5. Gleitschalungsextruder, wie in Anspruch 1 beansprucht, gekennzeichnet durch eine in Zufuhrrichtung progressiv abnehmende Ganghöhe des Gewindeganges (5') jedes Schneckenganges (2').
     
    6. Gleitschalungsextruder, wie in Anspruch 5 beansprucht, dadurch gekennzeichnet, daß die Ganghöhe des Gewindeganges (5') am hinteren Ende des Schneckenganges (2') 30...70%, vorzugsweise etwa 50% der Ganghöhe des Gewindeganges (5') am vorderen Ende des Schneckenganges (2') beträgt.
     
    7. Gleitschalungsextruder, wie in Anspruch 1 beansprucht, dadurch gekennzeichnet, daß jeder Schneckengang (2) und sein Kernelement (26) eine Konstruktion von annähernd konstantem Durchmesser aufweisen.
     
    8. Gleitschalungsextruder, wie in Anspruch 1 beansprucht, dadurch gekennzeichnet, daß die Profilhöhe des Gewindeganges (5) 3...10% des Durchmessers des Schneckenganges (2) beträgt.
     
    9. Gleitschalungsextruder, wie in Anspruch 1 beansprucht, dadurch gekennzeichnet, daß die Schneckengänge (2, 25) in bezug auf ihre entsprechenden kernbildenden Dorne (3, 30) synchron und gegenphasig hin- und herbewegbar sind.
     
    10. Gleitschalungsextruder, wie in Anspruch 1 beansprucht, dadurch gekennzeichnet, daß die kernbildenden Dorne (3, 30) so ausgelegt sind, daß sie unabhängig von der Bewegung der entsprechenden Schneckengänge (2, 25) eine Oszillations-Drehbewegung durchführen.
     


    Revendications

    1. Extrudeuse à coffrages glissants utilisable pour la fabrication d'éléments creux en béton (23), de construction mobile par rapport à un lit de coulée (4) et comprenant

    - un châssis (18) qui est mobile et, par exemple, supporté par des roues (19),

    - au moins deux vis d'Archimède (2, 25) comportant des spires (5), supportées en parallèle sur des paliers dans le châssis (18),

    - un système de transmission de puissance et d'entraînement principal (7, 15, 16, 17) pour la mise en rotation des vis (2),

    - un mandrin de formation de cavité (3) fixé à l'extrémité de sortie de chaque vis (2) et relié à un système de transmission de puissance et d'entraînement secondaire, et

    - un dispositif d'alimentation fixé au châssis (18), par exemple une trémie (1), pour distribuer le mélange de béton à couler sur les vis (2), caractérisée en ce que les mandrins de formation de cavité (3, 30) qui prolongent les vis adjacentes (2, 25) sont prévus pour être déplacés au moyen du système de transmission de puissance et d'entraînement secondaire (8,...14), d'une manière synchronisée et en opposition de phase dans la direction axiale l'un par rapport à l'autre, de sorte qu'une fente annulaire (29) définie entre l'extrémité de sortie des vis (2, 25) et les mandrins de formation de cavité correspondants (3, 30) s'élargit et se rétrécit alternativement du fait du mouvement relatif entre la vis (2, 25) et le mandrin de formation de cavité correspondant (3, 30) qui se déplace en opposition de phase.


     
    2. Extrudeuse à coffrages glissants suivant la revendication 1, caractérisée en ce que le système de transmission de puissance et d'entraînement secondaire comprend un actionneur (14), un moteur électrique, ainsi qu'un dispositif à manivelle (10) entraîné par le moteur et qui agit sur des tiges (8) connectées aux mandrins de formation de cavité adjacents (par exemple 3 et 30) et passant dans les vis correspondantes (2 et 25).
     
    3. Extrudeuse à coffrages glissants suivant la revendication 1, caractérisée en ce que la fréquence du mouvement alternatif des mandrins de formation de cavité (3) est de 0, 3 à 100 Hz et de préférence de 5 à 10 Hz.
     
    4. Extrudeuse à coffrages glissants suivant la revendication 1, caractérisée en ce que l'amplitude du mouvement alternatif (longueur de course) des mandrins de formation de cavité (3) est de 0,5 à 50 mm et de préférence de 10 mm environ.
     
    5. Extrudeuse à coffrages glissants suivant la revendication 1, caractérisée en ce que le pas de la spire (5') de chaque vis (2') diminue progressivement dans la direction de distribution.
     
    6. Extrudeuse à coffrages glissants suivant la revendication 5, caractérisée en ce que le pas de la spire (5') à l'extrémité de sortie de la vis (2') est de 30 à 70%, et de préférence de 50% environ, du pas de la spire (5') à l'extrémité d'entrée de la vis (2').
     
    7. Extrudeuse à coffrages glissants suivant la revendication 1, caractérisée en ce que chaque vis (2) et son noyau (26) ont une construction de diamètre sensiblement constant.
     
    8. Extrudeuse à coffrages glissants suivant la revendication 1, caractérisée en ce que la hauteur du profil de la spire (5) est de 3 à 10% du diamètre de la vis (2).
     
    9. Extrudeuse à coffrages glissants suivant la revendication 1, caractérisée en ce que les vis (2, 25) sont prévues pour se déplacer de manière alternative synchronisée et en opposition de phase par rapport à leurs mandrins de formation de cavité correspondants (3, 30).
     
    10. Extrudeuse à coffrages glissants suivant la revendication 1, caractérisée en ce que les mandrins de formation de cavité (3, 30) sont prévus pour se déplacer suivant un mouvement rotatif oscillant, non lié au mouvement des vis correspondantes (2, 25).
     




    Drawing