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EP 0 229 751 B1 |
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EUROPEAN PATENT SPECIFICATION |
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Mention of the grant of the patent: |
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18.04.1990 Bulletin 1990/16 |
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Date of filing: 12.01.1987 |
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Slipforming extruder for hollow-core concrete elements
Gleitfertiger für Hohldielen aus Beton
Machine à coffrages glissants pour la fabrication éléments creux en béton
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Designated Contracting States: |
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AT BE CH DE FR GB IT LI NL SE |
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Priority: |
17.01.1986 FI 860235
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Date of publication of application: |
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22.07.1987 Bulletin 1987/30 |
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Proprietor: KT-SUUNNITTELU OY |
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SF-37600 Valkeakoski (FI) |
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Inventors: |
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- Seppänen, Aimo
FI-37600 Valkeakoski (FI)
- Järvinen, Lassi
FI-37600 Valkeakoski (FI)
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Representative: Wolfram, Gustav, Dipl.-Ing. |
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Patentanwälte
Sonn, Pawloy, Weinzinger & Wolfram,
Riemergasse 14 1010 Wien 1010 Wien (AT) |
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References cited: :
EP-A- 0 174 923
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EP-A- 0 175 930
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| 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).
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[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.
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).
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.
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).