The present invention relates to a beam construction, particularly to a bearer beam construction, such as a doctor beam, and more specifically to a doctor beam that is used mainly in pulp and paper mills to hold in place a doctor blade, which is intended to scrape excess detrimental particles off the top of a roll. The invention also relates to a method for manufacturing the beam construction.
When reference is made to doctor beams in mills like those mentioned above, this nearly always means massive steel beams, which may be of considerable length, as the rolls used in pulp/paper mills can be quite large and the beam typically extends from one end of the roll to the other.
The steel beams are very heavy, which means that all of the structures must be very strong and stiff. Their large size and weight makes the beams difficult to install and maintain. In addition, such a beam is very expensive.
Attempts have also been made to make composite-construction beams, which are lighter than steel beams. One such is disclosed in U.S. Pat. No. 5,356,519, which discloses an essentially triangular beam, in which the structure is formed by three essentially V-shaped pieces rivetted to each other.
The present invention is intended to create an improved doctor beam. The intention is specifically to lighten the beam while at the same time to give it installability and serviceability characteristics of a whole different order to those of known steel beams. The intention is also to improve the stiffness of a composite-construction beam. Naturally, an additional intention is also to reduce the price of the beam.
The aforementioned and other advantages and benefits of the present invention are achieved in the manner described as characteristic in the accompanying Claims
In the following, the invention is examined in greater detail with reference to the accompanying patent drawings, which show some of the characteristic features of a beam according to the invention.
Thus:
The characteristic features of the method according to the invention will become apparent from the following description.
Thus
The prepreg material is a pre-impregnated so-called B-fabric, in which the impregnating agent is typically an epoxy resin, which in the moulding stage is still in a moldable state. The reinforcement or fabric is, on the other hand, formed from various fibres, most usually glass-fibre and carbon-fibre. The fibre can be oriented as desired, either in one direction or else crosswise in different ways. For example, it is possible to use one-direction tapes, in which case the components of the beam 1 are made by laying the tapes in layers, with the fibres in the different layers crossing each other in different directions. The material is, as such, known and in general use, for example, in the aviation industry. The material is available as a woven fabric and as a tape, i.e. as a one-direction fabric.
In order to be able to have the greatest effect on the strength of the construction, first and second flanges 5 and 6 which come outside the essentially triangular base structure, are formed in the first and second components 2 and 3, 4 respectively, and are brought against each other only in the assembly stage of the beam 1 and, in that stage, are glued onto each other, the joint being secured mechanically, for example, by bolts.
The first component 2 has a linear body with a first end at which the first flange 5 is disposed at an angle. The second component 3-4 has a V-shaped body with an apex and second and third sides 3 and 4, respectively, extending away from the apex to form an open mouth. The second flange 6 is disposed at the extended end of the second side 3. The second flange 6 is oriented at an angle to the side 3, away from the mouth. The first flange portion 5 is connected to the end 5′ of the side 4 within the mouth of the V-shaped body, and the second flange portion 6 is connected to the second end 6′ of the linear body or side 2. The resultant first and second flange structures 5-5′ and 6-6′ are thus two layer. In the finished beam 1, the flanges 5, 5′ and 6, 6′ and act as stiffeners against deflection and vibration, as well as an attachment surface for blade holders 7.
The disclosed manufacturing technique allows the thickness of the materials of the components of the beam to be selected as desired. For example, this can be easily done by laying more layers at points where it is assumed that the stronger material would be advantageous. Obviously, the thickness of the material can be made to vary in both the longitudinal and transverse directions. The deflection, vibration, and similar properties can also be substantially affected by the choice of the type of fabric.
The second flange component 6 of the assembled beam is used to attach the holder 7 of the doctor blade. The doctor blade, which is not marked in the figure, rests on the surface of the roll 8 being doctored, at a short distance from the holder 7.
Various conventional means, mainly screws, which can be adjusted to change the tension in the pre-tensioning rods, exist for tensioning and adjusting the pre- tensioning rods 9, 10 and 12.
In the above, the figures show only one cross-sectional form, though it is exceptionally good and appropriate for this purpose. However, the invention is not restricted to this form, instead, as is known, many other cross-sectional or other shapes can be used to create strong constructions. Various kinds of reinforcing ridges, grooves, or similar can also be used to strengthen the construction. If composite-construction and steel beams are compared to each other in terms of weight and installability, it will be noted that the composite construction is light and slim, even though no kind of reinforcing structure whatever is added to it in practice.
If desired, an adhesive can be led inside the beam according to the invention, for example a hot adhesive to prevent the beam sweating and to promote ventilation in general. The air can be fed mechanically, but even spontaneous ventilation can be created, by making holes oriented in a rational manner at suitable points in the beam. The orientations can be affected by many factors in the beam and its surroundings. One air-feed connection is marked with the reference number 11 in
Number | Date | Country | Kind |
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20041123 | Aug 2004 | FI | national |
Filing Document | Filing Date | Country | Kind | 371c Date |
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PCT/FI2005/000366 | 8/25/2005 | WO | 00 | 2/13/2007 |
Publishing Document | Publishing Date | Country | Kind |
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WO2006/021615 | 3/2/2006 | WO | A |
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WO 2005049919 | Jun 2005 | WO |
Number | Date | Country | |
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20080041011 A1 | Feb 2008 | US |