Blade for industrial axial fan and industrial axial fan comprising such blade

Abstract

A blade for an industrial axial fan including an attachment and an airfoil having a longitudinal axis, the attachment connecting the airfoil to a hub, wherein the attachment has a stiffness and a stiffness distribution that allows the attachment to deform in a way to have at least an inflection point along the longitudinal axis during the operation of the axial fan. The attachment includes a first part for connection to the hub and a second part for connection to a proximal end of the airfoil. The blade further includes a weight fixed at a distal end of the airfoil. The attachment has a decreasing stiffness along its longitudinal direction from the first part to the second part so that during the operation of the axial fan, the attachment deforms and includes the inflection point to thereby induce the blade to vibrate according to a second vibrating mode.

Claims

1. A blade for an industrial axial fan comprising: an attachment and an airfoil having a longitudinal axis, said attachment connecting the airfoil to a hub, wherein the attachment has a stiffness and a stiffness distribution that allows the attachment to deform in a way to have at least an inflection point along the longitudinal axis during the operation of the axial fan, wherein said attachment comprises a first part for the connection to the hub and a second part for the connection to a proximal end of the airfoil; wherein the attachment has a decreasing stiffness along its longitudinal direction from said first part to said second part so that during the operation of the axial fan, the attachment deforms and includes the inflection point to thereby induce the blade to vibrate according to a second vibrating mode.

2. The blade for an industrial axial fan according to claim 1, wherein said attachment comprises a necking zone.

3. The blade for an industrial axial fan according to claim 2 further comprising at least an additional weight fixed at a distal end of the airfoil.

4. The blade for an industrial axial fan according to claim 2, wherein said attachment has an I-shaped profile provided with lateral ribs.

5. The blade for an industrial axial fan according to claim 4 further comprising at least an additional weight fixed at a distal end of the airfoil.

6. The blade for an industrial axial fan according to claim 4, wherein the width and the length of the lateral ribs decrease in size spanwise, along the longitudinal direction.

7. The blade for an industrial axial fan according to claim 6 further comprising at least an additional weight fixed at a distal end of the airfoil.

8. The blade for an industrial axial fan according to claim 1, wherein said attachment has a cross-section with a wall-thickness which decreases along the longitudinal direction.

9. The blade for an industrial axial fan according to claim 8 further comprising at least an additional weight fixed at a distal end of the airfoil.

10. The blade for an industrial axial fan according to claim 1, wherein said attachment comprises a necking zone having a stiffness which is lower compared to the stiffness of both the first part and the second part.

11. The blade for an industrial axial fan according to claim 10 further comprising at least an additional weight fixed at a distal end of the airfoil.

12. The blade for an industrial axial fan according to claim 1, wherein said attachment has a quadrangular cross-section, a rectangular cross-section, a round cross-section, or an oval cross-section.

13. The blade for an industrial axial fan according to claim 12 further comprising at least an additional weight fixed at a distal end of the airfoil.

14. The blade for an industrial axial fan according to claim 1, wherein said attachment has a U-shaped cross-section profile having a pair of lateral ribs.

15. The blade for an industrial axial fan according to claim 14 further comprising at least an additional weight fixed at a distal end of the airfoil.

16. A method for the reduction of the energy transmitted from the blade in accordance with claim 1 to a structure of the industrial axial fan, the method comprising the step of providing the attachment for connecting the blade to the hub, said attachment having the stiffness and stiffness distribution that allows the attachment to deform with the inflection point during the operation of the axial fan.

17. An industrial axial fan characterized in that it comprises a blade according to claim 1.

18. The blade for an industrial axial fan according to claim 1 further comprising at least an additional weight fixed at a distal end of the airfoil.

19. A method for reducing energy transmitted from a fan blade to a hub of an industrial axial fan, the method comprising providing an attachment for connecting the blade to the hub, wherein said attachment has a stiffness and a stiffness distribution that allows the attachment to deform in a way to have at least an inflection point during the operation of the axial fan, wherein said attachment comprises a first part for the connection to the hub and a second part for the connection to the fan blade, the blade includes a distal end having a weight affixed thereto; wherein the attachment has a decreasing stiffness along its longitudinal direction from said first part to said second part so that during the operation of the axial fan, the attachment deforms and includes the inflection point to induce the blade to vibrate according to a second vibrating mode.

Description

DESCRIPTION OF THE DRAWINGS

(1) Further characteristics and advantages of the present invention will become clear from the following detailed description of a preferred embodiment that is merely illustrative and not limitative and is shown in the figures that are attached hereto, in which:

(2) FIGS. 1a, 1b, 2a, 2b, 2c, 2d show different examples of blades for axial fans according to the prior art;

(3) FIG. 3a shows the two deformed conditions of a blade system of the type known in the art in the operating condition;

(4) FIG. 3b shows a scheme of the displacement of a cantilever beam according to a first vibrating mode;

(5) FIG. 4a shows the deformed conditions of a blade according to the present invention;

(6) FIG. 4b shows a scheme of the displacement of a cantilever beam according to a second vibrating mode;

(7) FIG. 5 represents the variation of the dynamic amplification factor with the frequency rate for different values of the damping factor;

(8) FIG. 6a shows an example of a blade of the type known in the art;

(9) FIG. 6b shows a blade according to a first embodiment of the present invention, particularly for axial fans of small/medium sizes, in which the blade comprises an attachment having a necking zone;

(10) FIG. 6c shows a blade according to a second embodiment of the present invention, in which the airfoil comprises a necking zone;

(11) FIG. 7 shows a blade according to a third embodiment of the present invention, particularly adapted in case of axial fans of medium-large size;

(12) FIG. 8 shows an example of blade according to a fourth embodiment of the present invention comprising an attachment which is provided separately from the airfoil and then connected;

(13) FIG. 9 shows a further embodiment of the blade according to the present invention, characterized by an attachment having a U-shaped transversal section;

(14) FIG. 10 shows a further embodiment of the blade according to the present invention, characterized by an attachment cross-section having a thickness which decreases along the longitudinal direction of the attachment.

DESCRIPTION OF THE INVENTION

(15) With reference to the above mentioned Figures, the main task of the present invention is to provide a new blade for industrial axial fans, where the blade, subject to unsteady loads, is forced to vibrate in a way similar to that of the second vibrating mode of a cantilever beam.

(16) This result has been achieved by configuring the design of the blade and, in particular, its attachment and/or the airfoil area nearby, to force the blade to have an inflection point when deforming under unsteady operating loads.

(17) Further advantages can be achieved by configuring the blade weight and/or weight distribution.

(18) The influence of these factors on the behavior of the system is herewith explained. During operation, the alternated forces tend to deform cyclically upward and downward the blade and its attachment. The blade takes naturally a deformed shape as shown in FIG. 4a similar to the second vibration mode, see FIG. 4b. At the same time, the centrifugal force tends to counteract the blade deformation developed according to the first mode. The effect produced by the centrifugal force is linearly dependent on the deformation, whereas the alternated forces are not influenced by deformation.

(19) The stiffness on the attachment plays a key role in with respect to the effectiveness of the centrifugal force. In fact, the stiffness and stiffness distribution of the attachment influences the deformation of the attachment as well as the blade deformation.

(20) An attachment which is stiffer at the hub section and less stiff at the airfoil side amplifies the effectiveness of the centrifugal force.

(21) With a proper variation of the stiffness along the radial direction, an inflection point can be obtained, so that the camber of the deformed blade can be overturned along the radius, allowing the blade to deform similarly to the second vibrating mode.

(22) With respect to the blade weight, the capacity of the centrifugal force to overturn the camber of the deformation depends on its amount and on its radial distribution.

(23) In a typical industrial fan blade the weight distribution is such that it is decreasing from root to tip, because the size and the wall thickness of the airfoil is also decreasing this way.

(24) Therefore the centrifugal force in operation could not be sufficient by itself to generate the requested inflection point in the attachment as desired.

(25) The addition of weights to the tip section amplifies the effectiveness of the centrifugal force and would help the process.

(26) The blade and the axial fan comprising such blade according to the present invention obtain a substantial improvement in reducing the alternated loads with respect to the prior art.

(27) Another important characteristic of the present invention is that it leads to a higher unsteady load resistance when compared to the systems known in the art, including the hinged one, because the span-wise variation of the stiffness, combined with the additional weights at the blade tip, reduce significantly the response of the blade to the alternated loads, particularly at the resonance conditions, as it will be herewith explained.

(28) Considering the blade of the axial fan as a mass-damping-stiffness system and assuming it similar to a simple one-degree-of-freedom (SDoF) system, when the system is dynamically excited with a time dependent force f(t), the equation of motion is the following:
mx(t)+cx(t)+kx(t)=f(t)(3)

(29) Wherein:

(30) m is the blade mass;

(31) c is the damping coefficient;

(32) k is the blade stiffness;

(33) x(t) is the system response;

(34) f(t) is the forcing function.

(35) The solution of equation (3) is the sum of two parts: the homogeneous part describing the free vibration, and the particular part describing the forced response. The free vibrational response of a damped system decays over the time, therefore in a relatively short time the response of the system will correspond to the forced vibration, having the same frequency of the force.

(36) The most common alternated force exciting a fan blade is a simple sinusoidal function with a frequency ; the equation (3) becomes the following:
(m.sup.2+ic+k)X e.sup.it=F.sup.it(4)

(37) Where F and X are respectively the amplitude of the exciting force and the system response. Equation (4) can berewritten in terms of the dynamic variables .sub.n which is the system frequency and which is the damping ratio, both defined as follows:

(38) $\begin{array}{cc}{}_n=\sqrt{\frac{k}{m}}& \left(5\right)\\ =\frac{c}{2\sqrt{km}}& \left(6\right)\\ \frac{X}{X_{\mathrm{st}}}=\frac{1}{\sqrt{{\left(1-{}^2\right)}^2+{\left(2\right)}^2}}& \left(7\right)\end{array}$

(39) Where:

(40) X.sub.st is the system response to a static load F;

(41) is the frequency ratio between the blade and the force (=/.sub.n).

(42) The left-hand side term of equation (7) is called the dynamic amplification factor, and it is the factor by which the displacement responses are amplified due to the fact that the external force is dynamic and not static.

(43) The dynamic amplification factor depends on the frequency rate and the damping factor . Its variation with the frequency rate for different values of the damping factor is shown in FIG. 5.

(44) At the resonance condition, =1, the factor has its maximum value:

(45) $\begin{array}{cc}\frac{X}{X_{\mathrm{st}}}=\frac{1}{2}=\frac{\sqrt{km}}{c}& \left(8\right)\end{array}$

(46) The damping coefficient c depends on the material.

(47) For the present invention, the connecting part stiffness (k) reduction leaves the mass (m) almost unchanged even considering the mass which can be added on the tip of the airfoil, but reduces remarkably the stiffness (k).

(48) In conclusion, with respect to the prior art, the present invention reduces the response to alternated loads in general and in resonance condition in particular.

(49) The present invention can be applied profitably, technically and pricewise, to the whole range of cooling axial fans, from small, i.e. 500 millimeters in diameter, to big size, i.e. 20 meters in diameter, and in both cases when the connecting part is integral with the airfoil and when the attachment is a separated element with respect to the airfoil.

(50) Herewith following will be provided some examples of several preferred embodiments of the present invention.

(51) In a first embodiment of the blade according to the present invention a small/medium size blade is considered, the reference being to FIG. 6b.

(52) Small blades are generally realized as one piece cast aluminum, molded plastic, or fiberglass. In FIG. 6a, a typical small blade according to prior art is shown. In FIG. 6b, a blade according to the invention is represented.

(53) The implementation of the invention in this case is rather simple because the material will be injected in a mould and any shape will be easily obtained.

(54) To optimize the required deformation in the embodiment of FIG. 6b, the blade comprises a connecting part 10 which develops mainly along a longitudinal direction, and comprises a first part 11 for the connection to the huh of the axial fan, a second part 14 for the connection to the airfoil 20, a necking zone 13, and two lateral ribs 15. Further, in the embodiment of FIG. 6b the transversal section of the connecting part 10 has an I-shaped profile provided with lateral ribs 15, extending substantially perpendicular with respect to the longitudinal direction of the connecting part 10, and which could decrease in height and width spanwise, i.e. along the longitudinal direction length of the connecting part 10.

(55) That, added to the eventual thickness and width variation of the core part 12 of the connection part 10, will lead the blade to vibrate in the second vibrating mode.

(56) Along the length of the connecting part 10, i.e. along the longitudinal direction, in the area nearby the inflection section it can be left a necking zone 13 where the stiffness is constant and/or lower compared to the stiffness of both the first part 11 and the second part 14, to improve the minimization of loads and to increase the range of operating conditions where the inflection section lies close to the ideal point.

(57) An additional weight can be fixed up at the tip of the blade, leaving a space in a tip cap with a larger thickness.

(58) In case of medium big blades, i.e. up to 20 meters in diameter of the fan, the connecting part 10 of the blade according to a further embodiment of the present invention shown in FIG. 7 comprises a quadrangular, preferably rectangular, cross-section.

(59) The cross-section of the connecting part 10 decreases along the longitudinal direction, and also the thickness of the rectangular profile decreases along the longitudinal direction, as represented in FIG. 7, from a first part 11 for the connection to the hub of the axial fan to a second part 14 for the connection to a blade or airfoil 20.

(60) The connecting part can be realized in one single piece, made of fiberglass by means of a mold. In this case generally the structure of the material is made by fiberglass tissue laid in moulds and then impregnated with resin.

(61) A cost effective solution can be a trimmed section as represented in FIG. 7.

(62) As an alternative, to allow the blade to vibrate as the second mode, the inflection section can be induced in the first part of the airfoil, reducing locally the stiffness of the profile wall thickness similarly to what disclosed with reference to the first embodiment of FIG. 6b.

(63) This embodiment is exemplified in FIG. 6c, wherein the airfoil 20 comprises a necking zone 13. In this case, the airfoil and the connecting part constitutes a single piece.

(64) The same result can be achieved by reducing the wall-thickness of the cross-section of the blade profile, usually the blades having an hollow profile.

(65) As a further option, an additional weight can be fixed at the tip of the alar profile during the molding operation (part W in FIG. 7) or fixed up with different methods afterwards.

(66) According to a further embodiment of the present invention, the blade can comprise a connecting part 10 which is realized as a separated part with respect to the airfoil 20, as shown in FIG. 8.

(67) In this case the connecting part 10 can be made of fiberglass or an injectable material, and can be connected in various ways internally or externally to the airfoil 20.

(68) FIG. 8 shows the connecting part 10 in a deformed condition, i.e. with the axial fan in an operating condition.

(69) A further example of a preferred embodiment of the blade according to the present invention comprises a connecting part 10 characterized by a. U section comprising lateral ribs 15 as shown in FIG. 9; the width and the lateral ribs can reduce in size spanwise, along the longitudinal direction from a first part 11 for the connection to the hub of the axial fan to a second part 14 for the connection to the airfoil 20, to achieve the desired deformation, with an inflection point in operation.

(70) Several manufacturing systems can be used to produce such a piece; a simple one is cut to size a laminated sheet and then bend it.

(71) The separated connecting part 10 will have a section such to be extended inside the airfoil 20 more than ten percent to better distribute the deformation on a longer stretch and on the same time decreasing the loads on the profile because the connection is closer to tip.

(72) Of course the portion of the connecting part which is inside the airfoil will have the proper clearance to the airfoil walls to deform without touching it.

(73) A further embodiment of a blade for industrial axial fan according to the present invention is shown in FIG. 10, wherein the connecting part 10 of the blade has an hollow-profile with a quadrangular cross-section, the wall-thickness of said cross-section reducing along the longitudinal direction of the connecting part 10, the stiffness of the connecting part decreasing along the longitudinal direction without having a necking zone along the connecting part.

(74) To give some examples, a connecting part of a blade according to the present invention and realized for a small/big size fan to force it to vibrate to the second mode, is provided here below.

(75) For a 10 m diameter fan, the blade will have an overall length of 3.5 m, the stiffness value of the connecting part at the hub connection is 4E10 kgmm2, the ratio of the stiffness at 2 m distance is one fifth of the value at the hub, and the weight at the tip will help the blade to generate a centrifugal force of 34.000 N.

(76) These values could be completely different, for the same fan, when a different type of attachment is used; for example the same effect could be obtained with a three times heavier connecting part and developing a centrifugal force of 60.000 N.