JP6060370B2 - Blower - Google Patents

Description

  The present invention relates to an air blower used in an air conditioner, a ventilation fan, or the like, in which an impeller is blindfolded by a lattice, a slat or the like.

  Conventionally, this type of blower is known to improve performance by making the blade thickness non-uniform (see, for example, Patent Document 1).

  Hereinafter, the blower will be described with reference to FIG.

  As shown in the end view along the circumferential cut surface of the blade 101 in the axial flow impeller of FIG. 7, a rib 102 extending along the rotation direction leading edge 103 of the blade 101 is provided on the negative pressure side surface of the blade 101. The ribs 102 are reinforced by the ribs 102 without being thickened.

  As a result, along with the rotation of the blade 101, a creeping vortex attached to the negative pressure side surface of the blade 101 is generated in a region indicated by reference numeral 104 on the rear side in the rotation direction from the rib 102. As a result, the air flow 105 is separated. As a result, the aerodynamic characteristics and noise characteristics of the axial flow impeller are improved.

  Moreover, what suppresses a deformation | transformation of a wing | blade by a thick part is known. (For example, refer to Patent Document 2).

  Hereinafter, the blower will be described with reference to FIG.

  FIG. 8 shows the position and cross-sectional shape of the blade 113 of the axial-flow impeller 112 where the thickness is increased as compared with the conventional machine. FIG. 8A shows the position, and FIG. 8B shows the cross-sectional shape. Here, as a means for preventing deformation of the wing part, from the position where the front edge of the wing part 113 of the axial-flow impeller 112 is joined to the cylindrical support part 114 which is a support part for supporting the wing part to the center part of the front edge. As shown in FIG. 8C, the thickness of the wing portion in the range 116 connecting the range 115 and the position where the leading edge joins the cylindrical support portion 114 to the center position of the wing tip is centered on the maximum strain generation portion. It is thick.

  Thereby, the deformation amount at the time of rotation of the axial-flow impeller 112 can be reduced, and the performance at the time of design can be ensured. That is, a decrease in air volume can be suppressed, and an increase in noise can be suppressed with the same air volume.

Japanese Utility Model Publication No. 4-21487 JP-A-6-81544

  In the conventional blower devices such as Patent Document 1 and Patent Document 2, the thick part of the leading edge of the blade is uniformly added, but there are obstacles such as lattices and blades near the upstream side of the impeller. If an object is provided, pressure fluctuation will occur on a wide surface because the turbulent airflow from the obstacle is scratched by a thick part with a large surface area, causing pressure fluctuation especially at the outer peripheral part where the peripheral speed is large There was a problem that noise increased.

The present invention, the is intended to solve the conventional problems, by the suppressing airfoil shape pressure fluctuations against turbulent airflow, grid cosmetic near the front edge side of the impeller upstream That wing panel be present as an obstacle, and an object thereof is to provide an inhibiting blower increasing noise.

In order to achieve this object, the present invention provides an axial-flow impeller in which a plurality of blades are fixed to the outer periphery of a hub, an electric motor that rotates the impeller, and an air passage that supports the electric motor. a frame forming, a blower device having a grid-shaped decorative panel secured to the frame in proximity to the front edge side of the blade, the blade is radially in tangential towards the outside of the front edge A blade inner peripheral portion having a large component and a blade outer peripheral portion having a larger circumferential component than the blade inner peripheral portion , and in the projection plane where the impeller and the decorative panel are superimposed, the leading edge is In order not to fit in the lattice-like gap, the blade outer peripheral portion is provided with a leading edge that changes the inclination of the leading edge with respect to the blade inner peripheral portion and protrudes in the rotation direction, and the blade inner peripheral portion has the leading edge. cross section and a substantially arcuate thick portion, the thick portion toward the outer side And Nikuka, a shape obtained by eliminating the pre KinikuAtsu portion at the outermost end, the blade outer peripheral part, which has a blade thickness equal to the name Ru shape, thereby intended to achieve a given objective is there.

According to the present invention, even if there is a lattice-shaped decorative panel near the front edge side of the blade of the impeller, possible to suppress an increase in noise by a suppressing wing shape pressure fluctuations against turbulent airflow And an impeller that improves the strength of the blade mounting portion.

Sectional drawing of the air blower of Embodiment 1 of this invention Perspective view of impeller of same sending device Top view of the blades of the blower Radial sectional view of the air blower blade Schematic diagram showing the relationship between wings and gaps (projected view with impeller and decorative panel superimposed) The graph which shows the effect of the thickness shape of the wing of the same blower Sectional drawing which shows the blade | wing of the conventional air blower The perspective view which shows the impeller of the conventional air blower

The blower according to claim 1 of the present invention forms an air passage by supporting an impeller of an axial flow in which a plurality of blades are fixed to the outer periphery of the hub, an electric motor for rotating the impeller, and the electric motor. a blower device comprising a frame, a grid of the decorative panel secured to the frame in proximity to the front edge side of the blade, said blade, the radial component in the tangential towards the outside of the front edge The front edge is formed of a large blade inner peripheral portion and a blade outer peripheral portion having a larger circumferential component than the blade inner peripheral portion , and the leading edge is the lattice on the projection surface where the impeller and the decorative panel are overlapped. as not fit within Jo clearance, the blade outer peripheral part is provided to protrude in the direction of rotation by changing the inclination of the leading edge to the inner circumferential blade portion, the blade inner circumferential portion of the leading edge, cross There is a substantially arcuate thick portion, thinning the wall thickness portion outwardly side, A shape obtained by eliminating the said thick portion at the outer end, said blade outer peripheral part, a blower which is characterized in that the blade thickness equal to the name Ru shape.

As a result, with respect to the turbulent airflow in the vicinity of the impeller upstream of the impeller, the timing at which the protruding shape collides with the turbulence is shifted in the rotational direction at a location where the rotational speed of the blade outer periphery is large, and the blade inner periphery In the portion where the rotational speed is low, the substantially arc-shaped thick portion of the leading edge can suppress the separation flow against the axial disturbance. In addition, by reducing the thickness of the thick wall part and connecting it to the outer periphery of the protruding blade, the blade shape suppresses pressure fluctuations on the blade surface in order to scratch the airflow near the lattice- shaped decorative panel with the thick surface area with a small surface area. Therefore, even if an obstacle exists in the vicinity of the upstream side of the impeller, an increase in noise can be suppressed.

  In addition, the thickened part is gradually thinned toward the outside of the inner periphery of the blade, and noise sources from vortices that may be generated from the steps are removed, so that the noise rises. A greater effect can be obtained.

  In addition, the thin-wall start portion of the thick portion is characterized by being located at a position of 50 to 70% of the impeller radius, and by securing the thick portion in the region of 50% or less where the peripheral speed is small, Increases the effect of suppressing delamination due to thickening over the influence of pressure fluctuations on a wide surface due to thickening, and connects toward the blade outer periphery where there is no thick part in the region where the peripheral speed is 70% or more. By doing so, it is possible to obtain the most significant effect on the suppression of noise rise.

  In addition, the rear end of the outer periphery of the blade extends to the wake side to the periphery of the motor, and the blade root on the inner periphery of the blade is thickened to increase the strength. Even if the effective area of the blade is increased, the reaction of the blade Therefore, the air volume can be increased without increasing the size of the blower.

(Embodiment 1)
FIG. 1 is a sectional view of a blower according to Embodiment 1 of the present invention, and FIG. 2 is a perspective view of an impeller of the blower. In addition, the wing | blade part of the impeller of FIG. 1 is shown as a meridian surface shape.

  First, the configuration of the first embodiment will be described.

  As shown in FIG. 1, the blower 1 includes an axial-flow impeller 4 in which a blade 2 is fixed to a hub 3, an electric motor 5 connected to the impeller 4 on the downstream side, and an air passage that supports the electric motor 5. And a lattice-shaped decorative panel 7 which is fixed to the frame 6 and is close to the impeller 4 within 25% of the diameter of the impeller.

  Moreover, as shown in FIG. 2, the wing | blade 2 is four sheets.

  Here, as shown in the top view of FIG. 3, the blade 2 has a blade inner periphery in a region where the radial component (A) 11 is larger than the circumferential component (A) 10 of the tangent (A) 9 of the leading edge 8. 12 and the blade outer peripheral portion 16 in the region where the circumferential component (B) 15 is larger than the radial component (B) 14 of the tangent (B) 13 of the leading edge 8 suddenly change the curvature at the boundary point 17. It is connected.

  Further, as shown in FIG. 2, the leading edge from the hub 3 of the blade inner peripheral portion 12 to the thin-wall start portion 18 at a position of 60% of the radius is a thick-wall portion 19 having a substantially arc-shaped cross section. Up to the boundary point 17, the thickened portion that is smoothly reduced to an elliptical shape is the reduced thickened portion 20, and the reduced thickened portion 20 has a blade shape that disappears at the boundary point 17 and is equivalent to the blade thickness. . FIG. 4A shows the A-A ′ section in FIG. 2, FIG. 4B shows the B-B ′ section, and FIG. 4C shows the C-C ′ section.

  As shown in FIG. 2, the blade 2 has a rear end 21 that extends to the upstream side of the electric motor 5, and an area of the blade outer peripheral portion 16 is widened toward the downstream side of the blade as an extended region 22.

  Next, the operation of the first embodiment will be described.

  When the impeller 4 is rotated by the electric motor 5, the air flows through the decorative panel 7 from top to bottom in FIG. Since the decorative panel 7 has a lattice shape, the wind speed locally increases at the gap portion, and the turbulence is generated to come into contact with the wing.

  Here, FIG. 5 shows a schematic diagram of the relationship between the wing 2 and the gap 23 between the decorative panel. In this embodiment, the protrusion 24 is provided on the outer peripheral portion of the wing. However, when there is no protrusion 24, there is a phase in which the front edge 25 without the protrusion and the gap 23 of the decorative panel overlap (FIG. 5 matches). ), A portion having a high wind speed that has passed through the gap 23 of the decorative panel and all the leading edges in the radial direction interfere with each other at the same time, which causes noise generation. This is particularly the blade outer peripheral portion 16 having a high rotational peripheral speed of the blade. It will be a big influence.

  Therefore, as shown in FIG. 5, for example, the protrusion 24 has a triangular shape so that the front edge 25 without the protrusion does not fit in the gap 23 of the decorative panel, and the inclination of the front edge 25 without the protrusion is changed. The cause of noise generation can be suppressed by shifting the timing of interference in the circumferential direction, and this effect can be obtained in any phase during the rotation of the impeller 4.

  In the wing inner peripheral portion 12, since the rotational peripheral speed of the wing is small, the influence of interference with the decorative panel 7 is also reduced. Therefore, similarly to the suppression of peeling by the thick portion 19 near the leading edge shown in the background art. Pressure fluctuations that cause noise can be reduced.

  However, when the thick portion 19 extends to the outer peripheral side, the adverse effect of the disturbance from the decorative panel 7 is received by the large surface area of the thick portion 19, which causes an increase in noise.

  Therefore, in the present invention, the effect of the projecting portion 24 and the thickness portion 19 are reduced by reducing the thickness from the thin-wall start portion 18 to the boundary point 17 so as to be smoothly reduced to the elliptical shape shown in FIG. It can be set as the shape which can obtain the effect of the thick part 20 optimally. By adopting such a shape, it is possible to suppress an increase in noise even if there is an obstacle in the vicinity of the upstream side of the impeller 4.

  FIG. 6 shows the effect of the presence or absence of the reduced thickness portion 20 at an impeller diameter of 80 mm and a rotational speed of 2000 rpm in the first embodiment, the relationship between the air volume and static pressure, and the air volume and noise (noise measurement at a point 1 m ahead of the blower). It is shown in the relationship. Thus, noise can be reduced in the blower having the same air volume-static pressure characteristics.

  Further, since the thick portion 19 is connected to the hub 3 at the base of the blade 2, it serves to reinforce the connection portion between the blade 2 and the hub 3, and sufficient strength can be secured even if the connection portion is not large. Accordingly, the extension region 22 shown in FIG. 2 can be provided, and the extension region 22 increases the effective blade area for scratching the air, so that the air volume can be increased.

  Moreover, although the reduced thickness part 20 is made into the shape which reduces smoothly, it is reducing the material and weight by reducing the volume of the impeller 4 by reducing the thickness of the impeller 4 in a discontinuous manner such as a stepped shape in the middle. Also good.

  The air blower according to the present invention has a blade shape that suppresses pressure fluctuations against a turbulent air flow, so that an increase in noise can be suppressed and an air volume can be increased even if an obstacle exists near the impeller upstream side. Therefore, it is useful as various blower devices that generate an air current in a room where quietness and high blowing ability are required.

DESCRIPTION OF SYMBOLS 1 Blower 2 Wing 3 Hub 4 Impeller 5 Electric motor 6 Frame 7 Cosmetic panel 8 Front edge 9 Tangent (A)
10 Circumferential component (A)
11 Radial component (A)
12 Wing inner circumference 13 Tangent (B)
14 Radial component (B)
15 Circumferential component (B)
16 Blade outer peripheral part 17 Boundary point 18 Thin-walled starting part 19 Thick-walled part 20 Reduced-thickened part 21 Rear end 22 Extended region 23 Gap of decorative panel 24 Projection part 25 Front edge without projection part

Claims (4)

An impeller of the axial flow of fixing a plurality of blades on the outer circumference of the hub, an electric motor for rotating the impeller, and a frame for forming an air path in favor of the electric motor, adjacent the leading edge side of the blade A blower provided with a lattice- shaped decorative panel fixed to the frame,
The wing
Is composed from the front and inner circumferential blade portion the radial component is large in the tangential towards the outer edge, the wing outer peripheral portion and having an increased circumferential component as compared with the inner circumferential blade portion,
In the projection surface where the impeller and the decorative panel are overlapped, the blade outer peripheral portion changes the inclination of the front edge with respect to the blade inner peripheral portion so that the front edge does not fit in the lattice-shaped gap. To project in the direction of rotation,
Said inner circumferential blade portion the leading edge cross-section and a substantially arcuate thick portion, the thick portion thinned toward the outer side, a shape obtained by eliminating the pre KinikuAtsu portion at the outermost end ,
Blower, characterized in that said wings outer peripheral portion, and a blade thickness equal to the name Ru shape. The blower according to claim 1, wherein the thick part is gradually thinned toward the outer side of the inner peripheral part of the blade. The blower according to claim 1 or 2, wherein the thin-wall start portion of the thick portion is at a position of 50 to 70% of the impeller radius. The blower according to any one of claims 1 to 3, wherein a rear end of the blade outer peripheral portion is extended to the wake side around the electric motor.

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