JP5460749B2 - Cross-flow fan, blower and air conditioner - Google Patents

Description

  The present invention relates to a cross-flow fan used in an indoor unit of an air conditioner, a blower using the same, and an air conditioner.

In recent years, blowers and air conditioners have a larger required capacity to cope with a large room. For this purpose, it is required to increase the air volume of the blower. In order to save energy and improve comfort, blowers and air conditioners are required to have low input and low noise. There are cases where these objectives are realized by the fan blade shape.
(1) For example, there is a case where noise generation is suppressed by matching the direction in which the airflow flows into the blade and the inlet angle of the blade (for example, Patent Document 1).
(2) There is also a case where the sound generation timing is shifted by changing the fan outer diameter in the width direction (for example, Patent Document 2 and Patent Document 3).
(3) In addition, there is an example in which the chord length in the impeller axial direction is changed to uniform the axial wind speed distribution (for example, Patent Document 4).

Japanese Patent Laying-Open No. 2006-329099 (page 7, FIG. 1) Japanese Patent Laid-Open No. 9-1000079 (page 6, FIG. 2) JP 2001-50189 A (page 4, FIGS. 1 and 3) Japanese Patent Laid-Open No. 10-77788 (page 6, FIG. 4) International Publication No. 2006/35933

  Since the conventional cross-flow fan has the same blade cross-sectional shape in the width direction, the location where the direction of the blade row matches the direction of the airflow flowing into the blade row in the blowing blade row is the same position in the width direction. The wind speed increased locally. The energy loss when passing between the blades is proportional to the square of the wind speed, and the noise is proportional to the sixth power of the wind speed. For this reason, when the wind speed increases, the fan input deteriorates and the noise increases. In addition, because a high-speed mainstream remains locally in the air path after blowing out from the fan, vortices are generated due to the speed difference and energy loss increases, and high-speed flow collides with the airflow control vane at the outlet. Therefore, there is a problem that pressure fluctuation increases and noise increases. As shown in Patent Document 1, when the outlet angle on the fan outer peripheral side is changed in the width direction, the blowing position can be shifted by adjusting the ventilation resistance of the blade row by the magnitude of the angle. However, if the exit angle is too large, a separation phenomenon occurs in which the flow does not follow the blades in the blade row on the suction side, and a vortex is generated at the blade tip, resulting in increased energy loss and noise. Therefore, it is difficult to distribute the blown air volume over a wide range by controlling only the fan outer peripheral side.

  Further, when the fan outer diameter is changed as in Patent Document 2 and Patent Document 3, the length of the chord can be changed to increase or decrease the wind speed, and the wind speed distribution in the air path is made uniform. However, since the direction of the tip of the suction blade row changes depending on the fan diameter, if there is a place where the flow is along the blade, there will be a place where large separation occurs, and it is difficult to reduce the energy loss and noise of the entire blower. In addition, since the seal positions of the fan and the stabilizer (nose) are not the same in the width direction, there is a possibility that a leakage flow occurs and the blown-out air volume decreases. Further, when the fan diameter is increased, vibration is increased when a blade having a non-uniform thickness is manufactured due to manufacturing variations.

  In the case of changing the chord length in the axial direction as in the case of Patent Document 4, it seems that the wind speed distribution in the impeller axis direction can be made uniform, but it seems difficult to blow out uniformly in the impeller circumferential direction. It is. In order to blow out uniformly in the circumferential direction of the impeller, it is necessary to provide a clear difference in the blade shape in the rotation axis direction. As shown in FIG. 4 of Patent Document 4, in the blade shape in which the blade shape gradually changes, Like the two-dimensional blades having the same cross section, the blowout flow may concentrate only on a specific blade row.

  An object of the present invention is to reduce the fan input position and noise by reducing the maximum wind speed between the blades by shifting the fan blowing position while preventing the separation flow on the suction side. It is another object of the present invention to provide a blower or an air conditioner that reduces the energy loss and noise of the air passage by uniformizing the wind speed distribution of the air passage after the fan blows out.

The cross-flow fan of this invention
Two or more ring-shaped blade support members disposed at predetermined intervals in the longitudinal direction of the rotation shaft;
In a cross-flow fan comprising a plurality of blades arranged near the outer periphery and spaced apart in the circumferential direction between two adjacent blade support members,
A unit unit that is a constituent part composed of the plurality of blades disposed between two adjacent blade support members,
When cut at a plane between the rotation axis and the normal line at an arbitrary position between the two blade support members, two ends of an end portion far from an intersection of the rotation shaft and the plane and an end portion close to the end portion A section of each wing with a part appears,
End portions of the cross sections of the blades that are far from the intersection point are arranged on the plane of the first circle centered on the intersection point, and end portions of the cross sections of the blades that are close to the intersection point are on the plane surface. Arranged on the circumference of a second circle centered on the intersection at
A cross section of each wing exists between the first circle which is an outer circumference circle and the second circle which is an inner circumference circle,
At least one of the unit units is
When the plane is sequentially cut from the one blade support member toward the other blade support member in the plane, the radius of the second circle, which is the inner circumferential circle, continues with the first radius having a predetermined length. An appearance unit in which a first radius region and a second radius region in which a radius of the second circle which is the inner circumferential circle is continuous with a second radius shorter than the first radius appear,
The appearance unit is
When the plane is sequentially cut from one of the blade support members toward the other blade support member in the plane, the second radius region is one side of the blade support member in the rotation axis direction of the appearance unit and the other The first radiating region appears on both sides of the wing support member and only one first radiating region appears between the two second radiating regions.

  According to the present invention, a low-input, low-noise cross-flow fan can be provided.

1 is a configuration diagram of a cross-flow fan 1 according to Embodiment 1. FIG. FIG. 3 is a cross-sectional view of cross-flow fan 1 according to the first embodiment. FIG. 2 is a schematic view of a blade of cross-flow fan 1 according to the first embodiment. Sectional drawing of the air conditioner 30 using the cross-flow fan 1 of Embodiment 1. FIG. FIG. 3 is a schematic diagram showing an airflow between blades at the height of the fan central axis of the once-through fan 1 according to the first embodiment. FIG. 3 is a schematic diagram showing an airflow between blades in a lower part of the cross-flow fan 1 according to the first embodiment. FIG. 3 is a schematic diagram showing a blown air flow of the once-through fan 1 according to the first embodiment. The schematic diagram of the blowing wind speed distribution of the air blower of the conventional and cross-flow fan 1 of Embodiment 1. FIG. The figure which shows the test result of the air blower using the once-through fan 1 of Embodiment 1. FIG. Sectional drawing of the once-through fan 1 of Embodiment 2. FIG. Sectional drawing of the once-through fan 1 of Embodiment 3. FIG. Sectional drawing of the crossflow fan 1 of Embodiment 4. FIG. Sectional drawing of the once-through fan 1 of Embodiment 5. FIG. FIG. 7 is a schematic view of a blade of a crossflow fan 1 according to a fifth embodiment. Sectional drawing of the once-through fan 1 of Embodiment 7. FIG. FIG. 10 is a cross-sectional view of cross-flow fan 1 according to a ninth embodiment.

Embodiment 1 FIG.
The once-through fan 1 of Embodiment 1 is demonstrated with reference to FIGS. FIG. 1 is a diagram illustrating a structure of a cross-flow fan 1 according to the first embodiment. FIG. 1A is a perspective view showing the appearance of the cross-flow fan 1. FIG. 1B is an enlarged portion between the ring 2 and the ring 2.
FIG.1 (c) is the AA cross section of FIG.1 (b).

  Cross-flow fan 1 includes a plurality of ring-shaped blade support members (hereinafter referred to as rings) arranged at predetermined intervals in the longitudinal direction of rotating shaft 1-1 (FIG. 1A), and two adjacent rings 2 In between, there are a plurality of wings (FIG. 1 (c)) arranged near the outer periphery and spaced apart in the circumferential direction. The cross-flow fan 1 shown in FIG. 1A includes six rings 2, and 35 blades 3 are arranged between two adjacent rings. In FIG. 1A, a component part composed of a plurality of blades attached between two adjacent rings is a single impeller 4 (or a single station). The cross-flow fan 1 in FIG. 1A is composed of five “series” (unit units).

(Cross sectional shape of cross-flow fan 1 blades)
FIG. 2 is a view showing a cross-sectional shape and an appearance of the cross-flow fan 1. FIG. 2A is a view similar to FIG. FIG.2 (b) is a figure which shows SS cross section. FIG.2 (c) is a figure which shows CC cross section. As shown in FIG. 2A, a region between the ring 2-1 and the ring 2-2 in a series is divided into three regions having a predetermined width, and a region S (Side) which is a left region in order from the left. , A region C (Center) which is a central region and a region S which is a right region. The reason why the right and left sides are defined as the region S is that, as will be described later, the right and left sides have the same cross-sectional shape. The widths of these three regions are each 1/3 of one continuous width in the figure. In the region S, the region C, and the region S, the blade cross-sectional shape is changed as follows.

  Hereinafter, the region S close to the ring 2 may be referred to as “ring vicinity”, and the region C in the wing center may be referred to as “wing center”.

  The cross-sectional shapes of the blades in the ring vicinity (region S) and the blade center (region C) are compared. In FIG. 2B showing the SS cross section and FIG. 2C showing the CC cross section, a line (blade center line 5) connecting the centers of the blade thicknesses is formed by an arc. Then, circles (a first circle and a second circle described later having an inner diameter 7 and an outer diameter 8) passing through the center of curvature 6 of the blade tip R portion (the tip tip when there is no R portion) are defined. That is, as shown in FIGS. 2B and 2C, when a series is cut at a plane between the two rings at a normal line with the rotation axis 1-1 as a normal line, the rotation axis 1-1. And a cross section of each wing having two end portions, ie, an end portion 5-1 which is far from an intersection (a point P in FIG. 3 which is the center of the circle) and a near end portion 5-2. The far ends 5-1 of each blade section are arranged on the circumference of a first circle (radius 8, sometimes referred to as an outer diameter) centered on the intersection on the plane. Further, the end portions 5-2 of the cross sections of the blades are arranged on the circumference of a second circle (radius 7; sometimes referred to as an inner diameter) centered on the intersection on the plane. The cross section of each blade (SS cross section, CC cross section) exists between a first circle that is an outer circumference circle and a second circle that is an inner circumference circle (FIGS. 2B and 2C). )).

  Here, the inner diameter 7 and the outer diameter 8 of the blade in the region S (SS section) and the region C (CC section) are compared. Then, as shown in FIGS. 2B and 2C, the blade inner diameter (radius 7c) at the blade central portion is shorter than the blade inner diameter (radius 7s) in the vicinity of the ring (radius 7s> radius 7c). . The blade outer diameter is the same between the series (radius 8s = radius 8c). A short radius with respect to the inner circumferential side circle (second circle) means that the shape of the blade cross section (referred to as the chord length) is long. That is, the chord length in the region C is longer than that in the region S. This relationship is expressed by the lengths with the radii 7s and 7c in FIG. This will also be described in FIG.

(Appearance unit)
As shown in FIGS. 2A to 2C, a series (unit unit) is sequentially formed on a plane having the rotation axis 1-1 as a normal line from one ring 2-1 toward the other ring 2-2. When cut, a region S (first radius region) in which the radius 7 of the second circle, which is an inner circle, continues with a first radius 7a having a predetermined length, and a second radius shorter than the first radius 7a A continuous region C (second radius region) appears at 7c. A series in which the first radius area and the second radius area appear in the series is referred to as an appearance unit. As shown in FIG. 1A, the cross-flow fan 1 is composed of five series. All of the series of five may be appearance units, or at least one may be appearance units. When the appearance unit in FIG. 2A is sequentially cut from one ring 2-1 to the other ring 2-2 along a plane having the rotation axis 1-1 as a normal line, the region S (first radius) (Region) appears on both sides of the ring 2-1 side and the ring 2-2 side of the appearance unit, and a region C (second radius region) appears between the two regions S.

  FIG. 3 shows an external view of the wing 3 attached to the appearance unit. FIG. 3 shows one wing. The external appearance of the wing | blade 3 is a convex shape in which an inner peripheral side changes to the points 31-36 in the rotating shaft 1-1 direction. A step is connected between the region S (the range from the point 31 to the point 32 and the point 35 to the point 36) and the region C (the range from the point 33 to the point 34).

(Air conditioner)
FIG. 4 is a configuration example of an air conditioner 30 using the cross-flow fan 1. A heat exchanger 9 for exchanging heat between the air and the refrigerant is arranged so as to surround the periphery of the once-through fan 1 of the first embodiment. There is also a model in which a dust removing or air cleaning device 10 and a filter 11 are disposed between the heat exchanger 9 and the air outlet 18. The suction side and the blowout side of the cross-flow fan 1 are partitioned by a stabilizer 13 attached to the tip of the nozzle 12 on the front side of the unit and a rear guide 14 on the back side. Due to the rotation of the cross-flow fan 1 (rotation direction 15), the air flow 16 flowing in from the suction port passes through the filter 11, passes through the heat exchanger 9 and exchanges heat, and is then sucked into the blower (range 37), on the opposite side. (Range 38). The airflow that has passed through the air passage is discharged from the outlet 18 along the direction determined by the vane 17 for airflow control.

(Operation)
Next, the operation will be described. The airflow 16 flowing in from the suction port of the blower is sucked into the blade row of the once-through fan 1, passes through the inside of the fan, and blows from the blade row (range 38) opposite to the suction side (range 37) with respect to the fan center. put out. Here, the relationship between the blowing blade row of the fan and the inflow direction of the airflow will be described using the results of the airflow analysis.

(When fan center axis height is 19)
FIG. 5 shows the flow field around the blade row when the blade row is at the fan center axis height 19. FIG. 5A shows a blade row having a fan center axis height 19. FIG. 5B shows a cross section in the vicinity of the ring (corresponding to the SS cross section) at the fan central axis height 19. FIG. 5C shows a cross section of the blade central portion (corresponding to the CC cross section) at the fan center axis height 19. The direction 20 of airflow flowing into the wing (relative speed as viewed from the coordinate system of the rotating wing) and the direction of the chord line 21 (straight line connecting the inner and outer wing tips) are substantially parallel to each other. Since the draft resistance of the cascade is dominated by friction, the difference in draft resistance between the two cascades is small. Since the long chord wing gives a lot of energy to the air blown out, the blowing wind speed at the central portion (region C) of the long wing becomes high. That is, when the fan center axis height is 19, the blown wind speed is higher in the long chord blade region.

(In the case of the lower unit 22)
FIG. 6 shows the flow field around the cascade as the cascade rotates and moves to the lower unit 22. FIG. 6A shows the blade row at the unit lower part 22. FIG. 6B shows a cross section near the ring (corresponding to the SS cross section) at the unit lower part 22. FIG. 6C shows a cross section of the blade central portion (corresponding to the CC cross section) at the unit lower portion 22. When the blade row rotates and moves to the unit lower part 22, the blade central part (FIG. 6C) has inlet / outlet directions 23 and 24 (blade inlet / outlet directions) rather than the ring vicinity (FIG. 6B). The angle θ ₂₅ formed by the tangential direction of the blade center line at the tip is large (θ _25S <θ _25C ). Therefore, air flow 20 is because the air flow deflecting the inflow-outflow when passing between blades increases, ventilation resistance as the angle theta ₂₅ is large is increased. Therefore, speed of air blowing from the short chord blade row angle theta ₂₅ is small small resistance is increased.

  FIG. 7 shows the trajectory of the airflow blown out from the blade row of the fan center axis height 19 (FIG. 7A) and the unit lower part 22 (FIG. 7B) in the cross-flow fan 1. FIG. 7A shows the airflow in the region C (long chord blade region) at the fan center axis height 19. As will be described later with reference to FIG. 8A, it is difficult for the airflow to blow out from the blade row at the fan center axis height 19, but since the region C is a long chord blade, the effect of FIG. The airflow 26 a is blown out from between the 19 blades, and the airflow 26 a flows along the air path lower side 41. FIG. 7B shows the airflow in the region S (short chord blade region) in the unit lower part 22. As will be described later with reference to FIG. 8A, the air flow from the blade row is difficult to blow out at the unit lower portion 22, but the air flow 26b is blown out from between the blades of the unit lower portion 22 due to the effect described with reference to FIG. Flows along the upper wind path. At the position between the fan center axis height 19 and the unit lower part 22, the air flow is blown from the top to the bottom of the air path so that it is uniform in the air path height direction. A straight flow is formed. Further, since the air is also blown between the blade center portion and the ring vicinity portion, the blown airflow is also dispersed in the fan width direction. Thus, in the once-through fan 1 of the first embodiment, the blown airflow can be dispersed in the circumferential direction and the width direction.

  FIG. 8A shows a conventional fan blowing state. The conventional fan is in the same blowing state in each cross section. FIG. 8B corresponds to a state in which the blowout states of the cross sections of the appearance unit of the cross-flow fan 1 are overlapped. In the conventional fan shown in FIG. 8A, the blown airflow is biased between local blades. That is, in the conventional fan, the airflow is difficult to blow out at the fan center axis height 19 or the unit lower part 22. On the other hand, as shown in FIG. 8A, the air current is blown out locally in the direction of 45 degrees at the lower right. On the other hand, in the once-through fan 1 of the first embodiment, as shown in FIG. 8 (b), the blown airflow is not biased between the local blades but is dispersed in the fan circumferential direction, so that the blowout range is widened. If the same air volume is compared, the maximum wind speed passing through the blade row is reduced when the blowing range is wider, so that energy loss and noise when passing through the blade row are reduced. Further, since the local high speed region is eliminated in the air path downstream of the fan, the air speed distribution 27 is made uniform, the maximum air speed passing through the air path and the airflow control vane is reduced, the pressure loss is reduced, and the energy loss is reduced. Can be suppressed. Since the maximum wind speed is reduced, noise generated in the wind path is also reduced. In cross-flow fan 1 of the first embodiment, the airflow distribution is controlled by changing the shape of the inner periphery of the blade, so that separation that occurs at the outer periphery of the blade of the fan suction portion is not induced. Therefore, the airflow can be controlled without increasing noise on the suction side.

  Cross-flow fan 1 according to the first embodiment has a difference in blade shape (the size of blade inner diameter) between impellers alone (between rings on both sides) and ensures a range of different blade shapes by a predetermined width. , Enabling blowing airflow. If the blade shape is gradually changed as in Patent Document 4 cited in the background art, the difference in ventilation resistance of the blowing blade row becomes weak, so there is a possibility that the flow is biased to the local blade row, and the circumferential blowing is performed. Becomes difficult. In the once-through fan 1 of the first embodiment, the axial width with the same blade shape is set to 1/4 or more of the blade length of one impeller series so that the airflow blowing action works.

  FIG. 9 is a diagram showing a comparison result between the cross-flow fan 1 and the conventional fan. An experiment of a blower using the once-through fan 1 of the first embodiment was conducted, and in the once-through fan 1 of the first embodiment, as shown in FIG. 9, the torque load of the fan at the rated air volume (18 m3 / min) of the air conditioner Was reduced by about 3%, and noise was confirmed to be reduced by 0.3 dB.

  As described above, the cross-flow fan 1 according to the first embodiment widens the blowing range of the blade row so that a high-speed blowing flow is not locally generated. As a result, energy loss of the airflow passing between the blades can be reduced, and noise generated between the blades can be reduced. Moreover, since the high-speed flow of an air path can be suppressed, the air blower and air conditioner which can reduce the energy loss and noise in an air path are realizable.

  In the first embodiment, the following cross-flow fan 1 has been described. The cross-flow fan 1 includes a plurality of impellers (a series) composed of a plurality of blades and a ring that supports them connected to each other in the rotational axis direction of the impeller. Inhale and blow out the air to the other. In this cross-flow fan 1, blades sandwiched between rings (a series of blades) are divided into regions having a predetermined width in the rotation axis direction, the center of the blade is the central portion of the blade, and the vicinity of the rings on both sides is the vicinity of the ring , The inner diameter of the blade at the center of the blade is smaller than the inner diameter of the blade near the ring. The blade outer diameter is the same for the impeller alone.

Embodiment 2. FIG.
Next, Embodiment 2 will be described with reference to FIG. FIG. 10 shows the shape of the blades of cross-flow fan 1 in the second embodiment. FIG. 10 is substantially the same as FIG. 2, but the exit angles are shown in FIGS. 10 (b) and 10 (c). The characteristics of the cross-flow fan 1 of the second embodiment are as follows. In other words, the exit angle in the region S (short chord blade region) is larger than the exit angle in the region C (long chord blade region).

10B and 10C show examples of cross sections. The cross section of a series of impellers is divided into a ring vicinity (SS cross section) having a predetermined width and a blade center (CC cross section), and the inner diameter of the center is small (the center is a long chord) Wing shape). This is the same as in the first embodiment. When attention is paid to the outer peripheral portion of the blade cross section, the angle (exit angle θ ₂₉₎ formed by the tangent line 28 of the two lines at the point where the blade center line 5 and the blade outer diameter arc 8 (circumference of the first circle) intersect. However, the exit angle θ _{29s in} the vicinity of the ring (short chord blade region) is larger than the exit angle θ _{29c in the} center of the blade (θ _29s > θ _29c ).

Increasing the outlet angle θ ₂₉ reduces the turning resistance of the airflow flowing in and out of the blade row when the blowing blade row is in the unit lower part 22, and thus reduces the ventilation resistance. Accordingly, the region where the draft resistance of the blade row is reduced is enlarged near the lower portion of the unit, so that the blowing range is widened and the blowing air amount is further uniformized. Along with this, the wind speed distribution in the wind path is also made uniform, and the maximum wind speed is further reduced. It is possible to reduce pressure loss and noise generated in the wind direction vane 17 in the air passage or the outlet. In the second embodiment, since the outlet distribution is adjusted for both the inner and outer peripheral shapes of the blade, the change in the exit angle is small, and there is little risk of causing a large separation on the fan suction side.

  In the second embodiment described above, the cross-flow fan 1 in which the exit angle of the blade cross section is larger in the vicinity of the ring than in the center of the blade has been described.

Embodiment 3 FIG.
Next, Embodiment 3 will be described with reference to FIG. FIG. 11 shows the shape of the blades of cross-flow fan 1 according to the third embodiment. FIG. 11 is almost the same as FIG. In the cross-flow fan 1 according to the third embodiment, the region C of the appearance unit (the region of the long chord blade) has a region length from one ring 2-1 to the other ring 2-2 and two regions S on both sides. It is longer than the sum of the region lengths (short chord region). That is, in FIG. 11A, the length of the left region S in the rotation axis direction is Ls (left), the length of the right region S in the rotation axis direction is Ls (right), and the length of the central region C in the rotation axis direction is Let Lc be
Lc> Ls (left) + Ls (right)
It is a relationship.
That is, in FIG. 11, the cross section of a series of impellers is divided into a ring vicinity (region S) having a predetermined width and a blade center (region C), and the inner diameter of the blade center is smaller. The steps so far are the same as those in the first embodiment. When the ratio of the two types of blade shapes in the width direction is compared, the number of blades (region C) having a smaller inner diameter is greater than that of the first embodiment.

  As shown in FIG. 7, the airflow blown out from the fan at the fan center axis height 19 flows along the lower side 41 of the airway along the casing. Since the cross-flow fan 1 of Embodiment 3 has many areas with a small inner diameter (long chord blade area), the amount of air flowing along the casing 41 along the casing increases.

  When the airflow speed passing through the surface of the lower surface side (wind path lower side 41) of the air conditioner is slow, outside air enters during cooling and easily causes condensation and dew dropping on the wall surface, leading to quality deterioration. In order to prevent these, it is only necessary to increase the wind speed to prevent the outside air from entering. Therefore, the width of the blade having a small inner diameter and a long chord length is increased so that the blown airflow is increased at the fan center axis height 19. However, if the air flow is biased only to the lower side of the wind path, a local high-speed flow is generated, resulting in energy loss and increased noise. Since the wing of the third embodiment also includes a short chord wing, the blown airflow is also distributed to the upper airway 42, so that the local high speed region can be prevented and energy loss and noise increase can be suppressed.

  In Embodiment 3 above, when the blades of a single impeller are divided into a blade region having a predetermined width in the rotation axis direction and a blade region having a small inner diameter and a blade region having a large inner diameter, the blade region having a smaller inner diameter is The cross-flow fan 1 having a larger inner diameter than the blade region has been described.

Embodiment 4 FIG.
Next, a fourth embodiment will be described with reference to FIG. FIG. 12 shows the shape of the blades of cross-flow fan 1 according to the fourth embodiment. FIG. 12 is substantially the same as FIG. In the cross-flow fan 1 of the fourth embodiment, contrary to the third embodiment, the region C (the region of the long chord blade) of the appearance unit is the region length from one ring 2-1 toward the other ring 2-2. Is shorter than the sum of the region lengths of the two regions S (short chord regions) on both sides. That is, in FIG. 12A, the length of the left region S in the rotation axis direction is Ls (left), the length of the right region S in the rotation axis direction is Ls (right), and the length of the central region C in the rotation axis direction is Let Lc be
Ls (left) + Ls (right)> Lc
It is a relationship.
That is, as shown in FIG. 12, a series of impeller cross sections is divided into a ring vicinity (region S) and a blade center (region C) having a predetermined width, and the inner diameter of the blade center is small. Comparing the proportion of the two types of blade shapes in the width direction, the number of blades with a larger inner diameter is larger. Contrary to the third embodiment, the amount of air blown from the fan at the unit lower part 22 is increased, and for this reason, the airflow blown in the horizontal direction by the vane 17-2 in FIG. 4 is increased. This wing shape is suitable for increasing the airflow reach and air-conditioning a large room. As in the third embodiment, since long chord blades are combined so that the airflow is not locally deviated, energy loss and noise can be suppressed. Therefore, it is possible to realize an air conditioner that has a long airflow reach, low input, and low noise.

  When a blade of a single impeller is divided into a blade region having a predetermined width in the direction of the rotation axis and a small inner diameter, and a blade region having a large inner diameter, the blade region having a larger inner diameter is wider than the blade region having a smaller inner diameter. The once-through fan 1 has been described.

Embodiment 5 FIG.
Next, the fifth embodiment will be described with reference to FIGS. As shown in FIG. 14, the cross-flow fan 1 according to the fifth embodiment has two ring-side regions S as long chord blade regions and a central portion region C as short chord blades, contrary to the first embodiment. This is the shape of the region. 13 corresponds to FIG. 2, and FIG. 14 corresponds to FIG. As shown in FIG. 14, when the appearance unit is sequentially cut from one ring 2-1 toward the other ring 2-2 along a plane having the rotation axis 1-1 as a normal line, a region S (with a radius of 7 s) A long chord blade region) appears on both sides of one ring 2-1 side and the other ring 22-2 side in the rotation axis direction of the appearance unit, and a region C (short chord blade region) having a radius of 7c. Appears between the two regions S.

  FIG. 13 shows a cross section of a series of impellers divided into a ring vicinity (region S) having a predetermined width and a blade center (region C). In the first to fourth embodiments, the blade inner diameter of the blade center (region C) is made smaller than that of the ring vicinity (region S). In the fifth embodiment, the blade inner diameter 7s in the vicinity of the ring is smaller than the blade center portion 7c (radius 7s <radius 7c). FIG. 14 shows an external view of one wing. The appearance is a concave shape transitioning from point 51 to point 56, and the region S and the region C are connected in a stepped shape.

  In the once-through fan 1 of the fifth embodiment, the fan central axis height 19 increases the speed in the vicinity of the ring and the unit lower part 22 increases the speed of the blade center (short chord blade region). And vice versa. However, since the range of cascades that blow out from the fan is expanded and the local high-speed flow is suppressed, the unit with low input and low noise can be realized from the viewpoint of aerodynamic performance, as in the previous examples. . On the other hand, considering the structure, the heavy blades (long chord blades) are supported in the vicinity of the ring, which reduces the deflection of the blade between the two rings. It becomes smaller than the case. Therefore, since the cross-flow fan 1 according to the fifth embodiment reduces not only the airflow noise but also the vibration noise, a lower noise blower and air conditioner can be realized.

  In Embodiment 5 described above, when the blade sandwiched between the rings is divided into regions having a predetermined width in the rotation axis direction, the center of the blade is defined as the central portion of the blade, and the vicinity of the rings on both sides is defined as the vicinity of the ring. The cross-flow fan 1 has been described in which the inner diameter of the blade at the center is larger than the inner diameter of the blade near the ring and the outer diameter of the blade is the same for the impeller alone.

Embodiment 6 FIG.
The sixth embodiment is a case where the second embodiment (exit angle), the third embodiment (region S <region C), and the fourth embodiment (region S> region C) are applied to the fifth embodiment. The example of increasing the exit angle of the blade having a large inner diameter shown in the second embodiment, and the example in which the blade region having a large and small inner diameter in the width direction shown in the third to fourth embodiments is used. It does not depend on whether the part is in the vicinity of the ring or the wing center. For this reason, even if it is a cross-flow fan with the small blade inner diameter of the ring vicinity part, the same effect is acquired. These illustrations are omitted. That is, in the shape of the fifth embodiment, the region C (short chord wing region) of the appearance unit has two region S (long chord wing region) on both sides in the region length from one ring to the other ring. It may be longer than the sum of the region lengths. Alternatively, in the appearance unit region C (short chord blade region), the region length from one ring to the other ring is based on the sum of the region lengths of the two regions S (long chord blade region) on both sides. May be shorter. Further, as in the second embodiment, the exit angle of the short chord blade region may be larger than the exit angle of the long chord blade region.

Embodiment 7 FIG.
Next, Embodiment 7 will be described with reference to FIG. FIG. 15A is an external view of the cross-flow fan 1 according to the seventh embodiment. FIG. 15A shows a case where the series is composed of five. In FIG. 15A, it is assumed that all series are appearance units. Each series is the shape of the appearance unit described in the first embodiment. That is, in each of the five series of blade shapes, the blade inner diameter is smaller in the blade center portion (region C) than in the ring vicinity portion (region S). That is, the region C is a long chord wing region. In the seventh embodiment, the series 4-1 and the series 4-2 at both end portions of the cross-flow fan 1 are characterized in that the blade inner diameter is smaller than the series other than both ends. That is, each of the series 4-1 to the series 4-5 has the wing shape of FIG. 3 of the first embodiment, but the long chord area radius 7c (end of the series 4-1 at both ends and the series 4-2). Part) is smaller than the radius 7c (central part) of a long chord region of a series (for example, series 4-3 of the central part) other than both ends.

  As described above, cross-flow fan 1 according to the seventh embodiment includes at least three or more appearance units, and the appearance units are arranged at both ends in the direction of rotating shaft 1-1. In the appearance units arranged at both ends, the length of the radius of the long chord wing region is shorter than the length of the radius of the long chord wing region of the appearance unit arranged at a position different from both ends.

  As shown in FIG. 7, when the blade inner diameter is small, that is, when the blade chord is long, the wind is easy to blow down. At the end of the unit (fan end), the phenomenon that the outside air flows back from the outlet to the inside of the unit is particularly likely to occur. In the seventh embodiment, the inner diameter of the blade is set at the center of the unit so It is even smaller than the series. In this way, it is possible to improve quality by reducing energy loss and noise by making the blowout wind speed distribution uniform at the central part of the unit and preventing backflow at the end.

  In the seventh embodiment described above, a cross-flow fan 1 having a blade impeller having a small inner diameter is smaller in blade inner diameter of a single impeller disposed at the end of the cross-flow fan than a blade inner diameter of other impeller single blades. Explained.

Embodiment 8 FIG.
In the eighth embodiment, with respect to a series of end portions on both sides of the cross-flow fan 1 of the first embodiment, another series in which the blade inner diameter is small (the length in the rotation axis direction of the long chord region) is arranged at both ends. It is configured to be wider than

  As described above, the cross-flow fan 1 of the eighth embodiment includes at least three or more appearance units and the appearance units are arranged at both ends in the direction of the rotating shaft 1-1. The appearing units arranged at both ends have a longer chord area length in the direction of the rotation axis 1-1 longer than that of the appearing units arranged at positions different from both ends.

  If it does in this way, it will become easy to flow an air path lower part at a fan end, and back flow in a fan end can be prevented like Embodiment 7.

  In the above-described eighth embodiment, the cross-flow fan 1 in which the impeller alone disposed at the end of the cross-flow fan is wider than the other impellers in the region occupied by the blades having a small inner diameter in the single impeller has been described.

Embodiment 9 FIG.
FIG. 16 shows an external view of one blade of cross-flow fan 1 according to the ninth embodiment. The examples up to the embodiments 1 to 8 are examples in which blade shapes having different predetermined widths are mixed in the width direction of a single impeller, and in the point where the blade shape changes, a step difference occurs when the shape changes suddenly. There is a risk of wind noise. In the ninth embodiment, a process (region SC) in the middle of changing the blade shape from the region S to the region C is provided and smoothly joined by a curve. Instead of configuring everything entirely with curves, the straight lines and both ends may be connected with curves along the wing shape. As a result, it is possible to achieve a low noise and a low input by making the blowing flow uniform while suppressing wind noise.

  As described above, in the cross-flow fan 1 according to the ninth embodiment, each blade of the appearance unit is formed in a smooth shape that shifts from the short chord blade region to the long chord blade region.

  In the above Embodiments 1 to 9, the cross-flow fan intended for the blower and the air conditioner has been described, but the same effect can be obtained for other devices using the cross-flow fan, such as an air purifier and a dehumidifier. As a result, low noise and low input can be realized.

  In the ninth embodiment, the cross-flow fan 1 has been described in which a blade of a single impeller has a predetermined width, a region having a large blade inner diameter and a region having a small blade inner diameter, and the two regions are joined in an inclined shape or a curve.

  Although the cross flow fan 1 was demonstrated in the above Embodiments 1-9, it is set as embodiment of the air blower provided with the cross flow fan 1 demonstrated in Embodiment 1-9, or this air flow fan provided with this cross flow fan. Is also possible.

In the above embodiment,
Two or more ring-shaped blade support members disposed at predetermined intervals in the longitudinal direction of the rotation shaft;
In a cross-flow fan comprising a plurality of blades arranged near the outer periphery and spaced apart in the circumferential direction between two adjacent blade support members,
A unit unit that is a constituent part composed of the plurality of blades disposed between two adjacent blade support members,
When cut at a plane between the rotation axis and the normal line at an arbitrary position between the two blade support members, two ends of an end portion far from an intersection of the rotation shaft and the plane and an end portion close to the end portion A section of each wing with a part appears,
End portions of the cross sections of the blades that are far from the intersection point are arranged on the plane of the first circle centered on the intersection point, and end portions of the cross sections of the blades that are close to the intersection point are on the plane surface. Arranged on the circumference of a second circle centered on the intersection at
A cross section of each wing exists between the first circle which is an outer circumference circle and the second circle which is an inner circumference circle,
At least one of the unit units is
When the plane is sequentially cut from the one blade support member toward the other blade support member in the plane, the radius of the second circle, which is the inner circumferential circle, continues with the first radius having a predetermined length. It is an appearance unit in which a first radius region and a second radius region in which a radius of the second circle which is the inner circumference circle is continuous with a second radius shorter than the first radius appear. Explained once-through fans.

In the above embodiment,
The appearance unit is
When the plane is sequentially cut from the one blade support member toward the other blade support member in the plane, the first radius region is one side of the blade support member in the rotation axis direction of the appearance unit and the other. The cross-flow fan described above is characterized in that it appears on both sides of the blade support member and the second radius region appears between two of the first radius regions.

In the above embodiment,
The second radius region of the appearance unit is
A cross-flow fan has been described in which the region length from one blade support member to the other blade support member is longer than the sum of the region lengths of the two radius regions.

In the above embodiment,
The second radius region of the appearance unit is
The cross-flow fan has been described in which the region length from one blade support member to the other blade support member is shorter than the sum of the region lengths of the two radius regions.

In the above embodiment,
The appearance unit is
When the plane is sequentially cut from one of the blade support members toward the other blade support member in the plane, the second radius region is one side of the blade support member in the rotation axis direction of the appearance unit and the other The cross-flow fan described above is characterized in that it appears on both sides of the blade support member and the first radial region appears between two of the two radial regions.

In the above embodiment,
The first radius region of each wing of the appearance unit is
A cross-flow fan has been described in which the region length from one blade support member to the other blade support member is longer than the sum of the region lengths of the two radius regions.

In the above embodiment,
The first radius region of the appearance unit is
The cross-flow fan is characterized in that the region length from one blade support member to the other blade support member is shorter than the sum of the region lengths of the two two-radial regions.

In the above embodiment,
The cross-flow fan is
At least three or more appearance units are included and the appearance units are arranged at both ends in the direction of the rotation axis;
The appearance units arranged at both ends are
A length of the second radius of the second radius region is shorter than a length of the second radius of the second radius region of the appearance unit arranged at a position different from the both ends. Explained once-through fans.

In the above embodiment,
The cross-flow fan is
At least three or more appearance units are included and the appearance units are arranged at both ends in the direction of the rotation axis;
The appearance units arranged at both ends are
The region length of the second radius region from one of the blade support members toward the other blade support member is larger than the region length of the second radius region of the appearance unit arranged at a position different from the both ends. Also explained the cross-flow fan, which is characterized by a long time.

In the above embodiment,
Each wing of the appearance unit is
The cross-flow fan is characterized in that it is formed in a smooth shape transitioning from the first radius region to the second radius region.

In the above embodiment,
Each wing of the appearance unit is
The cross-flow fan is characterized in that the exit angle of the blade cross section of the first radius region is larger than the exit angle of the blade cross section of the second radius region.

  In the above embodiment, the air blower provided with said cross-flow fan was demonstrated.

  In the above embodiment, the air conditioner provided with said cross-flow fan was demonstrated.

  1 Cross-flow fan, 2 ring, 3 blades, 4 impeller unit, 5 blade center line, 6 R or tip of blade tip, 7 blade inner diameter, 8 blade outer diameter, 9 heat exchanger, 10 air cleaning device, DESCRIPTION OF SYMBOLS 11 Filter, 12 Nozzle, 13 Stabilizer, 14 Rear guide, 15 Direction of rotation of cross-flow fan, 16 Airflow passing through air conditioner, 17 Airflow control vane, 18 Air outlet, 19 Fan center axis height, 20 Between blades Airflow direction flowing into the blade, 21 blade chord line, 22 unit lower part, 23 blade row inlet direction, 24 blade row outlet direction, angle formed by 25 23 and 24, 26 air flow blown from between the blades, 27 blown air velocity distribution , 28 Both tangents passing through the intersection of the blade center line and the blade outer diameter, 29 exit angle.

Claims (9)

Two or more ring-shaped blade support members disposed at predetermined intervals in the longitudinal direction of the rotation shaft;
In a cross-flow fan comprising a plurality of blades arranged near the outer periphery and spaced apart in the circumferential direction between two adjacent blade support members,
A unit unit that is a constituent part composed of the plurality of blades disposed between two adjacent blade support members,
When cut at a plane between the rotation axis and the normal line at an arbitrary position between the two blade support members, two ends of an end portion far from an intersection of the rotation shaft and the plane and an end portion close to the end portion A section of each wing with a part appears,
End portions of the cross sections of the blades that are far from the intersection point are arranged on the plane of the first circle centered on the intersection point, and end portions of the cross sections of the blades that are close to the intersection point are on the plane surface. Arranged on the circumference of a second circle centered on the intersection at
A cross section of each wing exists between the first circle which is an outer circumference circle and the second circle which is an inner circumference circle,
At least one of the unit units is
When the plane is sequentially cut from the one blade support member toward the other blade support member in the plane, the radius of the second circle, which is the inner circumferential circle, continues with the first radius having a predetermined length. An appearance unit in which a first radius region and a second radius region in which a radius of the second circle which is the inner circumferential circle is continuous with a second radius shorter than the first radius appear,
The appearance unit is
When the plane is sequentially cut from one of the blade support members toward the other blade support member in the plane, the second radius region is one side of the blade support member in the rotation axis direction of the appearance unit and the other cross-flow fan the emerging on both sides of the side of the wing support member, and only one of the first radius region is characterized by the appearance between two of said second radius regions of. The first radius region of each wing of the appearance unit is
The cross-flow fan according to claim 1, wherein a region length from one of the blade support members toward the other blade support member is longer than a sum of the region lengths of the two second radius regions. The first radius region of the appearance unit is
The cross-flow fan according to claim 1, wherein a region length from one of the blade support members to the other blade support member is shorter than a sum of the region lengths of the two second radius regions. The cross-flow fan is
At least three or more appearance units are included and the appearance units are arranged at both ends in the direction of the rotation axis;
The appearance units arranged at both ends are
A length of the second radius of the second radius region is shorter than a length of the second radius of the second radius region of the appearance unit arranged at a position different from the both ends. The once-through fan according to any one of claims 1 to 3. The cross-flow fan is
At least three or more appearance units are included and the appearance units are arranged at both ends in the direction of the rotation axis;
The appearance units arranged at both ends are
The region length of the second radius region from one of the blade support members toward the other blade support member is larger than the region length of the second radius region of the appearance unit arranged at a position different from the both ends. The cross-flow fan according to claim 1, wherein the cross-flow fan is long. Each wing of the appearance unit is
The cross-flow fan according to any one of claims 1 to 5, wherein the cross-flow fan is formed in a smooth shape transitioning from the first radius region to the second radius region. Each wing of the appearance unit is
The cross-flow fan according to any one of claims 1 to 6, wherein an exit angle of a blade cross section of the first radius region is larger than an exit angle of a blade cross section of the second radius region.   A blower comprising the cross-flow fan according to claim 1.   The air conditioner provided with the cross-flow fan in any one of Claims 1-7.

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