Turbofan, and indoor unit for air conditioning device
A turbo fan and corrugated technology, which is applied in the field of turbo fans and indoor units for air conditioning devices, can solve the problems of not being able to reduce noise and control the airflow of blades, and achieve the effect of low noise
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Embodiment approach 1
[0027] figure 1 It is a perspective view of the turbo fan according to Embodiment 1 of the present invention. figure 2 It is a side view of the turbo fan according to Embodiment 1 of the present invention. image 3 It is a figure which shows the blade|wing of the turbofan concerning Embodiment 1 of this invention.
[0028] like Figure 1 ~ Figure 3 As shown, the turbofan 100 according to Embodiment 1 includes: a hub 1 rotating around an axis O; a main board 2 connected to the hub 1; a shroud 3 having a suction port 31 for sucking air; and a plurality of blades 4 between the shroud 3 .
[0029] On the front edge portion 41 of each blade 4, a wave-shaped protrusion portion 41a is formed. The wavy protrusion 41a is formed by connecting a plurality of protrusions 42 .
[0030] The formation form of the plurality of protrusions 42 will be described using the pitch P. A pitch P is defined as a distance from a valley portion 421 of a protrusion 42 to a valley portion 421 of an...
Embodiment approach 2
[0039] Next, use Figure 5 Embodiment 2 of the present invention will be described. Figure 5 Regarding the turbofan according to Embodiment 2 of the present invention, figure 2 Partial sectional view of the V-V line. In addition, this Embodiment 2 is the same as the said Embodiment 1 except the content demonstrated below.
[0040] like Figure 5 As shown, in the turbofan according to the second embodiment, the wavy protrusions 141 a of the leading edge portion of the blade 104 are partially curved outward in the radial direction viewed from the axis O. As shown in FIG. In other words, the wavy protrusion 141 a of the leading edge portion of the blade 104 is partially curved toward the front in the rotation direction R of the fan. In addition, the wavy protrusion 141a is curved radially outward (towards the front in the rotation direction R) so as to deviate from the extending direction of the blade thickness centerline C of the blade 104 when the wavy protrusion 41a is n...
Embodiment approach 3
[0044] Next, use Figure 5 and Figure 6 Embodiment 3 of the present invention will be described. Figure 5 Regarding the turbofan according to Embodiment 3 of the present invention, figure 2 Partial sectional view of the V-V line. in addition, Figure 6 Regarding the turbofan according to Embodiment 3 of the present invention, figure 2 Partial sectional view of line VI-VI. In addition, this Embodiment 3 is the same as the said Embodiment 1 except the content demonstrated below.
[0045] Figure 6 shown figure 2 The line VI-VI in section shows the ratio Figure 5 shown figure 2 The section along the line V-V in is close to the section of the wavy protrusion 241a at the front edge of the blade 204 on the side of the main board 2 . Figure 6 The local bending amount of the wave-shaped protrusion 241a in the front edge portion of the blade 204 in the fan rotation direction is configured to be larger than Figure 5 The amount of local bending in the fan rotation dir...
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