Impeller, fan, and air-conditioning apparatus

Patent metadata

Field	Value
Publication number	US-12510095-B2
Application number	US-202218836375-A
Country	US
Kind code	B2
Filing date	Feb 21, 2022
Priority date	Feb 21, 2022
Publication date	Dec 30, 2025
Grant date	Dec 30, 2025

Abstract

An impeller includes a blade including, at its leading edge part, a first leading-edge-side concavity, a leading-edge-side convexity, and a second leading-edge-side concavity, which are positioned in sequence from a radially middle part to an outboard edge part. The first leading-edge-side concavity is a part where the suction side of the impeller is concave. The leading-edge-side convexity is a part where the suction side is convex. The second leading-edge-side concavity is a part where the suction side is concave. At the leading edge part of the blade, the blade has a blade height defined in a direction along the rotational axis of the impeller toward the suction side. The blade height decreases monotonically from the radially middle part toward a first leading-edge-side stationary point, and increases monotonically from the first leading-edge-side stationary point toward a second leading-edge-side inflection point.

First claim

The invention claimed is:

1 . An impeller comprising:
a boss part configured to rotate about a rotational axis; and a blade disposed on an outer periphery of the boss part, the blade being rotatable about the rotational axis together with the boss part, wherein the blade includes
a leading edge part being an edge part located forward in a rotational direction of the blade,
a trailing edge part being an edge part located rearward in the rotational direction,
an outboard edge part being an edge part located at an outboard part of the blade, and
an inboard edge part being an edge part located at an inboard part of the blade,
wherein a direction from the rotational axis, the direction being perpendicular to the rotational axis, is a radial direction, wherein a position on the blade that is midway between the outboard edge part and the inboard edge part is a radially middle part, wherein the blade has a plurality of cylindrical cross-sections centered on the rotational axis, wherein in each of the plurality of cylindrical cross-sections, a span line is defined such that points where a distance from the leading edge part and a distance from the trailing edge part have a predetermined ratio relative to each other are extracted, and the extracted points are interconnected from the inboard edge part to the outboard edge part to form the span line, wherein the span line includes
a middle span line defined by interconnecting, from the inboard edge part to the outboard edge part, the points that are equidistant from the leading edge part and the trailing edge part, and
a leading-edge-side span line located closer to the leading edge part than is the middle span line,
wherein the blade has a spanwise cross-section, the span-wise cross-section being defined as a cross-section taken along the span line and parallel to the rotational axis, wherein a point on the outer periphery of the boss part is a mid-boss point, the point being a midpoint between an end of the leading edge part that is an end located at the boss part, and an end of the trailing edge part that is an end located at the boss part, wherein an imaginary plane passing through the mid-boss point and perpendicular to the rotational axis is a mid-boss imaginary plane, wherein the blade has a blade height, the blade height being defined as a distance between the mid-boss imaginary plane and the blade in a direction of the rotational axis, wherein in the span-wise cross-section taken along the leading-edge-side span line, the blade has, in sequence from the radially middle part to the outboard edge part,
a first leading-edge-side concavity where a suction side of the impeller is concave,
a leading-edge-side convexity where the suction side is convex, and
a second leading-edge-side concavity where the suction side is concave,
wherein a first leading-edge-side inflection point is defined as a boundary point between the first leading-edge-side concavity and the leading-edge-side convexity, wherein a second leading-edge-side inflection point is defined as a boundary point between the leading-edge-side convexity and the second leading-edge-side concavity, wherein the blade has
a first leading-edge-side stationary point between the radially middle part and the first leading-edge-side inflection point,
a second leading-edge-side stationary point between the first leading-edge-side inflection point and the second leading-edge-side inflection point, and
a third leading-edge-side stationary point between the second leading-edge-side inflection point and the outboard edge part,
wherein the blade height in a region between the radially middle part and the first leading-edge-side stationary point decreases monotonically from the radially middle part toward the first leading-edge-side stationary point, wherein the blade height in a region between the first leading-edge-side stationary point and the second leading-edge-side stationary point increases monotonically from the first leading-edge-side stationary point toward the second leading-edge-side stationary point, wherein the blade height in a region between the second leading-edge-side stationary point and the third leading-edge-side stationary point increases monotonically from the second leading-edge-side stationary point toward the third leading-edge-side stationary point, and wherein the blade height in a region between the third leading-edge-side stationary point and the outboard edge part increases monotonically from the third leading-edge-side stationary point toward the outboard edge part.

2 . The impeller of claim 1 ,
wherein the span line includes a trailing-edge-side span line, the trailing-edge-side span line being located closer to the trailing edge part than is the middle span line, and wherein in the span-wise cross-section taken along the trailing-edge-side span line, the blade has, in sequence from the radially middle part to the outboard edge part,
a trailing-edge-side convexity where the suction side is convex, and
a trailing-edge-side concavity where the suction side is concave.

3 . The impeller of claim 2 ,
wherein in the span-wise cross-section taken along the trailing-edge-side span line, the blade has
a trailing-edge-side inflection point defined as a boundary point between the trailing-edge-side convexity and the trailing-edge-side concavity,
a first trailing-edge-side stationary point between the radially middle part and the trailing-edge-side inflection point, and
a second trailing-edge-side stationary point between the trailing-edge-side inflection point and the outboard edge part,
wherein the blade height in a region between the radially middle part and the first trailing-edge-side stationary point decreases monotonically from the radially middle part toward the first trailing-edge-side stationary point, and wherein the blade height in a region between the first trailing-edge-side stationary point and the second trailing-edge-side stationary point increases monotonically from the first trailing-edge-side stationary point toward the second trailing-edge-side stationary point.

4 . The impeller of claim 3 ,
wherein in the span-wise cross-section taken along the trailing-edge-side span line, the blade height of the blade in a region between the second trailing-edge-side stationary point and the outboard edge part increases monotonically from the second trailing-edge-side stationary point toward the outboard edge part.

5 . The impeller of claim 1 , wherein
where in each of the plurality of cylindrical cross-sections of the blade, a straight-line distance between the leading edge part and the trailing edge part is L, with the impeller observed in the direction of the rotational axis, with respect to the radial direction running on the blade, a distance from the rotational axis to a given point on the blade is r, a distance from the rotational axis to the inboard edge part is r1, and a distance from the rotational axis to the outboard edge part is r2, σ has a minimum value falling within a range 0.5<ν<0.75, and has a maximum value falling within a range 0.75<ν<1 where

v
=

(

r
-

r
⁢
1

)

/

(

r
⁢
2

-

Assignees

• Mitsubishi Electric Corp

Inventors

• Hatakenaka Kisho
• Fukui Tomoya
• Sakoda Kenichi
• Saikusa Tetsuji
• Nakao Yuki

Classifications

• F24F1/38

  Fan details of outdoor units, e.g. bell-mouth shaped inlets or fan mountings · CPC title

• F04D29/666

  by means of rotor construction or layout, e.g. unequal distribution of blades or vanes · CPC title

• F04D29/325

  for axial flow fans (blade mountings F04D29/34, blades F04D29/38) · CPC title

• F04D19/002

  Axial flow fans · CPC title

• F05D2240/307

  related to the tip of a rotor blade · CPC title