Propeller fan and refrigeration cycle device

Patent metadata

Field	Value
Publication number	US-11002292-B2
Application number	US-201616329369-A
Country	US
Kind code	B2
Filing date	Nov 18, 2016
Priority date	Nov 18, 2016
Publication date	May 11, 2021
Grant date	May 11, 2021

Abstract

A propeller fan includes a boss and a blade. The boss rotates about an axis. The blade is provided at an outer periphery of the boss. The blade has a first region in a radial direction. In the first region, a blade chord center line shifts downstream toward an outer peripheral side. In a cylindrical cross section about an axis, a cross-sectional shape of the blade at least in the first region is an airfoil shape. When a cross section taken along the blade chord center line and projected onto a plane including the axis is viewed, the blade chord center line is a curve having a convex on a downstream side in an entire region in the radial direction.

First claim

The invention claimed is:

1. A propeller fan comprising:
a boss that rotates about an axis; and
a blade provided at an outer periphery of the boss, wherein:
in a radial direction, the blade has a first region, the first region being a region in which a blade chord center line bends downstream away from an inner peripheral end of the blade, and has a second region in which the blade chord center line bends upstream away from an end of the first region and toward an outer peripheral end of the blade, wherein the upstream and downstream is in view of air sending flow generated by a rotation of the blade,
in an axial cross section, viewed along a radial direction of the blade, a cross-sectional shape of the blade in the first region is an airfoil shape and a cross-sectional shape of the blade in the second region is a circular arc shape having substantially constant thickness from a leading edge toward a trailing edge,
when viewing a cross section taken along the blade chord center line and projected onto a plane including the axis, the blade chord center line is a curve having a convex toward a downstream side in an entire region in the radial direction, and
a boundary between the first region and the second region is set to a middle portion of the blade.

2. The propeller fan of claim 1 ,
wherein a rounded portion is provided at a downstream end of the blade at the outer peripheral end.

3. A refrigeration cycle device comprising:
a refrigerant circuit in which a compressor, a first heat exchanger, an expansion device, and a second heat exchanger are connected by pipes,
the propeller fan of claim 1 , and
a cooling unit,
wherein the propeller fan is installed in the cooling unit in conjunction with the first heat exchanger, and supplies air to the first heat exchanger.

4. The refrigeration cycle device of claim 3 ,
wherein the cooling unit includes a casing, the casing having a discharge portion and a suction portion, and the propeller fan is provided upstream of the discharge portion, and
wherein an angle (α) formed by a normal to a discharge plane of the discharge portion and a normal to a suction plane of the suction portion is an acute angle.

5. The refrigeration cycle device of claim 4 ,
wherein the cooling unit is mounted on a vehicle.

6. A propeller fan comprising:
a boss that rotates about an axis; and
a blade provided at an outer periphery of the boss, wherein:
in a radial direction, the blade has a first region, the first region being a region in which a blade chord center line bends downstream away from an inner peripheral end of the blade, and has a second region in which the blade chord center line bends upstream away from an end of the first region and toward an outer peripheral end of the blade, wherein the upstream and downstream is in view of air sending flow generated by a rotation of the blade,
in an axial cross section, viewed along a radial direction of the blade, a cross-sectional shape of the blade in the first region is an airfoil shape and a cross-sectional shape of the blade in the second region is a circular arc shape having a thin-walled portion at a trailing edge of the blade,
when viewing a cross section taken along the blade chord center line and projected onto a plane including the axis, the blade chord center line is a curve having a convex toward a downstream side in an entire region in the radial direction, and
a boundary between the first region and the second region is set to a middle portion of the blade.

Assignees

• Mitsubishi Electric Corp

Inventors

• Nakashima Seiji
• Kato Yasuaki
• Shingu Wahei
• Murakami Hiroaki

Classifications

• F04D29/667

  by influencing the flow pattern, e.g. suppression of turbulence · CPC title

• F05D2240/301

  Cross-sectional characteristics · CPC title

• F25B39/04

  Condensers · CPC title

• F25B2500/12

  Sound · CPC title

• F04D29/66 Primary

  Combating cavitation, whirls, noise, vibration or the like (gas-flow silencers for machines or engines in general F01N); Balancing (surge control F04D27/02) · CPC title