Propeller fan, air-sending device, and refrigeration cycle apparatus

Patent metadata

Field	Value
Publication number	US-11187239-B2
Application number	US-201716620650-A
Country	US
Kind code	B2
Filing date	Aug 9, 2017
Priority date	Aug 9, 2017
Publication date	Nov 30, 2021
Grant date	Nov 30, 2021

Abstract

A propeller fan according to an embodiment of the present invention includes a shaft provided a rotation axis of the propeller fan, and a blade provided on an outer peripheral side of the shaft. The blade has a trailing edge on a rear side of the blade in a rotation direction of the propeller fan. The trailing edge includes a first trailing edge located on an innermost side of the trailing edge, and a second trailing edge adjacent to and outward of the first trailing edge. Where an innermost point of the first trailing edge is a first connection point, a connection point between the first trailing edge and the second trailing edge is a second connection point, and a straight line that extends through the rotation axis and the first connection point is a reference line, the second connection point is located forward of the reference line in the rotation direction, or located on the reference line, and the second trailing edge is located rearward of the second connection point in the rotation direction.

First claim

The invention claimed is:

1. A propeller fan comprising:
a shaft provided on a rotation axis of the propeller fan; and
a blade provided on an outer peripheral side of the shaft,
wherein the blade has a trailing edge on a rear side of the blade in a rotation direction of the propeller fan, and
wherein the trailing edge includes
a first trailing edge located on an innermost side of the trailing edge, and
a second trailing edge adjacent to and outward of the first trailing edge,
wherein where an innermost point of the first trailing edge is a first connection point, a connection point between the first trailing edge and the second trailing edge is a second connection point, a straight line that extends through the rotation axis and the first connection point is a reference line, and an innermost one of points of tangency between the second trailing edge and a tangent line that extends through the first connection point is a first vertex, the second connection point is located forward of the reference line in the rotation direction, or located on the reference line, the second trailing edge is located rearward of the second connection point in the rotation direction, and a length of the first trailing edge is greater than or equal to a length of part of the second trailing edge that is located between the second connection point and the first vertex and
wherein the length of the first trailing edge is not more than twice the length of the part of the second trailing edge that is located between the second connection point and the first vertex.

2. The propeller fan of claim 1 , wherein the first trailing edge is located forward of the reference line in the rotation direction, or located on the reference line.

3. The propeller fan of claim 1 , wherein a radius of a circle whose center is located on the rotation axis and which passes through the second connection point is smaller than half a difference between a radius of a circle whose center is located on the rotation axis and which passes through an outer peripheral edge of the blade and a radius of a circle whose center is located on the rotation axis and which passes through the first connection point.

4. The propeller fan of claim 1 ,
wherein the blade has a leading edge on a front side of the blade in the rotation direction, and
wherein where a middle point of an arc that connects an innermost part of the leading edge and an innermost part of the trailing edge and has a constant radius from the rotation axis is a first middle point, and a middle point of an arc that connects the leading edge and the trailing edge, which forms an outer peripheral portion of the blade, has a constant radius from the rotation axis, is a second middle point, the first middle point is located upstream of the second middle point in a direction parallel to the rotation axis.

5. The propeller fan of claim 1 ,
wherein the blade is connected to an outer peripheral portion of the shaft, and
wherein where a connection point between the shaft and the leading edge on a forward side of the blade in the rotation direction is a third connection point, the shaft is formed such that a distance between the rotation axis and the first connection point is greater than a distance between the rotation axis and the third connection point.

6. The propeller fan of claim 1 , wherein the blade is one of a plurality of blades provided at an outer peripheral portion of the shaft,
the propeller fan further comprising a joint that is provided adjacent to the shaft and configured to connect two of the blades that are adjacent to each other in a circumferential direction about the rotation axis.

7. An air-sending device comprising:
the propeller fan of claim 1 ;
a drive source configured to give a driving force to the propeller fan; and
a casing that houses the propeller fan and the drive source.

8. A refrigeration cycle apparatus comprising:
the air-sending device of claim 7 ; and
a refrigerant circuit including a condenser and an evaporator,
wherein the air-sending device is configured to send air to at least one of the condenser and the evaporator.

Assignees

• Mitsubishi Electric Corp

Inventors

• Tadokoro Takahide
• Teramoto Takuya
• Yamamoto Katsuyuki
• Ito Hiroya
• Ugajin Yuki
• Hamada Shingo
• Ikeda Takashi
• Abe Takafumi

Classifications

• F25D17/067

  Evaporator fan units · CPC title

• F05D2240/303

  related to the leading edge of a rotor blade · CPC title

• F04D29/384 Primary

  characterised by form · CPC title

• F05D2240/304

  related to the trailing edge of a rotor blade · CPC title

• F25D2317/0681

  Details thereof · CPC title