JP6171955B2 - Axial fan - Google Patents

Axial fan Download PDF

Info

Publication number
JP6171955B2
JP6171955B2 JP2014014537A JP2014014537A JP6171955B2 JP 6171955 B2 JP6171955 B2 JP 6171955B2 JP 2014014537 A JP2014014537 A JP 2014014537A JP 2014014537 A JP2014014537 A JP 2014014537A JP 6171955 B2 JP6171955 B2 JP 6171955B2
Authority
JP
Japan
Prior art keywords
curvature
radial direction
outermost
protrusion
radius
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
JP2014014537A
Other languages
Japanese (ja)
Other versions
JP2015140741A (en
Inventor
宇佐見 卓也
卓也 宇佐見
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Denso Corp
Original Assignee
Denso Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Denso Corp filed Critical Denso Corp
Priority to JP2014014537A priority Critical patent/JP6171955B2/en
Publication of JP2015140741A publication Critical patent/JP2015140741A/en
Application granted granted Critical
Publication of JP6171955B2 publication Critical patent/JP6171955B2/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Description

本発明は、回転軸方向に空気流れを形成する軸流ファンに関するものである。   The present invention relates to an axial fan that forms an air flow in a rotation axis direction.

従来、この種の軸流ファンとして、例えば特許文献1に記載されたものがある。この特許文献1に記載された軸流ファンは、ボス部の周囲に回転方向に沿って複数のブレードが配置され、ブレードの外縁部がリングで繋がれている。また、騒音低減のために、ブレードの前縁または後縁に、径方向に沿って鋸歯状の突起部が複数形成されている。   Conventionally, as this type of axial fan, for example, there is one described in Patent Document 1. In the axial fan described in Patent Document 1, a plurality of blades are arranged around the boss portion along the rotation direction, and the outer edge portions of the blades are connected by a ring. In order to reduce noise, a plurality of serrated projections are formed along the radial direction on the front edge or the rear edge of the blade.

特許第3448136号公報Japanese Patent No. 3448136

ところで、ブレードには遠心力による引張荷重が作用し、突起部の谷部に応力が集中する。より詳細には、ブレードの外縁部がリングで繋がれた軸流ファンでは、最も径方向外側に位置する突起部の谷部に特に大きな応力が発生する。   By the way, a tensile load due to centrifugal force acts on the blade, and stress concentrates on the valley of the protrusion. More specifically, in an axial fan in which the outer edge portions of the blades are connected by a ring, a particularly large stress is generated in the valley portion of the protruding portion located on the outermost radial direction.

そして、突起部の谷部を所定の曲率半径の曲面にすることによって応力集中を避けることができ、突起部の谷部の曲率半径を大きくするほど応力低減効果が大きい。   And stress concentration can be avoided by making the valley part of a projection part into the curved surface of predetermined curvature radius, and the stress reduction effect is so large that the curvature radius of the valley part of a projection part is enlarged.

しかしながら、突起部の谷部の曲率半径を大きくすると、応力低減効果は大きいが騒音低減効果が小さくなってしまうという問題がある。   However, when the curvature radius of the valley portion of the protrusion is increased, there is a problem that the stress reduction effect is large but the noise reduction effect is reduced.

本発明は上記点に鑑みて、ブレードの外縁部がリングで繋がれた軸流ファンにおいて、応力低減効果と騒音低減効果を両立させることを目的とする。   The present invention has been made in view of the above points, and an object of the present invention is to achieve both a stress reduction effect and a noise reduction effect in an axial flow fan in which the outer edges of blades are connected by a ring.

上記目的を達成するため、請求項1に記載の発明では、回転中心に配置されたボス部(1)と、ボス部から径方向外側に向かって延びるとともに、回転方向に沿って複数配置されたブレード(2)と、複数のブレードの外縁部を繋ぐリング(3)と、ブレードの前縁または後縁に形成され、且つ径方向に沿って複数配置された鋸歯状の突起部(21)とを備え、最も径方向外側に位置する突起部(21a)の谷部(211a)の曲率半径は、最も径方向内側に位置する突起部(21b)の谷部(211b)の曲率半径よりも大であることを特徴とする。   In order to achieve the above object, in the invention described in claim 1, the boss portion (1) disposed at the center of rotation, the boss portion extends radially outward from the boss portion, and a plurality of the boss portions are disposed along the rotation direction. A blade (2), a ring (3) for connecting the outer edges of the plurality of blades, and a sawtooth-shaped protrusion (21) formed on the front edge or the rear edge of the blade and arranged in a radial direction. And the radius of curvature of the valley (211a) of the protrusion (21a) located on the outermost radial direction is larger than the radius of curvature of the valley (211b) of the protrusion (21b) located on the innermost radial direction. It is characterized by being.

これによると、径方向外側に位置して大きな荷重が作用する谷部の応力を小さくしつつ、径方向内側に位置する突起部に騒音低減効果を十分に発揮させることができる。   According to this, it is possible to sufficiently exert the noise reduction effect on the protrusions located on the radially inner side while reducing the stress of the valleys located on the radially outer side where a large load acts.

なお、この欄および特許請求の範囲で記載した各手段の括弧内の符号は、後述する実施形態に記載の具体的手段との対応関係を示すものである。   In addition, the code | symbol in the bracket | parenthesis of each means described in this column and the claim shows the correspondence with the specific means as described in embodiment mentioned later.

本発明の一実施形態に係る軸流ファンの正面図である。It is a front view of the axial flow fan concerning one embodiment of the present invention. 一実施形態に係る軸流ファンにおけるブレードの拡大正面図である。It is an enlarged front view of the blade in the axial flow fan concerning one embodiment. 一実施形態に係る軸流ファンの変形例を示すブレードの正面図である。It is a front view of the braid | blade which shows the modification of the axial fan which concerns on one Embodiment.

本発明の一実施形態について説明する。   An embodiment of the present invention will be described.

図1に示すように、本実施形態の軸流ファンは、ボス部1、ブレード2、リング3、および図示しない電動機を備えている。ボス部1、ブレード2、およびリング3は、樹脂にて一体成形されている。   As shown in FIG. 1, the axial fan of this embodiment includes a boss portion 1, a blade 2, a ring 3, and an electric motor (not shown). The boss part 1, the blade 2, and the ring 3 are integrally formed of resin.

ボス部1は、有底円筒状であり、底部中心部に電動機の出力軸(回転軸)が固定されている。すなわち、ボス部1は、回転中心に配置されている。   The boss 1 has a bottomed cylindrical shape, and an output shaft (rotary shaft) of the electric motor is fixed to the center of the bottom. That is, the boss portion 1 is disposed at the rotation center.

ブレード2は、ボス部1の円筒部外周面から径方向外側に向かって延びるとともに、回転方向Rに沿って複数配置されている。また、複数のブレード2の外縁部は、環状のリング3にて繋がれている。   A plurality of blades 2 extend radially outward from the outer peripheral surface of the cylindrical portion of the boss portion 1 and are arranged along the rotational direction R. Further, the outer edge portions of the plurality of blades 2 are connected by an annular ring 3.

図2に示すように、ブレード2の前縁には、径方向に沿って鋸歯状の突起部21が複数配置されている。なお、複数の突起部21のうち最も径方向外側に位置する突起部21aを、以下、最外突起部21aという。また、複数の突起部21のうち最も径方向内側に位置する突起部21bを、以下、最内突起部21bという。   As shown in FIG. 2, a plurality of serrated projections 21 are arranged on the front edge of the blade 2 along the radial direction. In addition, the protrusion part 21a located in the radial direction outermost among the several protrusion parts 21 is hereafter called the outermost protrusion part 21a. In addition, the protrusion 21b located on the innermost radial direction among the plurality of protrusions 21 is hereinafter referred to as an innermost protrusion 21b.

突起部21の谷部211は、所定の曲率半径の曲面になっている。そして、最外突起部21aの谷部211aの曲率半径は、最内突起部21bの谷部211bの曲率半径よりも大きく設定されている。   The valley 211 of the protrusion 21 is a curved surface with a predetermined radius of curvature. And the curvature radius of the trough part 211a of the outermost projection part 21a is set larger than the curvature radius of the trough part 211b of the innermost projection part 21b.

より詳細には、本実施形態においては、最外突起部21aの谷部211aの曲率半径は、他の全ての突起部21の谷部211の曲率半径よりも大きく設定されている。なお、最外突起部21a以外の突起部21の谷部211は、ピン角(すなわち、曲率半径≒0)でもよい。   More specifically, in this embodiment, the radius of curvature of the valley 211a of the outermost protrusion 21a is set to be larger than the radius of curvature of the valleys 211 of all other protrusions 21. Note that the valleys 211 of the protrusions 21 other than the outermost protrusion 21a may have a pin angle (that is, a radius of curvature ≈ 0).

上記構成になる軸流ファンは、ボス部1、ブレード2、およびリング3が、電動機にて回転駆動されることにより、回転軸方向の空気流れを形成する。   In the axial fan configured as described above, the boss portion 1, the blade 2, and the ring 3 are rotationally driven by an electric motor to form an air flow in the rotation axis direction.

このとき、最外突起部21aの谷部211aに特に大きな引張荷重が作用するが、最外突起部21aの谷部211aの曲率半径は大きいため、最外突起部21aの谷部211aへの応力集中が回避され、最外突起部21aの谷部211aの応力は小さくなる。   At this time, a particularly large tensile load acts on the trough portion 211a of the outermost projection portion 21a. However, since the curvature radius of the trough portion 211a of the outermost projection portion 21a is large, the stress on the trough portion 211a of the outermost projection portion 21a. Concentration is avoided and the stress of the valley 211a of the outermost projection 21a is reduced.

一方、最外突起部21a以外の突起部21の谷部211の曲率半径は小さいため、最外突起部21a以外の突起部21では騒音低減効果を十分に発揮することができる。   On the other hand, since the curvature radius of the trough part 211 of the projection parts 21 other than the outermost projection part 21a is small, the noise reduction effect can be sufficiently exerted in the projection parts 21 other than the outermost projection part 21a.

したがって、本実施形態によると、応力低減効果と騒音低減効果を両立させることができる。   Therefore, according to the present embodiment, both the stress reduction effect and the noise reduction effect can be achieved.

なお、上記実施形態においては、最外突起部21aの谷部211aを曲面にしたが、図3に示す変形例のように、最外突起部21aの谷部211aは、平面(すなわち、曲率半径が無限大)であってもよい。   In the above embodiment, the valley 211a of the outermost protrusion 21a is curved, but the valley 211a of the outermost protrusion 21a is flat (that is, the radius of curvature) as in the modification shown in FIG. May be infinite).

(他の実施形態)
上記実施形態では、最外突起部21aの谷部211aの曲率半径を、他の全ての突起部21の谷部211の曲率半径よりも大きくしたが、最外突起部21aの谷部211aを含む径方向外側に位置する複数の突起部21の谷部211の曲率半径を、径方向内側に位置する突起部21の谷部211の曲率半径より大きくしてもよい。
(Other embodiments)
In the said embodiment, although the curvature radius of the trough part 211a of the outermost projection part 21a was made larger than the curvature radius of the trough part 211 of all the other projection parts 21, the trough part 211a of the outermost projection part 21a is included. The curvature radii of the valleys 211 of the plurality of projections 21 located on the radially outer side may be larger than the curvature radii of the valleys 211 of the projections 21 located on the radially inner side.

また、全ての突起部21の谷部211の曲率半径を異ならせ、最内突起部21bから最外突起部21aに向かって順に曲率半径を大きくしてもよい。   Alternatively, the curvature radii of the valleys 211 of all the protrusions 21 may be made different so that the curvature radii increase in order from the innermost protrusion 21b toward the outermost protrusion 21a.

また、突起部21を複数のグループに分け、径方向内側に位置するグループから径方向外側に位置するグループに向かって、谷部211の曲率半径を段階的に大きくしてもよい。   Further, the protrusion 21 may be divided into a plurality of groups, and the radius of curvature of the valley 211 may be increased stepwise from the group located on the radially inner side to the group located on the radially outer side.

また、上記実施形態では、ブレード2の前縁に突起部21を配置したが、ブレード2の後縁に突起部21を配置してもよい。   Moreover, in the said embodiment, although the projection part 21 was arrange | positioned in the front edge of the braid | blade 2, you may arrange | position the protrusion part 21 in the rear edge of the braid | blade 2. FIG.

なお、本発明は上記した実施形態に限定されるものではなく、特許請求の範囲に記載した範囲内において適宜変更が可能である。   In addition, this invention is not limited to above-described embodiment, In the range described in the claim, it can change suitably.

また、上記実施形態において、実施形態を構成する要素は、特に必須であると明示した場合および原理的に明らかに必須であると考えられる場合等を除き、必ずしも必須のものではないことは言うまでもない。   Further, in the above-described embodiment, it is needless to say that elements constituting the embodiment are not necessarily indispensable except for the case where it is clearly indicated that the element is essential and the case where the element is clearly considered to be essential in principle. .

また、上記実施形態において、実施形態の構成要素の個数、数値、量、範囲等の数値が言及されている場合、特に必須であると明示した場合および原理的に明らかに特定の数に限定される場合等を除き、その特定の数に限定されるものではない。   Further, in the above embodiment, when numerical values such as the number, numerical value, quantity, range, etc. of the constituent elements of the embodiment are mentioned, it is particularly limited to a specific number when clearly indicated as essential and in principle. The number is not limited to a specific number except for cases.

また、上記実施形態において、構成要素等の形状、位置関係等に言及するときは、特に明示した場合および原理的に特定の形状、位置関係等に限定される場合等を除き、その形状、位置関係等に限定されるものではない。   In the above embodiment, when referring to the shape, positional relationship, etc. of components, the shape, position, etc., unless otherwise specified and in principle limited to a specific shape, positional relationship, etc. It is not limited to relationships.

1 ボス部
2 ブレード
3 リング
21 突起部
211 谷部
1 Boss 2 Blade 3 Ring 21 Projection 211 Valley

Claims (2)

回転中心に配置されたボス部(1)と、
前記ボス部から径方向外側に向かって延びるとともに、回転方向に沿って複数配置されたブレード(2)と、
複数の前記ブレードの外縁部を繋ぐリング(3)と、
前記ブレードの前縁または後縁に形成され、且つ径方向に沿って複数配置された鋸歯状の突起部(21)とを備え、
最も径方向外側に位置する前記突起部(21a)の谷部(211a)の曲率半径は、最も径方向内側に位置する前記突起部(21b)の谷部(211b)の曲率半径よりも大であることを特徴とする軸流ファン。
A boss part (1) arranged at the center of rotation;
A plurality of blades (2) extending radially outward from the boss portion and arranged along the rotational direction;
A ring (3) connecting outer edges of a plurality of the blades;
A plurality of serrated protrusions (21) formed on the front edge or the rear edge of the blade and arranged in a radial direction,
The curvature radius of the valley portion (211a) of the projection (21a) located on the outermost radial direction is larger than the curvature radius of the valley portion (211b) of the projection (21b) located on the innermost radial direction. An axial fan characterized by being.
最も径方向外側に位置する前記突起部の谷部の曲率半径は、他の全ての前記突起部の谷部の曲率半径よりも大であることを特徴とする請求項1に記載の軸流ファン。   2. The axial fan according to claim 1, wherein a radius of curvature of a valley portion of the protruding portion located on the outermost radial direction is larger than a curvature radius of a valley portion of all the other protruding portions. .
JP2014014537A 2014-01-29 2014-01-29 Axial fan Expired - Fee Related JP6171955B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2014014537A JP6171955B2 (en) 2014-01-29 2014-01-29 Axial fan

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2014014537A JP6171955B2 (en) 2014-01-29 2014-01-29 Axial fan

Publications (2)

Publication Number Publication Date
JP2015140741A JP2015140741A (en) 2015-08-03
JP6171955B2 true JP6171955B2 (en) 2017-08-02

Family

ID=53771256

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2014014537A Expired - Fee Related JP6171955B2 (en) 2014-01-29 2014-01-29 Axial fan

Country Status (1)

Country Link
JP (1) JP6171955B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112610513A (en) * 2020-12-04 2021-04-06 北京航空航天大学 Non-uniform wave-shaped front edge stationary blade and modeling method thereof

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2019052539A (en) * 2016-02-02 2019-04-04 株式会社デンソー Axial blower
USD901669S1 (en) 2017-09-29 2020-11-10 Carrier Corporation Contoured fan blade
CN108591119A (en) * 2018-03-07 2018-09-28 常州祥明智能动力股份有限公司 A kind of axial flow fan vane wheel

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5740693U (en) * 1980-08-19 1982-03-04
JP4972756B2 (en) * 2010-05-19 2012-07-11 宣彦 内藤 A propeller composed of a wing with a forced-axis parallel flow mechanism.
JP5880288B2 (en) * 2012-05-31 2016-03-08 株式会社デンソー Blower

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112610513A (en) * 2020-12-04 2021-04-06 北京航空航天大学 Non-uniform wave-shaped front edge stationary blade and modeling method thereof
CN112610513B (en) * 2020-12-04 2021-08-31 北京航空航天大学 Non-uniform wave-shaped front edge stationary blade and modeling method thereof

Also Published As

Publication number Publication date
JP2015140741A (en) 2015-08-03

Similar Documents

Publication Publication Date Title
JP6171955B2 (en) Axial fan
US8899930B2 (en) Fan
US20150152875A1 (en) Air blower
JP6611940B2 (en) Propeller fan
US20140064941A1 (en) Fan module for a heat exchanger
TWI526625B (en) Counter-rotating axial flow fan
JP5890802B2 (en) Blower assembly
US9206816B2 (en) Axial fan
JP5722367B2 (en) Centrifugal blower
CN104903589A (en) Shrouded axial fan with casing treatment
MY189574A (en) Impeller and axial flow fan
JP2016102467A (en) Blower device
JP6654627B2 (en) Fan wheel
US2779424A (en) Impeller
US20210372426A1 (en) Impeller With A Seamless Connection Of The Impeller Blades To A Disc Body
US9655278B2 (en) Slim fan structure
KR200493597Y1 (en) Blower Blade
US20160160878A1 (en) Blade Of A Ventilator Wheel, Ventilator Wheel And Axial Ventilator
JP2017110555A (en) Fan
JP6487876B2 (en) Impeller and fan equipped with the impeller
JP6433587B2 (en) AC alternator rotor for vehicles
JP6060370B2 (en) Blower
JP6531457B2 (en) Propeller fan
US11136990B2 (en) Edge design of a rotation element and impeller
EP2096318B1 (en) Impeller for multi-blade fan

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20160318

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20161220

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20161222

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20170606

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20170619

R151 Written notification of patent or utility model registration

Ref document number: 6171955

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R151

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

LAPS Cancellation because of no payment of annual fees