JPH03294699A - Impeller of blower - Google Patents
Impeller of blowerInfo
- Publication number
- JPH03294699A JPH03294699A JP2097132A JP9713290A JPH03294699A JP H03294699 A JPH03294699 A JP H03294699A JP 2097132 A JP2097132 A JP 2097132A JP 9713290 A JP9713290 A JP 9713290A JP H03294699 A JPH03294699 A JP H03294699A
- Authority
- JP
- Japan
- Prior art keywords
- dimples
- blade
- vanes
- low
- impeller
- 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.)
- Pending
Links
- 230000000694 effects Effects 0.000 abstract description 7
- 238000004299 exfoliation Methods 0.000 abstract 3
- 230000001788 irregular Effects 0.000 abstract 1
- 238000000926 separation method Methods 0.000 description 8
- 238000004519 manufacturing process Methods 0.000 description 4
- 210000003746 feather Anatomy 0.000 description 2
- 241000208140 Acer Species 0.000 description 1
- 238000007664 blowing Methods 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 235000003642 hunger Nutrition 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000001228 spectrum Methods 0.000 description 1
- 230000037351 starvation Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/38—Blades
- F04D29/384—Blades characterised by form
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/68—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers
- F04D29/681—Combating cavitation, whirls, noise, vibration or the like; Balancing by influencing boundary layers especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2240/00—Components
- F05D2240/20—Rotors
- F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor
- F05D2240/306—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor related to the suction side of a rotor blade
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
【発明の詳細な説明】 産業上の利用分野 本発明は送風機の低騒音化技術に関する。[Detailed description of the invention] Industrial applications The present invention relates to a technique for reducing noise of a blower.
従来の技術
従来の送風機は例えば特開平1−96498号公報に示
されるように第7図のような構造になってい九 すなわ
板 略円錐台形のハブfの周囲に複数枚の羽根すを設け
ていた 送風機としてはこの羽根車aを適当なケーシン
グに納へ 矢印の方向に回転させることにより送風作用
を起こしている。羽根車すは羽根車ボス部eにモーター
のシャフトを固定して回転するものである。−またこの
送風機の斜視図である第7図aで、羽根すの反り線上の
切断面は第7図すのように単純な構造になってい九
発明が解決しようとする課題
しかし 上記の構成を有する送風機の構造(よ低騒音化
のために一層の改善が必要である。BACKGROUND ART A conventional blower has a structure as shown in FIG. 7, as shown in, for example, Japanese Unexamined Patent Publication No. 1-96498. As a blower, this impeller a is housed in a suitable casing and rotated in the direction of the arrow to generate the air blowing action. The impeller rotates with the motor shaft fixed to the impeller boss e. - Also, in Fig. 7a, which is a perspective view of this blower, the cut plane on the warp line of the blade has a simple structure as shown in Fig. 7. The structure of the blower (further improvement is required to reduce noise).
一般ζミ 送風機から発生する騒音の1つとして、羽根
の低圧面より流れが剥離を生し 剥離に伴い圧力変動を
発生することが考えられている。本発明(友 これを改
善し 低騒音化を達成しようとするものである。General ζmi One of the noises generated from blowers is thought to be the separation of the flow from the low-pressure surface of the blades, which causes pressure fluctuations. The present invention aims to improve this problem and achieve noise reduction.
課題を解決するための手段
上記問題点を解決するために本発明(よ ハブの周囲に
複数枚の羽根を備え 前記羽根の低圧面側&Q 複数
個の略円形状のディンプルを設けたものである。Means for Solving the Problems In order to solve the above-mentioned problems, the present invention includes a plurality of blades around a hub, and a plurality of approximately circular dimples on the low pressure side of the blades. .
作用 上記手段による作用(よ 以下のとおりである。action The effects of the above means are as follows.
送風機の羽根の低圧面側に 複数個の略円形状的大きな
剥離を低減させる。そのことて 剥離に伴う圧力変動を
低減し より一層の低騒音化を達成するものである。Reduces multiple large approximately circular flakes on the low-pressure side of the blower blade. This reduces pressure fluctuations associated with peeling and achieves even lower noise.
実施例 以下、本発明の実施例について図面を参考に説明する。Example Embodiments of the present invention will be described below with reference to the drawings.
ここで(戴 斜流送風機への適用を例にとって説明する
。Here, we will explain the application to a mixed flow blower as an example.
ま咀 第1図と第2図は 本発明の第1の実施例につい
て説明したものである。Figures 1 and 2 illustrate a first embodiment of the present invention.
第1図a It 送風機羽根車の斜視@ 第1図すは
羽根車の反り線での切断面図である。Fig. 1a It is a perspective view of the blower impeller @ Fig. 1 is a cross-sectional view of the impeller along the warp line.
羽根車a 11 略円錐台形のハブ部fに羽根すが備
えられている。そして、羽根すの低圧面側に複数個の略
円形状のディンプルgが設けられている。Impeller a 11 A substantially truncated conical hub portion f is provided with blades. A plurality of approximately circular dimples g are provided on the low pressure side of the blade.
羽根車ボス部eにモーターシャフトを固定し 適切なケ
ーシングに納へ モーターにより矢印の方dより流出し
ていく。Fix the motor shaft to the impeller boss part e and place it in an appropriate casing.The motor will flow out in the direction of the arrow d.
この時、ディンプルgにより羽根の低圧面側すよりの流
れの剥離が減少し その結果 剥離による圧力変動が低
減され より一層の低騒音効果を有する。第2図に示し
たよう(l:、φ360mmの斜流羽根車(羽根枚数4
枚、オリフィス内径372mm)での風量と騒音の実験
データで(戴 約0.5dB低騒音となっている。また
騒音スペクトラムで(よ 約200H2〜約2500
Hzの広い周波数域で音圧レベルが低下している。At this time, the dimple g reduces flow separation on the low-pressure surface side of the blade, and as a result, pressure fluctuations due to separation are reduced, resulting in an even lower noise effect. As shown in Figure 2 (l:, φ360mm mixed flow impeller (number of blades: 4)
Experimental data on air volume and noise with an orifice inner diameter of 372 mm indicates a low noise level of about 0.5 dB.Also, the noise spectrum shows a range of about 200H2 to about 2500H2.
The sound pressure level has decreased in a wide frequency range of Hz.
第3図(よ 本発明の第2の技術的手段に関して説明し
たものである。FIG. 3 explains the second technical means of the present invention.
第3図でφは略円形状のディンプルgの代表寸法(たと
えば円であれば直微 楕円であれば長軸の長さ)を示t
、、hはディンプルgの深さを示している。ここで、φ
は1mm〜20mmで、hは羽根の厚さ5%〜50%の
範囲のディンプル寸法に限定する。これであれ(渋 第
1の実施例と同様に 羽根の低圧面側b′よりの流れの
剥離を低減できて低騒音効果を有するに加わえ 羽根の
強胆衝撃に対する耐力にも問題は生じなし箋 また
製造上の自由度が広がり、生産性やコスト低減にも寄与
できる。In Fig. 3, φ indicates the representative dimension of the approximately circular dimple g (for example, the length of the direct fine if it is a circle, or the length of the major axis if it is an ellipse).
, , h indicates the depth of the dimple g. Here, φ
is 1 mm to 20 mm, and h is limited to a dimple size within a range of 5% to 50% of the thickness of the blade. In addition to reducing the separation of the flow from the low-pressure side b' of the blade and having a low noise effect (similar to the first embodiment), there is no problem with the blade's resistance to strong impact. Note again
It increases the degree of freedom in manufacturing and can also contribute to productivity and cost reduction.
第4図(よ 本発明の第3の技術的手段に関して説明し
た羽根車の平面図である。FIG. 4 is a plan view of the impeller described regarding the third technical means of the present invention.
すなわ板 ディンプルgの代表寸法φと深さhを前述の
第2の技術的手段に示した範囲の内で種々に異ならせて
、羽根の低圧面側b′に不規則に配列したものである。In other words, the dimples g are irregularly arranged on the low-pressure surface side b' of the blade, with the representative dimensions φ and depth h of the dimples varied within the range shown in the second technical means mentioned above. be.
このよう置 ディンプルgの寸法と配列の両方に不規則
性をもたせると、第1の実施例以上に羽根の低圧面側b
′よりの剥離制御が可能となり、さらにより一層の低騒
音効果を有するものである。If irregularities are created in both the size and arrangement of the dimples g in this arrangement, the lower pressure side b of the blade will be larger than in the first embodiment.
This makes it possible to control peeling more than 100 cm, and has an even further low noise effect.
第5図a、bl;j 本発明の第4の技術的手段に関
して説明した羽根車の平面図である。Fig. 5a, bl;j is a plan view of the impeller described in relation to the fourth technical means of the present invention.
羽根の低圧面側b’cQ 第2の技術的手段に記載し
たディンプルの寸法範囲の内で、同一寸法のディンプル
gを格子状に配列したもの(第4図a)と、チドリ状に
配列したもの(第4図b)である。Low-pressure side b'cQ of the blade Within the dimple size range described in the second technical means, dimples g of the same size are arranged in a lattice pattern (Fig. 4a), and dimples arranged in a zigzag pattern are used. (Figure 4b).
このようなディンプルgの形状と配列に於いても、第1
の実施例と同様番ヘ 羽根の低圧面側b゛よりの流れ
の剥離を防止できるに加わえ 配列が規則的であるため
製造が容易となり生産コストを低減できることになる。Even in such a shape and arrangement of dimples g, the first
In addition to being able to prevent separation of the flow from the low-pressure surface side b of the blade, the arrangement is regular, making it easy to manufacture and reducing production costs.
第6図は 本発明の第5の技術的手段に関して説明した
羽根車の平面図である。FIG. 6 is a plan view of the impeller described regarding the fifth technical means of the present invention.
これ(よ 羽根の低圧面側b′へ 第2の技術的手段に
記載したディンプルの寸法範囲の内で、同一寸法のディ
ンプルgを不規則に配列したものである。このようにデ
ィンプルgの配列に不規則性をもたせると、第1の実施
例以上に羽根の低圧面側b゛よりの流れの剥離制御が可
能となり、さらにより一層の低騒音効果を有するととも
へ 製造発明の効果
以上のように本発明の送風機羽根車であればハブの周囲
に複数枚の羽根を備え 羽根の低圧面側に 複数個の略
円形状のディンプルを設けること六 羽根車が送風作用
をしている時に生じる羽根の低圧面での流れの剥離を低
減できる。このこ七により、剥離に伴なう圧力変動を低
減でき、従来よりも低騒音効果を有する。This (toward the low pressure side b' of the blade) dimples g of the same size are arranged irregularly within the dimple size range described in the second technical means. By creating irregularities in the blade, it is possible to control the separation of the flow from the low-pressure side b of the blade more than in the first embodiment, and to have an even more low noise effect, which is even more effective than the manufacturing invention. Thus, the blower impeller of the present invention has a plurality of blades around the hub, and a plurality of approximately circular dimples are provided on the low-pressure side of the blade. Separation of flow on the low-pressure surface of the blade can be reduced.This reduces pressure fluctuations caused by separation, resulting in a lower noise effect than in the past.
第1図(−a)は本発明の第一の実施例の送風機羽根車
の斜視医 第1図(、b)は本発明の第1の実施例の送
風機羽根車の羽根の反り線での断面図 第2図は同経音
特性@、第3図は本発明の第2の実施例で、ディンプル
の断面図 第4図は本発明の第3平面医 第6図は本発
明の第5の実施例の送風機羽根車の要部平面は 第7図
(ajは従来の送風機羽根車の斜視は 第7図(b)は
従来の送風機羽根車の羽根の反り線での断面図である。
a・・・・羽根取 b・・・・羽楓 C・・・・前縁
d・・・・復tie・・・・羽根車ボス餓 f・・・・
ハブKg・・・・ディング/k b” ・・・・羽根
の低圧面(KL b”・・・・羽根の高圧面倶L φ
・・・・代表寸?& h・・・・深さ。FIG. 1(-a) is a perspective view of the blower impeller according to the first embodiment of the present invention. FIG. 1(-b) is a perspective view of the blower impeller according to the first embodiment of the present invention. Cross-sectional view Figure 2 shows the same transsonal characteristic@, Figure 3 shows the second embodiment of the present invention, Figure 4 shows the third flat surface of the present invention, Figure 6 shows the fifth embodiment of the present invention. The principal parts of the blower impeller according to the embodiment are shown in FIG. a... Feather handle b... Feather maple C... Leading edge
d... Revenge... Impeller boss starvation f...
Hub Kg...Ding/k b"...Low pressure surface of the blade (KL b"...High pressure surface of the blade L φ
...Representative size? & h...depth.
Claims (5)
圧面側に、複数個の略円形状のディンプルを所定密度で
設けた送風機羽根車。(1) A blower impeller including a plurality of blades around a hub, and a plurality of approximately circular dimples provided at a predetermined density on the low-pressure side of the blades.
ルの代表寸法が1mm〜20mmまでで前記ディンプル
の深さが羽根の厚さの5%〜50%までの形状のディン
プルを有する請求項1記載の送風機羽根車。(2) A claim in which the approximately circular dimple provided on the low-pressure surface side of the blade has a typical dimension of 1 mm to 20 mm, and the depth of the dimple has a shape of 5% to 50% of the thickness of the blade. The blower impeller according to item 1.
、それらの種々の寸法のディンプルを不規則に前記羽根
の低圧面側に配列した請求項1記載の送風機羽根車。(3) The blower impeller according to claim 1, wherein the representative dimensions and depths of the dimples are varied and the dimples of various dimensions are irregularly arranged on the low pressure surface side of the blade.
状あるいはチドリ状に配列させた請求項2記載の送風機
羽根車。(4) The blower impeller according to claim 2, wherein dimples of the same size are arranged on the low-pressure side of the blade in a lattice or zigzag pattern.
に、不規則に配列させた請求項2記載の送風機羽根車。(5) The blower impeller according to claim 2, wherein the dimples of the same size are arranged irregularly on the low pressure side of the blade.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2097132A JPH03294699A (en) | 1990-04-12 | 1990-04-12 | Impeller of blower |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2097132A JPH03294699A (en) | 1990-04-12 | 1990-04-12 | Impeller of blower |
Publications (1)
Publication Number | Publication Date |
---|---|
JPH03294699A true JPH03294699A (en) | 1991-12-25 |
Family
ID=14184043
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2097132A Pending JPH03294699A (en) | 1990-04-12 | 1990-04-12 | Impeller of blower |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH03294699A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH05332294A (en) * | 1992-05-29 | 1993-12-14 | Daikin Ind Ltd | Axial fan |
JPH06159297A (en) * | 1992-11-25 | 1994-06-07 | Daikin Ind Ltd | Blower mechanism |
WO2006078083A2 (en) * | 2005-01-24 | 2006-07-27 | Lg Electronics Inc. | Air conditioner |
KR100794644B1 (en) * | 2005-11-01 | 2008-01-14 | 엘지전자 주식회사 | Air Conditioner |
WO2008099854A1 (en) * | 2007-02-13 | 2008-08-21 | Daikin Industries, Ltd. | Impeller for fan |
JP2008223760A (en) * | 2007-02-13 | 2008-09-25 | Daikin Ind Ltd | Impeller for blower |
US8231331B2 (en) | 2008-03-14 | 2012-07-31 | Wayne State University | Reduction of flow-induced noise in a centrifugal blower |
WO2019030868A1 (en) | 2017-08-09 | 2019-02-14 | 三菱電機株式会社 | Propeller fan, blower device, and refrigeration cycle device |
US10539157B2 (en) | 2015-04-08 | 2020-01-21 | Horton, Inc. | Fan blade surface features |
TWI800358B (en) * | 2022-04-25 | 2023-04-21 | 建準電機工業股份有限公司 | Impeller and cooling fan including the same |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6035199A (en) * | 1983-08-04 | 1985-02-22 | Matsushita Electric Ind Co Ltd | Impeller of blower |
JPS6365900B2 (en) * | 1980-04-16 | 1988-12-19 | Bendix Corp |
-
1990
- 1990-04-12 JP JP2097132A patent/JPH03294699A/en active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6365900B2 (en) * | 1980-04-16 | 1988-12-19 | Bendix Corp | |
JPS6035199A (en) * | 1983-08-04 | 1985-02-22 | Matsushita Electric Ind Co Ltd | Impeller of blower |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH05332294A (en) * | 1992-05-29 | 1993-12-14 | Daikin Ind Ltd | Axial fan |
JPH06159297A (en) * | 1992-11-25 | 1994-06-07 | Daikin Ind Ltd | Blower mechanism |
WO2006078083A2 (en) * | 2005-01-24 | 2006-07-27 | Lg Electronics Inc. | Air conditioner |
WO2006078083A3 (en) * | 2005-01-24 | 2007-03-08 | Lg Electronics Inc | Air conditioner |
KR100794644B1 (en) * | 2005-11-01 | 2008-01-14 | 엘지전자 주식회사 | Air Conditioner |
JP2008223760A (en) * | 2007-02-13 | 2008-09-25 | Daikin Ind Ltd | Impeller for blower |
WO2008099854A1 (en) * | 2007-02-13 | 2008-08-21 | Daikin Industries, Ltd. | Impeller for fan |
US8231331B2 (en) | 2008-03-14 | 2012-07-31 | Wayne State University | Reduction of flow-induced noise in a centrifugal blower |
US10539157B2 (en) | 2015-04-08 | 2020-01-21 | Horton, Inc. | Fan blade surface features |
US10662975B2 (en) | 2015-04-08 | 2020-05-26 | Horton, Inc. | Fan blade surface features |
WO2019030868A1 (en) | 2017-08-09 | 2019-02-14 | 三菱電機株式会社 | Propeller fan, blower device, and refrigeration cycle device |
EP3916240A1 (en) | 2017-08-09 | 2021-12-01 | Mitsubishi Electric Corporation | Air-sending device, and refrigeration cycle device |
US11434924B2 (en) | 2017-08-09 | 2022-09-06 | Mitsubishi Electric Corporation | Propeller fan, air-sending device, and refrigeration cycle device |
US11788547B2 (en) | 2017-08-09 | 2023-10-17 | Mitsubishi Electric Corporation | Propeller fan, air-sending device, and refrigeration cycle device |
TWI800358B (en) * | 2022-04-25 | 2023-04-21 | 建準電機工業股份有限公司 | Impeller and cooling fan including the same |
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