JPH06299997A - Mixed flow fan - Google Patents
Mixed flow fanInfo
- Publication number
- JPH06299997A JPH06299997A JP9111893A JP9111893A JPH06299997A JP H06299997 A JPH06299997 A JP H06299997A JP 9111893 A JP9111893 A JP 9111893A JP 9111893 A JP9111893 A JP 9111893A JP H06299997 A JPH06299997 A JP H06299997A
- Authority
- JP
- Japan
- Prior art keywords
- leading edge
- thickness
- blade
- thick wall
- flow fan
- 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
- 238000000926 separation method Methods 0.000 abstract description 11
- 239000012530 fluid Substances 0.000 abstract description 9
- 238000007664 blowing Methods 0.000 abstract description 3
- 238000009423 ventilation Methods 0.000 description 6
- 239000011347 resin Substances 0.000 description 3
- 229920005989 resin Polymers 0.000 description 3
- 239000000463 material Substances 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000009499 grossing Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
【0001】[0001]
【産業上の利用分野】本発明は、排気送風機器および空
気調和機器に使用される斜流ファンにおける静翼に関す
るものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a stationary blade in a mixed flow fan used in exhaust air blowers and air conditioners.
【0002】[0002]
【従来の技術】近年、居住および非居住空間で使用され
る排気送風機器および空気調和機器は運転時に発生する
騒音を低下することが求められている。2. Description of the Related Art Recently, exhaust blowers and air conditioners used in residential and non-residential spaces have been required to reduce noise generated during operation.
【0003】従来、この種の斜流ファンは、図7および
図8に示すものが一般的であった。以下、その構成に付
いて図を参照しながら説明する。Conventionally, a mixed flow fan of this type is generally shown in FIGS. 7 and 8. The configuration will be described below with reference to the drawings.
【0004】図に示すように、複数の静翼羽根101が
ケーシング102の内壁および内筒106間で等間隔を
保ちながら配置されている。また前縁部103の入口角
は設計点では動翼からでる風向きと同方向になり、後縁
部の出口角は旋回成分をなくし環状の通風口107と平
行に送風されるような形状となっている。As shown in the figure, a plurality of vane blades 101 are arranged at equal intervals between the inner wall of the casing 102 and the inner cylinder 106. At the design point, the inlet angle of the leading edge portion 103 is in the same direction as the direction of the air coming out of the moving blade, and the outlet angle of the trailing edge portion has a shape that eliminates the swirling component and is blown in parallel with the annular ventilation port 107. ing.
【0005】上記構成において斜流ファンの羽根車10
8が回転したときの一般的な通風方向は、斜流ファンを
介して図のようになる。In the above structure, the impeller 10 of the mixed flow fan
The general ventilation direction when 8 rotates is as shown in the figure via the mixed flow fan.
【0006】[0006]
【発明が解決しようとする課題】このような従来の斜流
ファンでは、羽根の入口角と静翼羽根101に流入する
流れの向きが一致していればスムーズな静翼羽根101
に沿った流入状態が保たれるが、使用状態により風量の
変化があり、また羽根車108の回転数も変化し、流入
方向は静翼羽根101の入口角と合わなくなり羽根の前
縁部103で剥離を生じ、送風効率の低下や騒音上昇の
原因につながるという問題があった。In such a conventional mixed flow fan, if the inlet angle of the blade and the direction of the flow flowing into the stationary blade 101 are the same, the stationary blade 101 is smooth.
Although the inflow state along the line is maintained, the air flow rate changes depending on the use state, and the rotation speed of the impeller 108 also changes, so that the inflow direction does not match the inlet angle of the stationary vane blade 101, and the blade leading edge portion 103 However, there is a problem in that peeling occurs, which leads to a decrease in blowing efficiency and an increase in noise.
【0007】本発明は上記課題を解決するもので、使用
状態による性能不安定を解消し、空力学的に良好な性能
を示すと共に、空力騒音も低く抑えることにある。The present invention is intended to solve the above-mentioned problems, and is to eliminate performance instability due to use conditions, to exhibit aerodynamically good performance, and to suppress aerodynamic noise as well.
【0008】[0008]
【課題を解決するための手段】本発明の目的を達成する
ための第1の手段は、ケーシング内に複数枚の羽根を設
けた羽根車と、前記ケーシング内にある略円錐台形の内
筒と、前記羽根車の下流側で前記ケーシングの内壁およ
び前記内筒間にあり、前記内筒を支持する複数枚の静翼
羽根を備え、前記静翼羽根の前縁部の負圧面側に断面形
状が略円弧状の厚肉を設けた構成をしている。A first means for achieving the object of the present invention is an impeller having a plurality of blades provided in a casing, and a substantially frustoconical inner cylinder provided in the casing. A plurality of stationary vane blades that are located between the inner wall of the casing and the inner cylinder on the downstream side of the impeller and support the inner cylinder, and have a cross-sectional shape on the suction surface side of the front edge portion of the stationary vane blade. Has a substantially arc-shaped thick wall.
【0009】また、第2の手段は、静翼羽根の前縁部に
略円弧状の断面形状の厚肉を設けた構成としている。The second means is constructed such that a thick wall having a substantially arcuate cross-sectional shape is provided at the front edge of the vane blade.
【0010】また、第3の手段は、第1の手段の厚肉に
変えて、略円弧状の断面形状を持つリングを設けた構成
としている。The third means has a structure in which a ring having a substantially arcuate cross-sectional shape is provided in place of the thickness of the first means.
【0011】[0011]
【作用】本発明は上記した第1の手段の構成により、静
翼羽根の前縁部の負圧面側の断面形状を静翼羽根の厚さ
より大きく取ることにより、使用状態による吸込流れの
方向が変化して、静翼羽根の前縁部の入口角と方向が異
なっていても肉厚が静翼羽根の転向角の変化を少なくす
るため剥離を防止し、流体流れをスムーズにすることが
できるものである。According to the present invention, by the structure of the above-mentioned first means, the suction flow direction depending on the use condition is changed by making the cross-sectional shape of the front edge portion of the vane blade larger than the thickness of the vane blade. Even if the inlet angle and the direction of the leading edge of the vane blade are changed, the wall thickness reduces the change in the turning angle of the vane blade, thus preventing separation and smoothing the fluid flow. It is a thing.
【0012】また、第2の手段の構成により、静翼羽根
の前縁部の断面形状を静翼羽根の厚さより大きく取るこ
とにより、使用状態による吸込流れの方向が変化して、
静翼羽根の前縁部の入口角と方向が異なっていても剥離
を防止し、しかも開放状態に近い点で流体が負圧面側か
ら流れても厚肉により流体流れをスムーズにすることが
できるものである。Further, according to the structure of the second means, by making the cross-sectional shape of the leading edge portion of the vane blade larger than the thickness of the vane blade, the direction of the suction flow changes depending on the use condition,
Even if the inlet angle of the front edge of the vane blade is different from the direction of separation, separation can be prevented, and even if the fluid flows from the suction surface side at a point close to the open state, the fluid flow can be made smooth by the thick wall. It is a thing.
【0013】また、第3の手段の構成により、静翼羽根
の前縁部の略円弧上の断面形状を厚肉の変わりに同一板
のリングにより作ることにより製作が容易になる。Further, according to the structure of the third means, the manufacturing is facilitated by forming the cross-sectional shape of the leading edge portion of the vane blade on the substantially arc by using the ring of the same plate instead of the thick wall.
【0014】[0014]
【実施例】以下、本発明の第1実施例について、図1お
よび図2を参照しながら説明する。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS A first embodiment of the present invention will be described below with reference to FIGS.
【0015】図に示すように、羽根車8の下流でケーシ
ング2の内壁および内筒6の間に円周方向に等間隔にて
静翼羽根1を複数枚備え、静翼羽根1は、前縁部3が静
翼羽根の厚さよりも大きく略円弧状の断面形状の樹脂製
の厚肉9を設けた構成となっている。As shown in the figure, a plurality of stationary vane blades 1 are provided at equal intervals in the circumferential direction between the inner wall of the casing 2 and the inner cylinder 6 downstream of the impeller 8, and the stationary vane blade 1 is The edge portion 3 has a configuration in which a resin thick wall 9 having a substantially arcuate cross-sectional shape that is larger than the thickness of the vane blade is provided.
【0016】上記構成により、静翼羽根1に流体が流入
されるとき、流入方向がいかなる場合でも厚肉9に沿っ
た流れとなり、前縁部3での剥離を防止し、剥離による
送風効率の低下を防止し、騒音の発生を低減できる。With the above structure, when the fluid is introduced into the vane blade 1, the flow is along the thick wall 9 regardless of the inflow direction, so that the separation at the front edge portion 3 is prevented and the ventilation efficiency due to the separation is improved. It is possible to prevent the decrease and reduce the generation of noise.
【0017】つぎに本発明の第2実施例について図3お
よび図4を参照しながら説明する。なお、第1実施例と
同一箇所には同一番号を付けて詳細な説明は省略する。Next, a second embodiment of the present invention will be described with reference to FIGS. 3 and 4. The same parts as those in the first embodiment are designated by the same reference numerals and detailed description thereof will be omitted.
【0018】図に示すように、第1実施例の構成の厚肉
9に加えて、正圧面側に略円弧状の断面形状の樹脂製の
厚肉10を設けた構成となっている。As shown in the drawing, in addition to the thick wall 9 of the first embodiment, a resin thick wall 10 having a substantially arc-shaped cross section is provided on the positive pressure surface side.
【0019】上記構成により、静翼羽根1に流体が流入
されるとき、流入方向がいかなる場合でも厚肉10に沿
った流れとなり、また開放状態に近い場合でも正圧面側
の前記厚肉10に沿った流れとなり、前縁部3での剥離
を防止し、剥離による送風効率の低下や騒音の発生が小
さくなる。With the above structure, when the fluid flows into the vane blade 1, the flow follows the thick wall 10 regardless of the inflow direction, and even when the fluid is close to the open state, it flows into the thick wall 10 on the pressure surface side. Along the flow, the separation at the front edge portion 3 is prevented, and the reduction of the ventilation efficiency and the generation of noise due to the separation are reduced.
【0020】なお、本実施例では、厚肉9および厚肉1
0は樹脂製のものを取り付けているが、ブレードと一体
成形も可能であるし、材質も多孔質材や鋼板を取り付け
ても良い。In this embodiment, the thick wall 9 and the thick wall 1 are provided.
Although 0 is made of resin, it may be integrally formed with the blade, and a porous material or a steel plate may be attached as the material.
【0021】つぎに本発明の第3実施例について図5お
よび図6を参照しながら説明する。なお、第1実施例と
同一箇所には同一番号を付けて詳細な説明は省略する。Next, a third embodiment of the present invention will be described with reference to FIGS. The same parts as those in the first embodiment are designated by the same reference numerals and detailed description thereof will be omitted.
【0022】図に示すように、第1実施例の構成の略円
弧状の断面形状の厚肉9および厚肉10に変えて、同一
位置に略円弧状の断面形状のリング11を設けた構成と
なっている。As shown in the drawing, in place of the thick wall 9 and the thick wall 10 having the substantially arc-shaped cross section of the structure of the first embodiment, a ring 11 having the substantially arc cross section is provided at the same position. Has become.
【0023】上記構成により、静翼羽根1に流体が流入
されるとき、流入方向がいかなる場合でも前記リング1
1に沿った流れとなり、前縁部3での剥離を防止し、剥
離による送風効率の低下や騒音の発生が小さくなる。With the above-mentioned structure, when the fluid flows into the vane blade 1, the ring 1 can be flowed in any direction.
The flow is in line with No. 1 and prevents peeling at the front edge portion 3, so that the reduction in blowing efficiency and the generation of noise due to peeling are reduced.
【0024】また、前記リング11は静翼羽根1と同一
材料のため容易に加工ができる。なお、本実施例では、
厚肉9および厚肉10およびリング11の形状を略円弧
状から多角形状の断面形状にしたり、凹凸面のあるもの
としても剥離を防止することができる。Since the ring 11 is made of the same material as the vane blade 1, it can be easily machined. In this example,
It is possible to prevent peeling even if the shapes of the thick wall 9, the thick wall 10, and the ring 11 are changed from a substantially arc shape to a polygonal cross-sectional shape, or if there is an uneven surface.
【0025】[0025]
【発明の効果】以上のように実施例から明らかなよう
に、本発明によれば静翼羽根の前縁部の厚肉及びリング
を設けたことにより、静翼羽根に流体が流入されると
き、流入方向がいかなる場合でも厚肉およびリングに沿
った流れとなり、前縁部での剥離を防止し、剥離による
送風効率の低下や騒音の発生が小さくなる。As described above, according to the present invention, when the fluid flows into the vane blade by providing the thick wall and the ring at the leading edge portion of the vane blade according to the present invention. In any case, the flow will be along the thick wall and along the ring, preventing separation at the front edge, and reducing the ventilation efficiency and noise due to separation.
【図1】本発明の第1実施例における斜流ファン用静翼
の構成を示す要部側面図FIG. 1 is a side view of an essential part showing the structure of a stationary blade for a mixed flow fan according to a first embodiment of the present invention.
【図2】同厚肉の詳細図[Fig. 2] Detailed view of the same thickness
【図3】同第2実施例における斜流ファン用静翼の構成
を示す要部側面図FIG. 3 is a side view of an essential part showing the structure of a vane for a mixed flow fan according to the second embodiment.
【図4】同厚肉の詳細図[Fig. 4] Detailed view of the same thickness
【図5】同第3実施例における斜流ファン用静翼の構成
を示す要部側面図FIG. 5 is a side view of a main portion showing the structure of a vane for a mixed flow fan according to the third embodiment.
【図6】同リングの詳細図FIG. 6 is a detailed view of the ring.
【図7】従来の斜流ファンの構成を示す正面図FIG. 7 is a front view showing the configuration of a conventional mixed flow fan.
【図8】同前縁部の詳細図FIG. 8 is a detailed view of the front edge portion.
1 静翼羽根 2 ケーシング 3 前縁部 4 負圧面 5 正圧面 6 内筒 7 通風口 8 羽根車 9 厚肉 10 厚肉 11 リング 1 Stator vane blade 2 Casing 3 Leading edge 4 Negative pressure surface 5 Positive pressure surface 6 Inner cylinder 7 Ventilation port 8 Impeller 9 Thick wall 10 Thick wall 11 Ring
Claims (3)
羽根車と、この羽根車の下流側に略円錐台形の内筒を設
け、前記ケーシングの内壁に前記内筒を支持する複数枚
の静翼羽根を備え、前記静翼羽根の前縁部の負圧面側に
断面形状が略円弧状の厚肉を持つ斜流ファン。1. An impeller having a plurality of blades in a casing, a substantially frustoconical inner cylinder provided on the downstream side of the impeller, and a plurality of inner cylinders supporting the inner cylinder on an inner wall of the casing. A mixed flow fan having a vane blade and having a thick wall with a substantially arc-shaped cross section on the suction surface side of the front edge of the vane blade.
の厚肉を持つ請求項1記載の斜流ファン。2. The mixed flow fan according to claim 1, wherein the leading edge portion of the stationary blade has a thick wall with a substantially arcuate cross-sectional shape.
一位置に略円弧状の断面形状を持つリングを設けた請求
項1記載または請求項2記載の斜流ファン。3. The mixed flow fan according to claim 1, wherein a ring having a substantially arc-shaped cross-sectional shape is provided at the same position, instead of the thick wall having the substantially arc-shaped cross-sectional shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9111893A JPH06299997A (en) | 1993-04-19 | 1993-04-19 | Mixed flow fan |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9111893A JPH06299997A (en) | 1993-04-19 | 1993-04-19 | Mixed flow fan |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH06299997A true JPH06299997A (en) | 1994-10-25 |
Family
ID=14017612
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9111893A Pending JPH06299997A (en) | 1993-04-19 | 1993-04-19 | Mixed flow fan |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH06299997A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112302995A (en) * | 2019-08-02 | 2021-02-02 | 珠海格力电器股份有限公司 | Fan assembly and cabinet air conditioner with same |
| CN116591993A (en) * | 2023-06-14 | 2023-08-15 | 武汉特种工业泵厂有限公司 | Guide vane, guide vane wheel and axial flow pump |
-
1993
- 1993-04-19 JP JP9111893A patent/JPH06299997A/en active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112302995A (en) * | 2019-08-02 | 2021-02-02 | 珠海格力电器股份有限公司 | Fan assembly and cabinet air conditioner with same |
| CN112302995B (en) * | 2019-08-02 | 2025-09-19 | 珠海格力电器股份有限公司 | Fan subassembly and have its cabinet air conditioner |
| CN116591993A (en) * | 2023-06-14 | 2023-08-15 | 武汉特种工业泵厂有限公司 | Guide vane, guide vane wheel and axial flow pump |
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