JPS623998U - - Google Patents
Info
- Publication number
- JPS623998U JPS623998U JP9453185U JP9453185U JPS623998U JP S623998 U JPS623998 U JP S623998U JP 9453185 U JP9453185 U JP 9453185U JP 9453185 U JP9453185 U JP 9453185U JP S623998 U JPS623998 U JP S623998U
- Authority
- JP
- Japan
- Prior art keywords
- hub
- rotor blade
- fan
- slit
- axial flow
- 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
- 238000005192 partition Methods 0.000 claims 1
- 238000010586 diagram Methods 0.000 description 4
- 230000000052 comparative effect Effects 0.000 description 2
- 230000003068 static effect Effects 0.000 description 1
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
第1図は、本考案の実施例にかかる軸流送風機
の概略的な断面図、第2図は、第1図の軸流送風
機における動翼面の平面図、第3図は、第1図の
軸流送風機における動翼の代表径での断面図、第
4図、第5図、第6図、第8図および第10図は
、軸流送風機におけくh―ΔQ、θ―ΔQ、l―
ΔQ、G―ΔQおよびm―ΔQ特性図、第7図、
第9図および第11図の各イ,ロは、l―ΔQ、
G―ΔQおよびm―ΔQ特性図において適切寸法
範囲外での空気流の状態を示す説明図、第12図
および第13図は、比較例と本実施例における流
量―静圧(Q―PS)、流量―運転音(Q―LA
)特性図、第14図は、従来公知(比較例)の軸
流送風機の概略的な断面図、第15図は、第14
図図示の軸流送風機における動翼の代表径での断
面図である。
1……フアン、2……フアンガイド、4……ハ
ブ、5……動翼、5a……ハブ側、5b……チツ
プ側、5c……圧力面、5d……負圧面、7……
スリツト。
FIG. 1 is a schematic cross-sectional view of an axial blower according to an embodiment of the present invention, FIG. 2 is a plan view of the rotor blade surface of the axial blower shown in FIG. 1, and FIG. 4, 5, 6, 8, and 10 are cross-sectional views at representative diameters of rotor blades in axial flow blowers, h-ΔQ, θ-ΔQ, l-
ΔQ, G-ΔQ and m-ΔQ characteristics diagram, Fig. 7,
Each of A and B in FIGS. 9 and 11 is l−ΔQ,
Explanatory diagrams showing the state of air flow outside the appropriate size range in the G-ΔQ and m-ΔQ characteristic diagrams, Figures 12 and 13 are flow rate vs. static pressure (Q-PS) in the comparative example and this example. , Flow rate-operating sound (Q-LA
) Characteristic diagram, FIG. 14 is a schematic cross-sectional view of a conventionally known (comparative example) axial flow blower, and FIG.
FIG. 2 is a cross-sectional view of the rotor blade at a representative diameter in the illustrated axial blower. 1... Fan, 2... Fan guide, 4... Hub, 5... Moving blade, 5a... Hub side, 5b... Chip side, 5c... Pressure surface, 5d... Negative pressure surface, 7...
Slits.
Claims (1)
てなるフアン1と、該フアン1の外周部に流入領
域と流出領域とを仕切るべく設けられたフアンガ
イド2とを有し、前記各動翼5のハブ側5aから
チツプ側5bにかけて、圧力面5cから負圧面5
dに空気が通過し得るようにスリツト7を形成し
てなる軸流送風機において、前記動翼5における
ハブ4外周面からチツプ側5bまでの径方向の長
さH、前記ハブ4外周面から径方向にとつた前記
スリツト7の長さをh、前記動翼5の平均流量半
径における反り角をθとするとき、 0.5H≦h≦0.9H 30°≦θ≦70° となるように設定したことを特徴とする軸流送風
機。[Claims for Utility Model Registration] A fan 1 comprising a plurality of rotor blades 5, 5... formed on the outer periphery of a hub 4, and a fan 1 provided on the outer periphery of the fan 1 to partition an inflow region and an outflow region. from the hub side 5a to the tip side 5b of each rotor blade 5, from the pressure surface 5c to the negative pressure surface 5.
In the axial flow blower in which a slit 7 is formed to allow air to pass through the rotor blade 5, the radial length H from the outer circumferential surface of the hub 4 to the tip side 5b of the rotor blade 5, the radial length H from the outer circumferential surface of the hub 4 When the length of the slit 7 in the direction is h, and the warp angle at the average flow radius of the rotor blade 5 is θ, then 0.5H≦h≦0.9H 30°≦θ≦70°. An axial flow blower characterized by the following settings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9453185U JPS623998U (en) | 1985-06-21 | 1985-06-21 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP9453185U JPS623998U (en) | 1985-06-21 | 1985-06-21 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS623998U true JPS623998U (en) | 1987-01-10 |
Family
ID=30653115
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP9453185U Pending JPS623998U (en) | 1985-06-21 | 1985-06-21 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS623998U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100437019B1 (en) * | 2001-09-03 | 2004-06-23 | 엘지전자 주식회사 | A high thrust axial fan |
| JP2007529662A (en) * | 2004-03-18 | 2007-10-25 | ロトリオンテ,フランク,ダニエル | Turbine and rotor therefor |
-
1985
- 1985-06-21 JP JP9453185U patent/JPS623998U/ja active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR100437019B1 (en) * | 2001-09-03 | 2004-06-23 | 엘지전자 주식회사 | A high thrust axial fan |
| JP2007529662A (en) * | 2004-03-18 | 2007-10-25 | ロトリオンテ,フランク,ダニエル | Turbine and rotor therefor |
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