JPH09242694A - Cylindrical impeller - Google Patents
Cylindrical impellerInfo
- Publication number
- JPH09242694A JPH09242694A JP8047057A JP4705796A JPH09242694A JP H09242694 A JPH09242694 A JP H09242694A JP 8047057 A JP8047057 A JP 8047057A JP 4705796 A JP4705796 A JP 4705796A JP H09242694 A JPH09242694 A JP H09242694A
- Authority
- JP
- Japan
- Prior art keywords
- blade
- tip
- blades
- impeller
- root
- 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.)
- Granted
Links
- 239000003381 stabilizer Substances 0.000 abstract description 13
- 230000002093 peripheral effect Effects 0.000 abstract description 9
- 238000005422 blasting Methods 0.000 abstract 3
- 230000003292 diminished effect Effects 0.000 abstract 2
- 238000007664 blowing Methods 0.000 description 13
- 229920003002 synthetic resin Polymers 0.000 description 2
- 239000000057 synthetic resin Substances 0.000 description 2
- 238000009423 ventilation Methods 0.000 description 2
- 238000003466 welding Methods 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
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/02—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
- F04D17/04—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal of transverse-flow type
-
- 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
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/281—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
- F04D29/282—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers the leading edge of each vane being substantially parallel to the rotation axis
- F04D29/283—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers the leading edge of each vane being substantially parallel to the rotation axis rotors of the squirrel-cage type
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Air-Conditioning Room Units, And Self-Contained Units In General (AREA)
Abstract
Description
【0001】[0001]
【発明の属する技術分野】この発明は、空気調和機等に
使用されるクロスフローファン等の送風用の筒状羽根車
に関するものである。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a cylindrical impeller for blowing air such as a cross flow fan used in an air conditioner or the like.
【0002】[0002]
【従来の技術】従来、前記のような筒状羽根車として、
支持板の一端面に軸方向に沿ってまっすぐに延出する多
数の羽根を周方向に所定間隔で形成したエレメントを所
定数連結したものが知られている。この筒状羽根車を以
下、図面に基づき説明する。図6において、1は合成樹
脂の一体成形品からなるエレメントであり、環状または
円板状の支持板2の一端面に、軸方向に延出する多数の
羽根3を周方向に所定間隔を設けて一体に成形したもの
である。前記、各羽根3は、エレメント1の半径方向に
対して傾斜し、近似円弧状に湾曲した翼状の横断面形状
に形成してある。また、羽根3が延出していない支持板
2の反対側の端面には、別のエレメントをまっすぐにね
じれないように連結するために、その羽根の先端部を嵌
合固定する嵌合溝4が形成されている。2. Description of the Related Art Conventionally, as a cylindrical impeller as described above,
It is known that a predetermined number of elements, each of which has a large number of blades extending straight along the axial direction and formed at predetermined intervals in the circumferential direction, are connected to one end surface of a support plate. This cylindrical impeller will be described below with reference to the drawings. In FIG. 6, reference numeral 1 denotes an element made of a synthetic resin integrally molded product, and a large number of axially extending blades 3 are provided at predetermined intervals in the circumferential direction on one end surface of an annular or disc-shaped support plate 2. It is integrally molded. Each of the blades 3 is formed in a wing-like cross-sectional shape that is inclined with respect to the radial direction of the element 1 and is curved in an approximate arc shape. Further, on the opposite end surface of the support plate 2 where the blades 3 do not extend, there is provided a fitting groove 4 for fitting and fixing the tips of the blades in order to connect another element so as not to be twisted straight. Has been formed.
【0003】図7に示すように、前段のエレメント1の
羽根3の先端部を次段のエレメント1の支持板2上に嵌
合し保持させて接着または超音波溶着によって固定し、
前記操作を繰り返して所定個数のエレメント1を軸方向
にねじれないように連結し、先端のエレメント1に羽根
3を嵌合、支持する端板2aを設けることにより、筒状
羽根車5を構成している。As shown in FIG. 7, the tips of the blades 3 of the preceding element 1 are fitted and held on the support plate 2 of the following element 1 and fixed by adhesion or ultrasonic welding.
The tubular impeller 5 is configured by repeating the above operation to connect a predetermined number of elements 1 so as not to be twisted in the axial direction, and providing an end plate 2a for fitting and supporting the blade 3 on the tip element 1 ing.
【0004】また、図8は、従来の筒状羽根車の要部を
羽根先端部11から軸方向に沿って羽根3の根元部12
を見た拡大図である。羽根3は、筒状羽根車5の中心か
ら半径R1の位置に半径方向に対する取り付け傾斜角度
θ1で根元部12を配置してある。羽根3の先端部11
は、軸方向にまっすぐに延出し、抜き勾配分だけ根元部
12より小さい。Further, FIG. 8 shows an essential part of a conventional cylindrical impeller from the blade tip 11 to the root 12 of the blade 3 along the axial direction.
It is the enlarged view which looked at. The blade 3 has a root portion 12 arranged at a radius R1 from the center of the tubular impeller 5 at a mounting inclination angle θ1 with respect to the radial direction. Tip 11 of blade 3
Extends straight in the axial direction and is smaller than the root portion 12 by the draft.
【0005】そして、図9に示すように、空気調和機の
送風装置として前段の筒状羽根車5をケーシングを形成
するスタビライザ6とリアガイダ7の間に配置する。筒
状羽根車が、矢印8の時計方向に回転することにより、
矢印9の方向から空気が流入し、矢印10の方向に空気
が流出するようにしている。Then, as shown in FIG. 9, a cylindrical impeller 5 at the front stage is arranged as a blower for an air conditioner between a stabilizer 6 and a rear guider 7 which form a casing. By rotating the cylindrical impeller in the clockwise direction of arrow 8,
Air flows in from the direction of arrow 9 and flows out in the direction of arrow 10.
【0006】[0006]
【発明が解決しようとする課題】前記のエレメント1を
配置して筒状羽根車5を構成した場合には、エレメント
1の羽根3の枚数zと1分間当たりの回転数nからなる
(n×z)/60Hzの周波数の音とその整数倍の周波
数の音が発生するという問題があった。この音は、羽根
ピッチ音やnz音と呼ばれており、聴覚的に笛を吹くよ
うな耳ざわりな音である。When the element 1 is arranged to form the cylindrical impeller 5, the number of the blades 3 of the element 1 is z and the number of revolutions per minute is n (n ×). There is a problem that a sound having a frequency of z) / 60 Hz and a sound having a frequency that is an integral multiple thereof are generated. This sound is called a blade pitch sound or an nz sound, and is a sound that feels like hearing a whistle.
【0007】以下、この耳ざわりな音をnz音と呼ぶこ
とにする。このnz音は、エレメン1の羽根3、羽根3
の取り付けピッチ、スタビライザ6、リアガイダ7の形
状とそれらの位置関係により変化する。たとえば、送風
効率を上げるために筒状羽根車5とスタビライザ6の間
隔dを狭くすると、nz音が大きくなる。このように、
送風効率を上げようとすると、nz音も大きくなってし
まい、送風効率を極限まで上げられないという問題があ
った。Hereinafter, this harsh sound will be referred to as an nz sound. This nz sound is generated by the blades 3 and 3 of the element 1.
The mounting pitch, the shape of the stabilizer 6 and the rear guider 7 and their positional relationship change. For example, if the distance d between the cylindrical impeller 5 and the stabilizer 6 is narrowed in order to improve the blowing efficiency, the nz sound becomes large. in this way,
When trying to increase the air blowing efficiency, there is a problem that the nz sound also becomes loud and the air blowing efficiency cannot be raised to the limit.
【0008】また、筒状羽根車のエレメント1は、一般
に合成樹脂の成形品であるが、金型から成形品であるエ
レメント1を取り出すために、羽根3には抜き勾配が必
要となる。これにより、羽根3の根元部12の断面形状
に対して先端部11の断面形状が小さくなってしまい、
送風効率が羽根3の根元部12と先端部11とで異な
り、送風効率を極限まで上げられないという問題があっ
た。Further, the element 1 of the tubular impeller is generally a synthetic resin molded product, but the blade 3 needs a draft to remove the molded element 1 from the mold. As a result, the cross-sectional shape of the tip portion 11 becomes smaller than the cross-sectional shape of the root portion 12 of the blade 3,
There is a problem that the air blowing efficiency differs between the root portion 12 and the tip portion 11 of the blade 3, and the air blowing efficiency cannot be raised to the limit.
【0009】この発明は、前述のような問題を解決する
もので、羽根3の根元部12と羽根先端部11での送風
効率の差を少なくして、送風効率を向上させると共に、
nz音のない筒状羽根車を提供することを目的とする。The present invention solves the above-mentioned problems, reduces the difference in the air blowing efficiency between the root portion 12 and the blade tip portion 11 of the blade 3, and improves the air blowing efficiency.
An object is to provide a cylindrical impeller without nz sound.
【0010】[0010]
【課題を解決するための手段】請求項1の発明は、環状
または円板状の支持板の端面に、軸方向に沿って延出す
る多数の羽根を周方向に所定間隔で形成した筒状羽根車
において、前記羽根の筒状羽根車半径方向に対する取り
付け角度を、羽根の根元部から先端部にかけて徐々に変
化させたものである。According to a first aspect of the present invention, a plurality of blades extending in the axial direction are formed on an end surface of an annular or disc-shaped support plate at a predetermined interval in the circumferential direction. In the impeller, the mounting angle of the blade with respect to the radial direction of the cylindrical impeller is gradually changed from the root to the tip of the blade.
【0011】請求項2の発明は、前記環状または円板状
の支持板の端面に、軸方向に沿って延出する多数の羽根
を周方向に所定間隔で形成した筒状羽根車において、前
記羽根の筒状羽根車中心からの取り付け位置を、羽根の
根元部から先端部にかけて徐々に変化させたものであ
る。According to a second aspect of the present invention, there is provided a tubular impeller in which a large number of blades extending in the axial direction are formed at predetermined intervals in a circumferential direction on an end surface of the annular or disc-shaped support plate. The mounting position of the blade from the center of the tubular impeller is gradually changed from the root to the tip of the blade.
【0012】[0012]
【発明の実施の形態】以下、この発明の実施形態を図に
基づいて説明する。図1は、この発明の第1実施形態に
係る筒状羽根車のエレメント1の斜視図であり、図2
は、図1に示したエレメント1を複数個軸方向に連結し
て先端部に端板2aを設けた筒状羽根車5である。この
筒状羽根車5は、各エレメント1に設けた各羽根3以外
は、図6,図7に示した従来のものと同様である。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS An embodiment of the present invention will be described below with reference to the drawings. 1 is a perspective view of an element 1 of a tubular impeller according to a first embodiment of the present invention.
Is a tubular impeller 5 in which a plurality of elements 1 shown in FIG. 1 are axially connected to each other and an end plate 2a is provided at a tip portion thereof. This tubular impeller 5 is the same as the conventional one shown in FIGS. 6 and 7, except for each blade 3 provided in each element 1.
【0013】図3は、第1実施形態に係る筒状羽根車の
羽根3の先端部11側から軸方向に沿って羽根3の根元
部12を見た拡大図である。図3に示すように、第1実
施形態の羽根3は、筒状羽根車の中心Oから半径R1の
位置に、半径方向に対する取り付け傾斜角度θ1で羽根
3の根元部12を配置してあり、羽根3の先端部11
は、筒状羽根車の中心Oから同じ半径R1の位置に、半
径方向に対する取り付け傾斜角度θ2で軸方向に所定距
離だけ羽根3の根元部12から延出した位置に配置して
ある。これらの配置によって、羽根3の筒状羽根車半径
方向に対する取り付け傾斜角度を、根元から先端にかけ
て徐々に変化させ、羽根3の前縁に後倒れになる外周側
稜線13を構成してある。FIG. 3 is an enlarged view of the root portion 12 of the blade 3 along the axial direction from the tip 11 side of the blade 3 of the tubular impeller according to the first embodiment. As shown in FIG. 3, in the blade 3 of the first embodiment, the root portion 12 of the blade 3 is arranged at a position of a radius R1 from the center O of the tubular impeller at an attachment inclination angle θ1 with respect to the radial direction, Tip 11 of blade 3
Are arranged at the same radius R1 from the center O of the tubular impeller and at a position extending from the root 12 of the blade 3 by a predetermined distance in the axial direction at a mounting inclination angle θ2 with respect to the radial direction. With these arrangements, the mounting inclination angle of the blade 3 with respect to the radial direction of the cylindrical impeller is gradually changed from the root to the tip, and the outer peripheral ridgeline 13 is formed at the front edge of the blade 3 to be tilted rearward.
【0014】なお、図3では1枚の羽根3を示して説明
したが、筒状羽根車の各羽根のすべてを、前述した羽根
と同様に半径方向に対する傾斜角度を根元から先端にか
けて徐々に変化させてある。Although the single blade 3 is shown in FIG. 3, all the blades of the tubular impeller are gradually changed in inclination angle with respect to the radial direction from the root to the tip in the same manner as the above-mentioned blades. I am allowed.
【0015】前記のような羽根3の構成にすることによ
り、抜き勾配によって生じる羽根3の根元部12と先端
部11の断面形状の差による送風効率の差を少なくでき
る。また、羽根3の外周側稜線13とケーシングを構成
しているスタビライザ6との間隔d1,d2は、羽根3
の根元部12の位置でd1=R0−R1であり、先端部
11でd2=R0−R1であるからd1とd2は共に同
じ間隔である。しかし、羽根3が矢印8に示す時計方向
に回転することにより、羽根3の外周側稜線13は、ケ
ーシングを構成しているスタビライザ6に対して、間隔
を一定に保ったまま、一直線上ではなく徐々に変化する
位置関係を構成する。このため、羽根3への風の流入9
と流出10がなめらかに変化する。これにより、nz音
をなくすことができる。By configuring the blade 3 as described above, it is possible to reduce the difference in blowing efficiency due to the difference in cross-sectional shape between the root portion 12 and the tip portion 11 of the blade 3 caused by the draft. Further, the distances d1 and d2 between the ridgeline 13 on the outer peripheral side of the blade 3 and the stabilizer 6 forming the casing are equal to each other.
Since d1 = R0-R1 at the position of the root portion 12 and d2 = R0-R1 at the tip portion 11, both d1 and d2 have the same interval. However, when the blade 3 rotates in the clockwise direction shown by the arrow 8, the outer peripheral ridgeline 13 of the blade 3 is not aligned with the stabilizer 6 forming the casing while keeping a constant interval. Construct a positional relationship that changes gradually. Therefore, the inflow 9 of the wind to the blades 3
And the outflow 10 changes smoothly. As a result, the nz sound can be eliminated.
【0016】図4は、第2実施形態に係る筒状羽根車の
羽根3の先端部11側から軸方向に沿って羽根3の根元
部12を見た拡大図である。図4に示すように、第2実
施形態の羽根3は、筒状羽根車の中心Oから半径R1の
位置に、半径方向に対する取り付け傾斜角度θ1で羽根
3の根元部12を配置してあり、羽根3の先端部11
は、筒状羽根車の中心Oから異なる半径R2の位置に、
半径方向に対する異なる取り付け傾斜角度θ3で軸方向
に所定距離だけ根元部12から延出した位置に配置して
ある。これらの配置によって、羽根3の筒状羽根車中心
Oからの取り付け位置を、根元から先端にかけて徐々に
変化させ、羽根3を外倒れに構成してある。FIG. 4 is an enlarged view of the root portion 12 of the blade 3 along the axial direction from the tip 11 side of the blade 3 of the tubular impeller according to the second embodiment. As shown in FIG. 4, in the blade 3 of the second embodiment, the root portion 12 of the blade 3 is arranged at a position of a radius R1 from the center O of the tubular impeller at a mounting inclination angle θ1 with respect to the radial direction, Tip 11 of blade 3
At a position with a radius R2 different from the center O of the cylindrical impeller,
It is arranged at a position extending from the root portion 12 by a predetermined distance in the axial direction at different mounting inclination angles θ3 with respect to the radial direction. With these arrangements, the mounting position of the blade 3 from the cylindrical impeller center O is gradually changed from the root to the tip, so that the blade 3 is tilted outward.
【0017】なお、図4では、1枚の羽根3のみを示し
て説明したが、筒状羽根車の各羽根のすべてを、前述し
た羽根と同様に、取り付け位置を根元から先端にかけて
徐々に変化させてあり、また、羽根以外の構成は前述し
た図6,図7に示した従来のものと同様である。Although only one blade 3 is shown and described in FIG. 4, all the blades of the tubular impeller are gradually changed in mounting position from the root to the tip like the above-mentioned blades. The configuration other than the blades is the same as the conventional one shown in FIGS. 6 and 7.
【0018】前記のような羽根3の構成にすることによ
り、抜き勾配によって生じる羽根3の根元部12と先端
部11の断面形状の差による送風効率の差を少なくでき
る。また、羽根3の外周側稜線13とケーシングを構成
しているスタビライザ6との間隔d1,d2は、羽根3
の根元部12の位置でd1=R0−R1であり、羽根3
の先端部11でd2=R0−R2である。そして、羽根
3の外周側稜線13は、ケーシングを構成しているスタ
ビライザ6との位置関係では一直線上に並ぶが、羽根3
の根元部12から先端部11にかけて間隔が徐々に変化
する位置関係を構成するため、羽根3が矢印8に示す時
計方向に回転することにより、羽根3への風の流入9と
流出10がなめらかに変化する。これにより、nz音を
なくすことができる。By configuring the blades 3 as described above, it is possible to reduce the difference in blowing efficiency due to the difference in cross-sectional shape between the root portion 12 and the tip portion 11 of the blades 3 caused by the draft. Further, the distances d1 and d2 between the ridgeline 13 on the outer peripheral side of the blade 3 and the stabilizer 6 forming the casing are equal to each other.
D1 = R0-R1 at the position of the root portion 12 of the blade 3
D2 = R0-R2 at the tip 11 of the. The outer peripheral ridgelines 13 of the blades 3 are aligned on a straight line in the positional relationship with the stabilizer 6 forming the casing.
Since the interval is gradually changed from the root 12 to the tip 11 of the blade, the blade 3 rotates clockwise in the direction indicated by the arrow 8 so that the inflow 9 and the outflow 10 of the wind to the blade 3 are smooth. Changes to. As a result, the nz sound can be eliminated.
【0019】図5は、第3実施形態に係る筒状羽根車の
羽根3の先端部11側から軸方向に沿って羽根3の根元
部12を見た拡大図である。図5に示すように、第3実
施形態の羽根3は、筒状羽根車の中心Oから半径R1の
位置に、半径方向に対する取り付け傾斜角度θ1で羽根
3の根元部12を配置してあり、羽根3の先端部11
は、筒状羽根車の中心Oから異なる半径R2の位置に、
半径方向に対する異なる取り付け傾斜角度θ4で軸方向
に所定距離だけ根元部12から延出した位置に配置して
ある。これらの配置によって、羽根3の筒状羽根車半径
方向に対する取り付け傾斜角度と、筒状羽根車の中心O
からの取り付け位置とを根元部から先端部にかけて徐々
に変化させ、羽根3の前縁に後倒れになる外周側稜線1
3を構成すると共に、羽根3を外倒れに構成してある。
なお、第3実施形態の羽根の構成は、図3,図4に示し
た第1,第2実施形態の羽根の構成を、併せて具備させ
た構成である。FIG. 5 is an enlarged view of the root portion 12 of the blade 3 along the axial direction from the tip 11 side of the blade 3 of the tubular impeller according to the third embodiment. As shown in FIG. 5, in the blade 3 of the third embodiment, the root portion 12 of the blade 3 is arranged at a position of a radius R1 from the center O of the tubular impeller, at a mounting inclination angle θ1 with respect to the radial direction, Tip 11 of blade 3
At a position with a radius R2 different from the center O of the cylindrical impeller,
It is arranged at a position extending from the root portion 12 by a predetermined distance in the axial direction at different mounting inclination angles θ4 with respect to the radial direction. By these arrangements, the mounting inclination angle of the blade 3 with respect to the radial direction of the tubular impeller and the center O of the tubular impeller are set.
From the root portion to the tip portion, and the outer edge line 1 is inclined rearward to the front edge of the blade 3.
3 and the blade 3 is tilted outward.
The configuration of the blade of the third embodiment is a configuration including the configuration of the blade of the first and second embodiments shown in FIGS. 3 and 4 together.
【0020】なお、図5では1枚の羽根3のみを示して
説明したが、筒状羽根車のすべての羽根を、同様に取り
付け傾斜角度と取り付け位置とを根元部から先端部にか
けて徐々に変化させてあり、また、羽根以外の構成は前
述した図6,図7に示した従来のものと同様である。Although only one blade 3 is shown in FIG. 5, all the blades of the cylindrical impeller are similarly changed in inclination angle and attachment position from the root to the tip. The configuration other than the blades is the same as the conventional one shown in FIGS. 6 and 7.
【0021】前記のような羽根3の構成にすることによ
り、抜き勾配によって生じる羽根3の根元部12と先端
部11との断面形状の差による送風効率の差を少なくで
きる。また、羽根3の外周側稜線13とケーシングを構
成しているスタビライザ6との間隔は、根元部12の位
置でd1=R0−R1であり、羽根3の先端部11でd
2=R0−R1である。しかし、羽根3の外周側稜線1
3は、ケーシングを構成しているスタビライザ6との位
置関係が一直線上になく、羽根3が矢印8に示す時計方
向に回転することにより間隔が徐々に変化する位置関係
を構成するため、羽根3への風の流入9と流出10がな
めらかに変化する。これにより、nz音をなくすことが
できる。By configuring the blade 3 as described above, it is possible to reduce the difference in blowing efficiency due to the difference in cross-sectional shape between the root portion 12 and the tip portion 11 of the blade 3 caused by the draft. Further, the distance between the outer peripheral ridgeline 13 of the blade 3 and the stabilizer 6 forming the casing is d1 = R0-R1 at the position of the root portion 12, and d at the tip portion 11 of the blade 3.
2 = R0-R1. However, the outer ridge line 1 of the blade 3
3 does not have a positional relationship with the stabilizer 6 that constitutes the casing in a straight line, and the blade 3 rotates in the clockwise direction shown by an arrow 8 to form a positional relationship in which the interval gradually changes. The inflow 9 and the outflow 10 of the wind change smoothly. As a result, the nz sound can be eliminated.
【0022】この発明において、前記各実施形態のもの
は複数のエレメントを軸方向に連結して筒状羽根車を構
成したが、1個のエレメントの羽根の先端部に端板を装
着して筒状羽根車を構成してもよい。In the present invention, in each of the above-described embodiments, a plurality of elements are connected in the axial direction to form a cylindrical impeller, but an end plate is attached to the tip of the blade of one element to form a cylindrical impeller. You may comprise an impeller.
【0023】[0023]
【発明の効果】以上説明したように、請求項1の発明に
係る筒状羽根車は、支持板の端面から軸方向に沿って延
出する多数の羽根を有し、これらの羽根の筒状羽根車の
半径方向に対する取り付け傾斜角度を、根元部から先端
部にかけて徐々に変化させてあるので、抜き勾配によっ
て生じる羽根の根元部と羽根の先端部との断面形状の差
による送風効率の差を少なくして、送風効率を向上させ
ることができる。また、羽根の外周側稜線は、ケーシン
グを構成しているスタビライザに対して、間隔を一定に
保ったまま、一直線上ではなく徐々に変化する位置関係
を構成するため、羽根への空気の流入と流出がなめらか
に変化する。これにより、耳ざわりなnz音をなくする
ことができる。As described above, the cylindrical impeller according to the invention of claim 1 has a large number of blades extending in the axial direction from the end surface of the support plate, and the cylindrical shape of these blades. Since the mounting inclination angle of the impeller with respect to the radial direction is gradually changed from the root part to the tip part, the difference in blowing efficiency due to the difference in cross-sectional shape between the root part of the blade and the tip part of the blade caused by the draft By reducing the amount, the blowing efficiency can be improved. Further, since the outer peripheral ridge of the blade forms a positional relationship with the stabilizer that constitutes the casing while maintaining a constant distance, it does not form a straight line but a gradually changing positional relationship. The outflow changes smoothly. As a result, it is possible to eliminate the unpleasant nz sound.
【0024】また、請求項2の発明に係る筒状羽根車
は、支持板の端面から軸方向に沿って延出する多数の羽
根を有し、これらの羽根の筒状羽根車の中心からの取り
付け位置を羽根の根元部から先端部にかけて徐々に変化
させてあるので、抜き勾配によって生じる羽根の根元部
と羽根の先端部の断面形状の差による送風効率の差を少
なくして、送風効率上を向上させることができる。ま
た、羽根の外周側稜線は、ケーシングを構成しているス
タビライザとの位置関係が一直線上に並ぶが、間隔が徐
々に変化する位置関係を構成するため、羽根への風の流
入と流出がなめらかに変化する。これにより、耳ざわり
なnz音をなくすことができる。The cylindrical impeller according to the invention of claim 2 has a large number of blades extending in the axial direction from the end surface of the support plate, and these blades are arranged from the center of the cylindrical impeller. Since the mounting position is gradually changed from the root to the tip of the blade, the difference in the ventilation efficiency due to the difference in the cross-sectional shape of the blade root and the blade tip caused by the draft is reduced, and the ventilation efficiency is improved. Can be improved. In addition, the outer peripheral ridges of the blades are aligned in a straight line with the stabilizers that form the casing, but since the gaps form a positional relationship that gradually changes, the flow of air into and out of the blades is smooth. Changes to. This makes it possible to eliminate the nz sound that is unpleasant to the ear.
【図1】この発明の第1実施形態に係る筒状羽根車のエ
レメントを示した斜視図。FIG. 1 is a perspective view showing an element of a tubular impeller according to a first embodiment of the present invention.
【図2】この発明の第1実施形態に係る筒状羽根車を示
した一部切り欠き斜視図。FIG. 2 is a partially cutaway perspective view showing a tubular impeller according to the first embodiment of the present invention.
【図3】図2に示した筒状羽根車の羽根の先端部から軸
方向に沿って羽根の根元部を見た拡大図。FIG. 3 is an enlarged view of the blade root of the tubular impeller shown in FIG. 2 as viewed from the tip of the blade along the axial direction.
【図4】この発明の第2実施形態に係る筒状羽根車の羽
根の先端部から軸方向に沿って羽根の根元部を見た拡大
図。FIG. 4 is an enlarged view of the blade root of the tubular impeller according to the second embodiment of the present invention, as viewed from the tip of the blade along the axial direction.
【図5】この発明の第3実施形態に係る筒状羽根車の羽
根の先端部から軸方向に沿って羽根の根元部を見た拡大
図。FIG. 5 is an enlarged view of the blade root of the tubular impeller according to the third embodiment of the present invention, as viewed from the tip of the blade along the axial direction.
【図6】従来の筒状羽根車のエレメントを示した斜視
図。FIG. 6 is a perspective view showing an element of a conventional tubular impeller.
【図7】図6に示したエレメントを連結した従来の筒状
羽根車の一部切り欠き斜視図。7 is a partially cutaway perspective view of a conventional tubular impeller in which the elements shown in FIG. 6 are connected.
【図8】図7に示した筒状羽根車の羽根の先端部から軸
方向に沿って羽根の根元部を見た拡大図。FIG. 8 is an enlarged view of the blade root of the tubular impeller shown in FIG. 7 as viewed from the tip of the blade along the axial direction.
【図9】空気調和機における筒状羽根車とケーシングと
の位置関係を示す断面説明図。FIG. 9 is an explanatory cross-sectional view showing the positional relationship between the cylindrical impeller and the casing in the air conditioner.
1 エレメント 2 支持板 3 羽根 4 嵌合溝 5 筒状羽根車 6 スタビライザ 7 リアガイダ 8 筒状羽根車の回転方向 9 流入方向 10 流出方向 11 羽根の先端部 12 羽根の根元部 13 羽根の外周側稜線 DESCRIPTION OF SYMBOLS 1 Element 2 Support plate 3 Blade 4 Fitting groove 5 Cylindrical impeller 6 Stabilizer 7 Rear guider 8 Rotating direction of cylindrical impeller 9 Inflow direction 10 Outflow direction 11 Blade tip 12 Blade root 13 Blade outer edge line
Claims (2)
方向に沿って延出する多数の羽根を周方向に所定間隔で
形成した筒状羽根車において、前記羽根の筒状羽根車半
径方向に対する取り付け角度を、羽根の根元部から先端
部にかけて徐々に変化させたことを特徴とする筒状羽根
車。1. A cylindrical impeller in which a large number of blades extending in the axial direction are formed at predetermined intervals in the circumferential direction on an end surface of an annular or disc-shaped support plate, and the cylindrical impeller of the blades. A cylindrical impeller characterized in that the mounting angle with respect to the radial direction is gradually changed from the root part to the tip part of the blade.
に、軸方向に沿って延出する多数の羽根を周方向に所定
間隔で形成した筒状羽根車において、前記羽根の筒状羽
根車中心からの取り付け位置を、羽根の根元部から先端
部にかけて徐々に変化させたことを特徴とする筒状羽根
車。2. A tubular impeller in which a large number of blades extending in the axial direction are formed at predetermined intervals in the circumferential direction on an end surface of the annular or disc-shaped support plate. A cylindrical impeller characterized in that the mounting position from the car center is gradually changed from the root to the tip of the blade.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP04705796A JP3850061B2 (en) | 1996-03-05 | 1996-03-05 | Cylindrical impeller |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP04705796A JP3850061B2 (en) | 1996-03-05 | 1996-03-05 | Cylindrical impeller |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH09242694A true JPH09242694A (en) | 1997-09-16 |
| JP3850061B2 JP3850061B2 (en) | 2006-11-29 |
Family
ID=12764537
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP04705796A Expired - Fee Related JP3850061B2 (en) | 1996-03-05 | 1996-03-05 | Cylindrical impeller |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP3850061B2 (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010106854A (en) * | 2010-02-16 | 2010-05-13 | Sharp Corp | Cross-flow fan, blower, and impeller forming machine |
| JP2010106853A (en) * | 2010-02-16 | 2010-05-13 | Sharp Corp | Cross-flow fan, blower, and impeller forming machine |
| JP2010209849A (en) * | 2009-03-11 | 2010-09-24 | Sharp Corp | Cross-flow fan and method of manufacturing the cross-flow fan |
| WO2015046110A1 (en) * | 2013-09-30 | 2015-04-02 | 日清紡メカトロニクス株式会社 | Bladed wheel for fan |
| JP2017214937A (en) * | 2017-09-19 | 2017-12-07 | 日清紡メカトロニクス株式会社 | Cross-flow fan |
| CN112412832A (en) * | 2020-10-28 | 2021-02-26 | 青岛海尔空调器有限总公司 | Cross-flow fans and air conditioners |
| WO2025014026A1 (en) * | 2023-07-11 | 2025-01-16 | 한온시스템 주식회사 | Vehicle blower unit |
-
1996
- 1996-03-05 JP JP04705796A patent/JP3850061B2/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2010209849A (en) * | 2009-03-11 | 2010-09-24 | Sharp Corp | Cross-flow fan and method of manufacturing the cross-flow fan |
| JP2010106854A (en) * | 2010-02-16 | 2010-05-13 | Sharp Corp | Cross-flow fan, blower, and impeller forming machine |
| JP2010106853A (en) * | 2010-02-16 | 2010-05-13 | Sharp Corp | Cross-flow fan, blower, and impeller forming machine |
| WO2015046110A1 (en) * | 2013-09-30 | 2015-04-02 | 日清紡メカトロニクス株式会社 | Bladed wheel for fan |
| JP2015068269A (en) * | 2013-09-30 | 2015-04-13 | 日清紡メカトロニクス株式会社 | Vane wheel for blower |
| CN105793575A (en) * | 2013-09-30 | 2016-07-20 | 日清纺精密机器株式会社 | Bladed wheel for fan |
| JP2017214937A (en) * | 2017-09-19 | 2017-12-07 | 日清紡メカトロニクス株式会社 | Cross-flow fan |
| CN112412832A (en) * | 2020-10-28 | 2021-02-26 | 青岛海尔空调器有限总公司 | Cross-flow fans and air conditioners |
| WO2025014026A1 (en) * | 2023-07-11 | 2025-01-16 | 한온시스템 주식회사 | Vehicle blower unit |
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| Publication number | Publication date |
|---|---|
| JP3850061B2 (en) | 2006-11-29 |
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