JPH08200283A - Cross-flow fan and air conditioner provided with it - Google Patents

Cross-flow fan and air conditioner provided with it

Info

Publication number
JPH08200283A
JPH08200283A JP7012721A JP1272195A JPH08200283A JP H08200283 A JPH08200283 A JP H08200283A JP 7012721 A JP7012721 A JP 7012721A JP 1272195 A JP1272195 A JP 1272195A JP H08200283 A JPH08200283 A JP H08200283A
Authority
JP
Japan
Prior art keywords
cross
blade
blades
flow fan
pitch
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
Application number
JP7012721A
Other languages
Japanese (ja)
Inventor
Yoji Sekine
洋治 関根
Yuuji Kofude
裕二 小筆
Takashi Saotome
隆 早乙女
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.)
Hitachi Ltd
Original Assignee
Hitachi Ltd
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 Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP7012721A priority Critical patent/JPH08200283A/en
Publication of JPH08200283A publication Critical patent/JPH08200283A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/281Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
    • F04D29/282Rotors 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
    • F04D29/283Rotors 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/666Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by means of rotor construction or layout, e.g. unequal distribution of blades or vanes

Abstract

PURPOSE: To reduce a rotational sound of low frequency according to rotation by tilting an individual blade at a prescribed angle in the same direction relating to an axial direction parallel line from one end disk leading to the other end disk of a plurality of the support disks, also arranging the blade by a random pitch in the peripheral direction. CONSTITUTION: A cross-flow fan 1 of an air conditioner has blades 2... which are a single sheet blade inserted through each support disk 3 from one end to the other end of a plurality of the support disks 3 arranged with an almost equal space in an axial direction of the fan. Each blade 2 is uniformly formed with a tilt, so-called skew, of advancing a drive side (motor 5 side) rather than a driven side (shaft 4 side) by a prescribed amount in a rotational direction U. The blade 2 is formed in a sectional shape bent to be tilted forward to a side of the rotational direction U, to arrange the many blades 2 in a peripheral direction aside the periphery of the support disk 3 by random pitches P1 , P2 , P3 , P4 ...P34 . This random degree δ (maximum pitch/minimum pitch) is selected to a prescribed value in a 1.2 to 1.5 range.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、貫流ファンおよびこれ
を備えた空気調和機に係り、特に、軸方向の翼並び(位
相)に起因する羽根車体の回転音と流れによる乱れ音を
低下させ、翼ピッチに関係する回転一次音、熱交換器位
置に起因する回転二次音を低下させるに好都合で、か
つ、騒音レベルも低く聴感のよいものが得られ、空気調
和機のコンパクト化あるいは省資源、省エネルギ−に貢
献する構造の貫流ファンおよびこれを備えた空気調和機
に関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a cross-flow fan and an air conditioner equipped with the same, and particularly to reduce the rotational noise of the blade body and the turbulent noise caused by the flow due to the blade arrangement (phase) in the axial direction. , A rotary primary sound related to the blade pitch, and a secondary rotary sound due to the position of the heat exchanger, which is convenient and has a low noise level and good audibility, can be obtained, and the size of the air conditioner can be reduced or reduced. The present invention relates to a once-through fan having a structure that contributes to resource and energy saving, and an air conditioner including the same.

【0002】[0002]

【従来の技術】従来の貫流ファンは、回転音を低減する
方法として、例えば、実開平4−79991号公報記載
のように、故意に羽根の弦長あるいは羽根ピッチを翼列
方向(周方向)にランダムにし、その羽根車を複数個連
結した構造が知られていた。また、例えば、実開昭52
−132312号公報記載のように、翼を、支え円板の
左端から右端に至り一枚翼で、軸方向に対して所定角度
傾斜させ、翼列が等ピッチのものが知られていた。そし
て、翼の断面は翼列の内周側から外周側にかけて同一曲
率で回転方向にわん曲するものであった。この種の貫流
ファンを用いた空気調和機は、熱交換器の影響で騒音が
発生するのを防止するために、熱交換器を貫流ファンか
らできるだけ遠ざけて配置していた。
2. Description of the Related Art In a conventional cross-flow fan, as a method of reducing the rotation noise, for example, as described in Japanese Utility Model Laid-Open No. 4-79991, the chord length or blade pitch of the blades is intentionally set in the blade row direction (circumferential direction). A structure in which a plurality of impellers are connected randomly is known. Also, for example, the actual exploitation 52
As described in Japanese Patent No. 13232312, it has been known that the blade is a single blade extending from the left end to the right end of the supporting disk and is inclined at a predetermined angle with respect to the axial direction, and the blade row has an equal pitch. The blade cross section is curved in the rotational direction with the same curvature from the inner peripheral side to the outer peripheral side of the blade row. In an air conditioner using this type of cross-flow fan, the heat exchanger is arranged as far as possible from the cross-flow fan in order to prevent noise from being generated due to the influence of the heat exchanger.

【0003】[0003]

【発明が解決しようとする課題】上記従来技術の前者に
おいて、翼(ブレード)の弦長のランダムなものは、弦
長の短い翼の分だけ弦長の長い翼を設けて能力を上げる
必要があり、その分だけファン外径が大となる問題があ
った。
In the former case of the above-mentioned prior art, in the case where the chord length of the blade is random, it is necessary to increase the ability by providing a blade having a longer chord length for the shorter chord length. However, there was a problem that the outer diameter of the fan would be correspondingly large.

【0004】図11は、従来の貫流ファンの正面図、図
12は、図11のB−B矢視断面図、図13は、図11
の貫流ファンを備えた従来の空気調和機の縦断面図であ
る。図11に示す貫流ファン31は、円板に垂直に翼3
2が支持された横幅(軸方向長さ)の小さい小羽根車3
1aを多数連結することにより一台の送風機を構成して
いるものである。図12に示すように、翼列方向の羽根
ピッチをランダムにしたものは、連結部すなわち支え円
板33を境に翼32の位相が急激にずれることとなり小
羽根車31aの連結数に関係する低周波の回転音が発生
する。そして、風の流れに関しても、連結部を中心に左
右の速度差により干渉を生じて流体音が大きくなり風量
も減少するという問題があった。
FIG. 11 is a front view of a conventional cross-flow fan, FIG. 12 is a sectional view taken along the line BB of FIG. 11, and FIG.
FIG. 8 is a vertical cross-sectional view of a conventional air conditioner including the cross-flow fan of FIG. The cross-flow fan 31 shown in FIG. 11 has blades 3 perpendicular to the disk.
Small impeller 3 with a small width (axial length) supporting 2
One air blower is configured by connecting a plurality of 1a. As shown in FIG. 12, in the case where the blade pitch in the blade row direction is random, the phase of the blades 32 is abruptly deviated at the connecting portion, that is, the supporting disk 33, and is related to the number of small impellers 31a connected. Low-frequency rotating noise is generated. Also, regarding the flow of wind, there is a problem in that interference occurs due to the difference in speed between the left and right sides of the connecting portion, the fluid noise increases, and the air volume decreases.

【0005】また、翼列方向のピッチP01,P02,…の
ランダム化は多数の組合せが考えられ、ランダム度(こ
こでは、最大ピッチ/最小ピツチの比をいうことにす
る)によっては、回転音が意向に反して高くなってしま
うという問題があるこについて認識が不足していた。こ
れに加えて、吸込側に能力の小さい翼32(弦の小さい
あるいはピツチの狭い部分)がきて、同時に吐出側にも
能力の小さい翼32がきた場合には風量が減少し、これ
と反対の場合には風量が増加する。したがって、通風量
の変動や振動の発生を招き、これと同時に羽根車体の振
動数(あるいは回転数)に合う整数倍の回転音を生ずる
問題があった。
A large number of combinations can be considered for randomizing the pitches P 01 , P 02 , ... In the blade row direction, and depending on the degree of randomness (here, the maximum pitch / minimum pitch ratio will be referred to), There was a lack of awareness about the problem that the rotating sound was unintentionally high. In addition to this, if a blade 32 with a small capacity (a part with a small string or a narrow pitch) comes to the suction side and at the same time a blade 32 with a small capacity also comes to the discharge side, the air volume decreases, which is the opposite of this. In some cases, the air volume will increase. Therefore, there is a problem in that the amount of ventilation is changed and vibrations are generated, and at the same time, a rotation sound that is an integral multiple of the vibration frequency (or rotation speed) of the blade body is generated.

【0006】上記従来技術の後者の貫流送風機は、支え
円板の左端から右端に至り一枚翼のものであるが、同一
翼に対しては軸方向の位相のずれ(階段状で一般に小羽
根車ひとつおきに同位相となる)があっても、翼列が等
ピッチで翼間寸法が全て同じであるために、翼と固定ケ
−シングとの干渉や翼間の流れ形態が同じことから、翼
数に起因する回転一次音の発生を十分に無くすことがで
きないという問題があった。
The latter through-flow blower of the above-mentioned prior art is a single blade extending from the left end to the right end of the supporting disk, but with respect to the same blade, there is a phase shift in the axial direction (stepwise generally small blades. (Each vehicle has the same phase), but because the blade rows have the same pitch and the dimensions between blades are all the same, the interference between the blades and fixed casing and the flow form between the blades are the same. However, there is a problem that the generation of the rotating primary sound due to the number of blades cannot be sufficiently eliminated.

【0007】また、以上の前者,後者の翼32は翼列の
内周側から外周側にかけて、ふくらみ側、へこみ側とも
に各々一円曲率にして、内周側と外周側が対称形状のほ
ぼ三日月形にした樹脂製のものや、あるいは同一厚みの
金属板を同心曲率で回転方向にわん曲したものであっ
た。そのため、図13に示すように、空気調和機をコン
パクトにするために、熱交換器33を貫流ファン31に
接近して配置しようとすると、翼端は風の流入に敏感に
影響し、熱交換器33のフイン33aとパイプ33b近
辺の流速分布の違いにより、回転移動する翼32への流
入状況の変動が激しくなり、翼32部から回転二次音を
発生するという問題があり、従来技術は、これを防止す
るための配慮が不足していた。
The former and latter blades 32 have a substantially crescent shape in which the inner peripheral side and the outer peripheral side are symmetrical, with a bulge side and a concave side each having a circular curvature from the inner peripheral side to the outer peripheral side of the blade row. It was made of a resin or a metal plate of the same thickness bent in the rotational direction with concentric curvature. Therefore, as shown in FIG. 13, when it is attempted to arrange the heat exchanger 33 close to the cross-flow fan 31 in order to make the air conditioner compact, the blade tips sensitively affect the inflow of wind and the heat exchange is performed. Due to the difference in the flow velocity distribution in the vicinity of the fin 33a of the vessel 33 and the pipe 33b, the fluctuation of the inflow situation into the rotatively moving blade 32 becomes severe, and there is a problem that a rotational secondary sound is generated from the blade 32 portion. , There was a lack of consideration to prevent this.

【0008】本発明は、上記従来技術の問題点を解決す
るためになされたものであり、その第一の目的は、翼の
支え円板近辺の不連続な流体音を低減し、風量変動を少
なくし、羽根車としての回転に伴う低周波数の回転音を
低減し、また、これにより周波数の高い翼数に関係する
回転一次音を主体に低減し、付随して翼数に関する回転
二次音を低減し、聴感のよい低騒音の貫流ファンを提供
することにある。また、本発明の第二の目的は、上記貫
流ファンを用いることにより、熱交換器の後流に発生す
る回転二次音を主体に低減して製品の低騒音化とコンパ
クト化をはかり、それにより、省資源化あるいは省エネ
ルギ−化にも貢献できる空気調和機を提供することにあ
る。
The present invention has been made in order to solve the above-mentioned problems of the prior art, and the first object thereof is to reduce the discontinuous fluid noise near the supporting disk of the blade and to reduce the air flow fluctuation. This reduces the low-frequency rotation noise that accompanies the rotation of the impeller, and mainly reduces the rotational primary sound related to the number of blades with high frequency. It is to provide a low-flow once-through fan with good hearing and low noise. A second object of the present invention is to reduce the secondary noise generated in the downstream of the heat exchanger mainly by using the cross-flow fan to reduce the noise and compact the product. Accordingly, it is to provide an air conditioner that can contribute to resource saving or energy saving.

【0009】[0009]

【課題を解決するための手段】上記第一の目的を達成す
るために、本発明の貫流ファンに係る第一の発明の構成
は、軸方向に所定間隔に並べた複数の支え円板の外周寄
りの周方向に、多数の翼を配列してなる貫流ファンにお
いて、前記の個々の翼を、前記複数の支え円板の一端の
円板から他端の円板に至る軸方向平行線に対して所定角
度で同一方向に傾斜させるとともに、前記多数の翼は、
周方向にランダムなピッチで配列したものである。より
詳しくは、個々の翼は、その翼の断面形状における外周
側先端を、それより内側の曲率よりわずかに強くした曲
率で回転方向に傾けたものである。
In order to achieve the above-mentioned first object, the structure of the first invention relating to the cross-flow fan of the present invention is the outer circumference of a plurality of supporting discs arranged in the axial direction at predetermined intervals. In a cross-flow fan in which a large number of blades are arranged in the circumferential direction closer to each other, the individual blades are arranged with respect to an axial parallel line extending from a disc at one end of the plurality of supporting discs to a disc at the other end. And inclining in the same direction at a predetermined angle, the multiple wings are
It is arranged at a random pitch in the circumferential direction. More specifically, each blade has a tip end on the outer peripheral side in the cross-sectional shape of the blade inclined in the rotational direction with a curvature slightly larger than the curvature inside thereof.

【0010】また、上記第一の目的を達成するために、
本発明の貫流ファンに係る第二の発明の構成は、支え円
板の外周寄りの一面に、周方向に多数の翼を配列してな
る一体成形の小羽根車を、軸方向に複数個連結してなる
貫流ファンにおいて、前記多数の翼は、支え円板を介し
て、その複数の支え円板の一端の円板から他端の円板に
至る軸方向平行線に対して、所定角度で直線状ならびに
同一方向に傾斜したものである。そして、多数の翼は、
周方向にランダムなピッチで配列したものであり、多数
の翼は、その翼の断面形状における外周側先端を、それ
より内側の曲率よりわずかに強くした曲率で回転方向に
傾けたものである。
Further, in order to achieve the above first object,
The structure of the second invention relating to the cross-flow fan of the present invention is such that a plurality of integrally-formed small impellers each having a plurality of blades arranged in the circumferential direction are axially connected to one surface near the outer circumference of the supporting disk. In the cross-flow fan, the plurality of blades are arranged at a predetermined angle with respect to an axial parallel line extending from a disc at one end of the plurality of support discs to a disc at the other end through the support discs. It is straight and inclined in the same direction. And many wings
The blades are arranged at random pitches in the circumferential direction, and a large number of blades are obtained by inclining the outer circumferential end of the blades in the cross-sectional shape in the rotational direction with a curvature slightly stronger than the inner curvature.

【0011】翼の軸方向平行線に対する傾斜は、羽根車
を複数個連結する構成であっても個々の羽根車について
行なうことにより達成できる。前記第一,第二の発明に
おいて、軸方向平行線に対する翼の傾斜角度(スキュ−
角度)を1°〜4.5°傾け、翼の周方向の配列は、ラ
ンダム度(最大ピッチ/最小ピツチ)を1.2〜1.5
に設定することにより効果高く達成できる。
The inclination of the blade with respect to the parallel line in the axial direction can be achieved by performing it for each impeller even if a plurality of impellers are connected. In the first and second aspects of the invention, the blade inclination angle (skew
Angle) of 1 to 4.5 degrees, and the arrangement of the blades in the circumferential direction is a random degree (maximum pitch / minimum pitch) of 1.2 to 1.5.
It can be achieved highly effectively by setting to.

【0012】上記貫流ファンは支え円板に翼の挿入作業
終了後に羽根車を捻じり、翼を支え円板のカシメあるい
は溶着等により固定することにより容易に製作できる。
あるいは、樹脂製の複数個連結形のファンの場合は、翼
間成形型をわずかの回転スライド式にすることにより容
易に製作できる。
The cross-flow fan can be easily manufactured by twisting the impeller after the work of inserting the blade into the supporting disk and fixing the blade by caulking or welding the supporting disk.
Alternatively, in the case of a plural-connection type fan made of resin, it can be easily manufactured by making the blade-to-blade forming die a slight rotary slide type.

【0013】また、上記第二の目的を達成するために、
本発明に係る空気調和機の構成は、上記のいずれかの貫
流ファンを用い、その貫流ファンの入口開口部側に、少
なくとも2個所の曲げ部を有して前記貫流ファンを包囲
する断面構成のクロスフィンパイプ形熱交換器を配設
し、ケーシングに前記熱交換器に見合う位置に吸込開口
部を設けたものである。
In order to achieve the above second object,
The structure of the air conditioner according to the present invention uses one of the cross-flow fans described above, and has a cross-sectional structure that surrounds the cross-flow fan by having at least two bent portions on the inlet opening side of the cross-flow fan. A cross fin pipe type heat exchanger is provided, and a suction opening is provided at a position corresponding to the heat exchanger in the casing.

【0014】[0014]

【作用】上記各技術的手段の働きは下記の通りである。
すなわち、翼を、支え円板の左端から右端に至り一枚翼
にて軸方向平行線に対して所定角度傾斜させることによ
り、また、羽根車の複数個連結形の場合には各羽根車毎
に翼を所定角度傾斜させて支え円板を経て直線状に並べ
ることにより、支え円板部毎の階段状の翼の位相ずれは
皆無となり、滑らかな回転が得られる。したがって、支
え円板を境にした流速変化および乱れの少ないスム−ズ
な流れが得られるほか、羽根車体としての回転に伴う低
周波数の振動(毎秒回転数およびその整数倍周波数)お
よび、その回転音を無くすことができる。
The function of each of the above technical means is as follows.
That is, the blade is inclined from the left end to the right end of the supporting disk by a predetermined angle with respect to the parallel line in the axial direction with a single blade, and in the case of a plurality of connected impellers, each impeller is By tilting the blades by a predetermined angle and arranging them linearly through the supporting discs, there is no stepped phase deviation of the blades for each supporting disc portion, and smooth rotation can be obtained. Therefore, a smooth flow with little change in flow velocity and turbulence at the supporting disk is obtained, and low-frequency vibration (rotation speed per second and its integral multiple frequency) accompanying rotation of the blade body and its rotation are obtained. You can eliminate the sound.

【0015】また、翼の周方向の配列(羽根ピッチ)を
ランダムに配置することにより、翼移動の周期性を無く
し翼数に関係する周波数の高い回転音を分散させること
ができるとともに、翼間寸法の違いにより流体音の発生
周波数が分散して聴き易くなり、騒音のレベルも低くす
ることができる。さらに、翼断面の先端(翼列外周側)
のわずかを、それより内側の曲率よりわずかに強くした
曲率で回転方向に傾けた構成とすることにより、前ケ−
シングの流入端部からの翼に急激な入り込み開始を柔ら
げ、回転一次音を主に、付随して回転二次音の発生をも
少なくし、同時に翼の強度を向上させる。
Further, by randomly arranging the blades in the circumferential direction (blade pitch), it is possible to eliminate the periodicity of blade movement and to disperse high-frequency rotation noise related to the number of blades, and also between blades. Due to the difference in size, the generation frequency of the fluid sound is dispersed to make it easier to hear, and the noise level can be lowered. Furthermore, the tip of the blade section (outer side of the blade row)
By arranging a small amount of
It softens the start of sudden entry into the wing from the inflow end of the sing, and reduces the generation of rotational secondary sound, mainly accompanying rotational primary sound, and at the same time improves the strength of the wing.

【0016】本発明の貫流ファンを用いた空気調和機
は、上記作用に加え、貫流ファンに近接して配置した熱
交換器の後流の不均一な速度分布に対して、翼部通過時
の流入変化を少なくして、特に、翼と熱交換器との干渉
による回転二次音を低減させることができる。したがっ
て、騒音の聴感を良くし、騒音レベル(オ−バ−オ−ル
値)を低減できる。空気調和機構造としては、熱交換器
が貫流ファンを包囲するように近接して配置されてコン
パクトに構成できるほかに、大きな伝熱面積を持たせる
ことができるので、熱交換能力を向上させ、その分を省
資源や省エネルギ−化(省電力)させることができる。
In addition to the above-mentioned operation, the air conditioner using the cross-flow fan according to the present invention has a non-uniform velocity distribution in the wake of the heat exchanger arranged in the vicinity of the cross-flow fan. The change in inflow can be reduced, and in particular, the secondary sound due to the interference between the blade and the heat exchanger can be reduced. Therefore, the audibility of noise can be improved and the noise level (overall value) can be reduced. As an air conditioner structure, the heat exchanger is arranged in close proximity so as to surround the once-through fan and can be configured compactly, and since it can have a large heat transfer area, the heat exchange capacity is improved, The amount can be saved as resources and energy (power).

【0017】[0017]

【実施例】以下、本発明の各実施例を図1ないし図10
を参照して具体的に説明する。 〔実施例 1−1〕まず、図1は、第一の発明の一実施
例に係る貫流ファンの正面図、図2は、図1の羽根車の
A−A矢視断面図、図3は、図1および後述する図4,
6に示す貫流ファンを備えた空気調和機の縦断面図であ
る。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Hereinafter, each embodiment of the present invention will be described with reference to FIGS.
It will be specifically described with reference to. [Embodiment 1-1] First, FIG. 1 is a front view of a cross-flow fan according to an embodiment of the first invention, FIG. 2 is a sectional view of the impeller of FIG. , FIG. 1 and FIG.
6 is a vertical cross-sectional view of an air conditioner including the cross-flow fan shown in FIG.

【0018】図1,2に示す翼2は、貫流ファン1の軸
方向にほぼ等間隔に並べた複数個の支え円板3の一端か
ら他端、すなわち図1に向かって左端から右端に至り各
支え円板3を一枚翼にて貫通するものである。各翼2は
一様に、被駆動側(軸4側)よりも駆動側(モ−タ5
側)を所定の量で回転方向U進ませた傾斜、いわゆる、
スキュ−を形成している。その翼2の断面は、同一厚み
の素材を、矢印に示す回転方向U側に一円弧に塑性加工
してわん曲前傾させてある。上記所定の傾斜角度の量
は、軸方向に平行線を想定して該平行線に対する翼の傾
斜角度θを、展開図で1°〜4.5°(軸方向平行線を
底辺とし、軸方向最端の外周上に沿ってずれる平面展開
距離とのtan角の範囲で所定値に選定し、この種ファ
ンでは約1.5ピッチ分〜約6.0ピッチ分に相当す
る)としたものである。
The blades 2 shown in FIGS. 1 and 2 extend from one end to the other end of a plurality of supporting discs 3 arranged at substantially equal intervals in the axial direction of the cross-flow fan 1, that is, from the left end to the right end in FIG. One blade penetrates each supporting disk 3. Each blade 2 is evenly arranged on the drive side (motor 5) rather than the driven side (shaft 4 side).
(Side) is moved by a predetermined amount in the direction U of rotation, a so-called inclination,
It forms a skew. The blade 2 has a cross section in which a material having the same thickness is plastically worked into a circular arc on the side in the direction of rotation U indicated by an arrow and is bent and bent forward. As for the amount of the predetermined inclination angle, the inclination angle θ of the blade with respect to the parallel line is assumed to be 1 ° to 4.5 ° in the development view (assuming the parallel line to the axial direction, the axial parallel line is the base, and the axial direction is the axial direction). It is set to a predetermined value within the range of the tan angle with the plane development distance shifted along the outermost periphery, and this type of fan corresponds to about 1.5 pitch to about 6.0 pitch). is there.

【0019】また、翼2は支え円板3の外周寄り周方向
にランダムなピッチP1,P2,P3,P4,……P34で多
数配置し、そのランダム度δ(最大ピッチ/最小ピツ
チ)を1.2〜1.5の範囲にて所定値に選定し、ピッ
チの並び順が同一になる部分ができるだけ無いようにし
てある。6は前ケ−シングであって、図3に示すように
貫流ファン1からわずかに離れ、周囲を約10%包囲し
て、回転方向Uに遅れる端を入口用の前縁6aとなし、
貫流ファン1の軸方向外周と狭い平行な距離をなしてい
て、他方の回転方向Uに早い端を出口用の舌部6bと
し、貫流ファン1との距離を上記前縁6aよりも大にし
ている。そしてその裏側を第一の露受皿6cとして兼ね
ている。
Further, a large number of blades 2 are arranged at a random pitch P 1 , P 2 , P 3 , P 4 , ... P 34 in the circumferential direction near the outer circumference of the supporting disk 3, and the randomness δ (maximum pitch / The minimum pitch) is selected to be a predetermined value within the range of 1.2 to 1.5 so that there is no portion where the pitch arrangement order is the same as much as possible. Reference numeral 6 denotes a front casing, which is slightly separated from the cross-flow fan 1 and surrounds the periphery by about 10% as shown in FIG. 3, and the end delayed in the rotational direction U is formed as a front edge 6a for the inlet.
A narrow parallel distance is formed with the outer periphery of the cross-flow fan 1 in the axial direction, and the end that is early in the other rotation direction U is used as an outlet tongue portion 6b, and the distance with the cross-flow fan 1 is made larger than the front edge 6a. There is. The back side thereof also serves as the first dew tray 6c.

【0020】また、7は後ケ−シングであって、上記前
縁6aから約180°ずれた位置を巻き始点7aとして
貫流ファン1からわずかに離れ、貫流ファン1の周囲を
回転方向Uにそって次第に遠ざかり約90°余巻いて巻
き終端7bを形成している。前記前縁6aと巻き始点7
aとの間を入口開口部9、舌部6bと巻き終端7bとの
間を出口開口部10としている。前ケ−シング6は入口
開口部9と出口開口部10の圧力仕切作用をなし、後ケ
−シング7は流れを外部空気から隔離して送風の効率を
高め、流れの方向の案内の役目も果たすものである。
Further, 7 is a rear casing, which is slightly separated from the cross-flow fan 1 with a position shifted by about 180 ° from the front edge 6a as a winding start point 7a, and is gently swirled around the cross-flow fan 1 in the rotational direction U. The winding end 7b is formed by gradually winding away the extra 90 °. The leading edge 6a and the winding start point 7
The inlet opening 9 is defined between a and a, and the outlet opening 10 is defined between the tongue 6b and the winding end 7b. The front casing 6 functions as a pressure partition between the inlet opening 9 and the outlet opening 10, and the rear casing 7 separates the flow from the outside air to improve the blowing efficiency and also serves as a guide for the flow direction. To fulfill.

【0021】11は、流れが翼部を貫通することにより
生じる内部渦、12は、前縁6aの後流にできる自由
渦、13はクロスフインパイプ形の熱交換器であって、
入口開口部9にて、その断面を三個所曲げにして貫流フ
ァン1を包囲するように近接して配設してある。16は
外箱、16aは前面,上面,上後面の吸込開口部であっ
て、熱交換器13の前面に見合う位置に設けてある。1
7は冷媒輸送用の配管、18は据付の係合部、19は据
付板、20は第二露受皿である。
Reference numeral 11 is an internal vortex generated by the flow passing through the blade portion, 12 is a free vortex that can be formed in the backflow of the leading edge 6a, and 13 is a cross-fin pipe type heat exchanger,
At the inlet opening 9, the cross section thereof is bent at three places, and the cross-flow fan 1 is disposed so as to surround it. Reference numeral 16 denotes an outer box, and 16a denotes suction openings on the front surface, the upper surface, and the upper rear surface, which are provided at positions corresponding to the front surface of the heat exchanger 13. 1
Reference numeral 7 is a pipe for transporting the refrigerant, 18 is an engaging portion for installation, 19 is an installation plate, and 20 is a second dew tray.

【0022】上記のように構成した貫流ファン1は、ケ
−シング6,7の間で回転させることにより、遠心力に
よって前ケ−シング6寄りの羽根車内に内部渦11を発
生させ、風は通風路の幅の広い入口開口部9から吸い込
まれ、羽根車内を貫通して内部渦11を中心に約90°
以上偏向して通風路の幅の狭い出口開口部10から吐出
される。
The cross-flow fan 1 constructed as described above is rotated between the casings 6 and 7 to generate an internal vortex 11 in the impeller near the front casing 6 by centrifugal force, and the wind is generated. It is sucked from the wide inlet opening 9 of the ventilation passage, penetrates the inside of the impeller, and has an internal vortex 11 at a center of about 90 °.
It is deflected as described above and discharged from the outlet opening 10 having a narrow width of the ventilation passage.

【0023】ここで、翼2が前ケ−シング6寄りを移動
する場合、前ケ−シング6と翼2の間の流速は入口開口
部9に向かって翼2より速く移動し、翼間においては流
れが停滞して翼2との相対速度は零に等しい状況で進
み、翼2が前縁6aに来た途端に翼間から急激に羽根車
内に流入する。従来は、この流れ変化と同時に生じる前
縁6aからの急激な流入、および前縁6aから発生する
自由渦12が翼2へ流入する際に翼2と干渉し、回転一
次音および高周波の乱れ音を生じていた。
Here, when the blade 2 moves near the front casing 6, the flow velocity between the front casing 6 and the blade 2 moves toward the inlet opening 9 faster than that of the blade 2, and between the blades. Flows in a situation where the flow is stagnant and the relative velocity with the blades 2 is equal to zero, and as soon as the blades 2 reach the leading edge 6a, they rapidly flow into the impeller from between the blades. Conventionally, a rapid inflow from the leading edge 6a that occurs at the same time as this flow change, and a free vortex 12 generated from the leading edge 6a interferes with the blade 2 when flowing into the blade 2 and causes a rotating primary sound and a high-frequency turbulent sound. Was occurring.

【0024】しかし、本貫流ファンの構成は、翼2が支
え円板3の左端から右端に至り、全数翼を軸方向平行線
に対して所定角度同一方向に傾斜させてあるので、前記
前縁6aに対する翼位相のずれは左端から右端に至り、
段差なく少しずつ連続的に行なわれることになり、ま
た、支え円板3を境にした左右で翼2に位相差が無くな
る。したがって、左右の速度がほぼ同一になって干渉が
無くなり、全幅にわたり翼2への流入を滑らかにでき
る。このため、回転一次音の低減はもとより、流れの変
動が少なくなり、羽根車体としての回転の低周波の振動
(一秒間あたりの回転数の整数倍の周波数)および従来
干渉により生じていた高周波の流体騒音(一次回転音よ
り高い周波数)も低減することができる。
However, in the structure of this cross-flow fan, since the blades 2 extend from the left end to the right end of the supporting disk 3 and all the blades are inclined in the same direction at a predetermined angle with respect to the parallel lines in the axial direction, The blade phase shift for 6a goes from the left end to the right end,
The steps are performed continuously little by little, and there is no phase difference between the blades 2 on the left and right with the support disk 3 as a boundary. Therefore, the left and right velocities are substantially the same, interference is eliminated, and the inflow to the blade 2 can be made smooth over the entire width. For this reason, the fluctuation of the flow is reduced as well as the reduction of the primary sound of rotation, and the low-frequency vibration of the rotation of the blade body (a frequency that is an integral multiple of the number of rotations per second) and the high-frequency waves that have been generated due to the conventional interference. Fluid noise (frequency higher than the primary rotation sound) can also be reduced.

【0025】実際に、冷却能力2.5kWの図3に示す
ような、クロスフィンパイプ形の熱交換器13を、その
断面を三個所で曲げた形にして伝熱面積を稼ぐ構成にし
て、貫流ファン1を包囲するようにコンパクトに配設し
た空気調和機試作品を用いて、外径90mm、軸方向長
さ634mm、翼数34枚、等ピッチ翼、断面二重円弧
翼の樹脂製貫流ファン1を組み込み、毎分1242回転
で運転し、それを10Hzピッチで騒音分析を行なっ
た。
Actually, as shown in FIG. 3 having a cooling capacity of 2.5 kW, the cross-fin pipe type heat exchanger 13 is formed by bending the cross section at three points to increase the heat transfer area. Using an air conditioner prototype that is compactly arranged to surround the cross-flow fan 1, an outer diameter of 90 mm, axial length of 634 mm, number of blades of 34, uniform pitch blade, cross-flow double arc blade made of resin The fan 1 was incorporated and operated at 1242 rpm, and noise analysis was performed at a 10 Hz pitch.

【0026】図7は、図1の実施例の貫流ファン1の、
翼2に連続スキューをしたものの効果を示す騒音分析結
果の線図である。図7は、横軸に周波数(Hz)、縦軸
に音圧レベル(dB)をとり、本実施例の連続スキュー
ファンのデータを破線、従来の階段状位相ファンのデー
タを実線で示したものである。
FIG. 7 shows the cross-flow fan 1 of the embodiment of FIG.
It is a diagram of the noise analysis result which shows the effect of what made the blade 2 the continuous skew. FIG. 7 shows the frequency (Hz) on the horizontal axis and the sound pressure level (dB) on the vertical axis, showing the data of the continuous skew fan of this embodiment with a broken line and the data of the conventional stepwise phase fan with a solid line. Is.

【0027】図7に示すように、支え円板毎に翼32の
半ピッチずつの階段状位相のある従来の樹脂製の複数個
連結形ファン(図11参照)と比較して、本実施例の翼
2の連続した傾斜角度θが2.6°のものでは、羽根車
体としての毎秒回転数Nに関係する整数倍の低周波1N
(20.7Hz)〜20N(414Hz)の回転音が3
dB〜9dB低減でき、回転一次音1NZ(704H
z)についても30dBあったものが24dBまで6d
B低減でき、騒音のオ−バ−オ−ル値では42dBであ
ったものが41dBになり1dB低減できた。また、風
量を4%増加させる効果を確認できた。同一風量で実質
の効果を比較するとオ−バ−オ−ル値で2dBの低減が
できたことになる。
As shown in FIG. 7, this embodiment is compared with a conventional multi-connection fan made of resin (see FIG. 11) having a stepwise phase of half pitch of blades 32 for each supporting disk. When the blade 2 has a continuous inclination angle θ of 2.6 °, an integral multiple of low frequency 1N related to the rotation speed N per second as the blade body
(20.7Hz) ~ 20N (414Hz) rotating sound is 3
dB to 9 dB can be reduced, and the rotating primary sound 1NZ (704H
As for z), what was 30 dB was 6 dB up to 24 dB.
B could be reduced, and the noise over-all value was 42 dB from 41 dB to 1 dB. Also, the effect of increasing the air volume by 4% was confirmed. Comparing the actual effects with the same air volume, it is possible to reduce the over-all value by 2 dB.

【0028】また、図示は省略したが、傾斜角度θが1
°未満のものでは効果を確認できず、傾斜角度θが4.
5°を越えると翼の塑性加工に無理な歪み個所(例えば
翼の断面傾きの過不足個所)および支え円板を除いた個
所に外径が小になる部分ができて、回転一次音1NZが
高くなるに加え風量が少なくなることがわかった。
Although not shown, the inclination angle θ is 1
If it is less than °, the effect cannot be confirmed, and the tilt angle θ is 4.
If it exceeds 5 °, there will be a part where the outer diameter is small at the strained part where the plastic working of the blade is impossible (for example, the part where the blade cross-section inclination is excessive or insufficient) and the part where the supporting disc is removed, and the rotating primary sound 1NZ It was found that the air volume decreased as the temperature increased.

【0029】また、本発明では翼2の周方向の配列は、
ランダム度δ(最大ピッチ/最小ピツチ)を1.2〜
1.5の範囲にて所定ピッチに配列したことに特徴があ
るので、前ケ−シング6の前縁6aに対して翼2の通過
に周期性を無くして、翼数に関する回転一次音1NZを
低減できるとともに翼ピッチP1,P2,P3,P4,…P
34の寸法が各々異なり分散しているので、流体音を広い
周波数帯域に分散し、音圧レベルも低く聴き易い騒音に
できる。
In the present invention, the circumferential arrangement of the blades 2 is
Randomness δ (maximum pitch / minimum pitch) 1.2 to
Since it is characterized in that the blades are arranged at a predetermined pitch in the range of 1.5, there is no periodicity in the passage of the blade 2 with respect to the front edge 6a of the front casing 6, and the rotating primary sound 1NZ relating to the number of blades is obtained. The blade pitch can be reduced and the blade pitches P 1 , P 2 , P 3 , P 4 , ... P can be reduced.
Since the 34 dimensions are different and dispersed, the fluid sound can be dispersed in a wide frequency band, and the sound pressure level can be made low to make it easy to hear.

【0030】実験によれば、前述と同様に図3の空気調
和機試作品を用いて、外径90mm、軸方向長さ634
mm、翼数34枚、翼15の傾斜角度θが2.6°、断
面二重円弧翼の樹脂製貫流ファンを組み込み、毎分12
42回転で行ない、それを10Hzピッチで騒音分析を
行なった。その結果、翼配列のランダム度δが1.43
のものが最も優れていた。図8は、図1の実施例の貫流
ファンの、二重円弧の翼でランダムピッチにしたものの
効果を示す騒音分析結果の線図である。図8は、横軸に
周波数(Hz)、縦軸に音圧レベル(dB)をとり、ラ
ンダムピッチ翼ファンのデータを実線、等ピッチ翼ファ
ンのデータを破線で示したものである。
According to the experiment, the air conditioner prototype shown in FIG. 3 was used as described above, and the outer diameter was 90 mm and the axial length was 634.
mm, the number of blades is 34, the inclination angle θ of the blades 15 is 2.6 °, and a resin cross-flow fan with a double circular arc blade in cross section is incorporated, and 12 per minute
It was performed at 42 rotations, and noise analysis was performed at a 10 Hz pitch. As a result, the randomness δ of the blade arrangement is 1.43.
The ones were the best. FIG. 8 is a diagram of a noise analysis result showing an effect of the cross-flow fan of the embodiment of FIG. 1 in which a double-arc blade has a random pitch. FIG. 8 shows the frequency (Hz) on the horizontal axis and the sound pressure level (dB) on the vertical axis, and shows the data of the random pitch blade fan with a solid line and the data of the equal pitch blade fan with a broken line.

【0031】図8に実線で示すように、翼数に関係する
回転一次音1NZは翼配列が等ピッチであるものが24
dBあったのに対し19dBと5dB低減し、一次音の
低下に付随して、回転二次音2NZは26dBから20
dBに6dBの低減が得られた。騒音のオ−バ−オ−ル
値では41dBであったものがを39.5dBになり、
風量はほとんど変わらず、その変動も少なくなり、1.
5dBの低減効果を確認できた。この場合、ランダム化
により翼間に狭い部分ができる影響で900Hz以上の
高周波の流体音が少し高くなったが、実際の聴感によれ
ば、むしろ残った回転音二次音2NZを目立たなくする
効果を生むことを確認できた。
As shown by the solid line in FIG. 8, the rotational primary sound 1NZ related to the number of blades has 24 blades with a uniform pitch.
It was reduced by 19 dB to 5 dB compared to dB, and the secondary secondary sound 2NZ was reduced from 26 dB to 20 with the decrease in the primary sound.
A 6 dB reduction in dB was obtained. The over-the-noise value of 41dB was changed from 41dB to 39.5dB,
The air volume is almost unchanged, and the fluctuation is small.
A reduction effect of 5 dB was confirmed. In this case, the high frequency fluid sound of 900 Hz or higher was slightly increased due to the influence of a narrow portion between the wings due to the randomization, but according to the actual hearing feeling, the effect of making the remaining rotational sound secondary sound 2NZ less noticeable. I was able to confirm that

【0032】また、図示は省略したが、ランダム度δが
1.2未満である場合には、回転音低減の効果は翼配列
が等ピッチであるものに比較し、騒音のオ−バ−オ−ル
値で0.5dB未満の効果である。ランダム度δが1.
5を越えると、羽根車体としての、低周波の回転一次音
1NZが生じはじめ、熱交換器後流の影響も受けて二次
音2NZも出てくる。一方、翼間に狭い部分ができるた
め二次音2NZ近辺からそれより高い周波数の音を発
し、また、翼間の広い部分の影響で羽根車体自身に低周
波数の振動を発生するようになり、翼配列が等ピッチで
あるものに比較し、騒音のオ−バ−オ−ル値は高くなっ
てしまうことを確認した。なお、最も優れていたランダ
ム度δが1.43においても、まだ回転二次音2NZが
ピ−クとしてスペクトルに残るが、これは熱交換器13
からの流れに影響されているものであるが、引き続き述
べる翼形状により解決し得るものである。
Although not shown in the figure, when the randomness δ is less than 1.2, the effect of reducing the rotating noise is compared with that in the blade array having a uniform pitch, and the noise is overwhelmed. -The effect is less than 0.5 dB in terms of the Rule value. Randomness δ is 1.
When the number exceeds 5, the low-frequency rotating primary sound 1NZ of the vane body begins to be generated, and the secondary sound 2NZ also appears due to the influence of the heat exchanger wake. On the other hand, since there is a narrow part between the wings, a sound with a higher frequency is emitted from the vicinity of the secondary sound 2NZ, and due to the wide part between the wings, low-frequency vibration is generated in the blade body itself. It was confirmed that the over-all value of noise was higher than that of the blades with the same pitch. Even if the best randomness δ is 1.43, the rotating secondary sound 2NZ still remains in the spectrum as a peak, but this is due to the heat exchanger 13
However, it can be solved by the blade shape described later.

【0033】〔実施例 1−2〕図4は、第一の発明の
他の実施例に係る貫流ファンの翼の拡大断面図、図5
(a)は、図4の翼への通風抵抗の小なる部分における
流入状況を説明する速度三角形、図5(b)は、図4の
翼への通風抵抗の大なる部分における流入状況を説明す
る速度三角形、図9は、図4の実施例の貫流ファンの、
翼先端曲げ増しを加えた効果を示す騒音分析結果の線図
である。
[Embodiment 1-2] FIG. 4 is an enlarged cross-sectional view of a blade of a cross-flow fan according to another embodiment of the first invention, FIG.
(A) is a velocity triangle for explaining the inflow situation in the portion where the draft resistance to the blade in FIG. 4 is small, and FIG. 5 (b) is the velocity triangle for explaining the inflow situation in the portion where the draft resistance to the blade in FIG. 4 is large. Speed triangle, FIG. 9 shows the flow-through fan of the embodiment of FIG.
It is a diagram of the noise analysis result which shows the effect which added the blade tip bending increase.

【0034】図4は、図1に示した貫流ファンの翼先端
に改良を加えた実施例である。破線は従来形状を示し、
実線は本実施例の形状を示すものである。図4に示す翼
14は、アルミあるいは鋼板を素材にして断面を同一厚
にした例であって、曲率に沿った翼長の約10%にあた
る外周側先端を、それより内側の大部分の曲率Raより
わずかに回転方向に強くした曲率Rbを有するもので、
羽根車の中心Oを通り翼14の先端厚中点Pを結ぶ中心
線OPの接線と翼14の先端厚中点Pの接線のなす角、
すなわち、外周側入口角Bb1を従来のBa1より約1
0°あまり小さくしているものである。
FIG. 4 shows an embodiment in which the blade tip of the once-through fan shown in FIG. 1 is improved. The broken line shows the conventional shape,
The solid line shows the shape of this embodiment. The blade 14 shown in FIG. 4 is an example in which the cross section is made of aluminum or a steel plate and has the same thickness, and the tip of the outer peripheral side, which is about 10% of the blade length along the curvature, has most of the inside curvature. It has a curvature Rb that is slightly stronger in the direction of rotation than Ra,
An angle formed by a tangent line of a center line OP connecting the tip thickness midpoint P of the blade 14 through the center O of the impeller and a tangent line of the tip thickness midpoint P of the blade 14,
That is, the outer peripheral inlet angle Bb1 is about 1 compared to the conventional Ba1.
It is made to be too small by 0 °.

【0035】続いて、図4に示す翼形状について、先端
を曲げた効用を図5(a),(b)に示す速度三角形に
より説明する。図5(a)において、U1は翼14の周
速度、V1は通風抵抗が小で風の流入の速い部分の流入
絶対速度、W1は風と翼の相対速度であってU1とV1
のベクトル和、α1は流入の速い部分の流入角であって
W1とU1とのなす角である。また、図5(b)におい
て、U2(=U1)は翼14の周速度、V2は通風抵抗
が大で風の流入の遅い部分の流入絶対速度、W2は風と
翼の相対速度であってU2とV2のベクトル和、α2は
風の流入の遅い部分の流入角であってW2とU2とのな
す角である。
Next, regarding the blade shape shown in FIG. 4, the effect of bending the tip will be described with reference to velocity triangles shown in FIGS. 5 (a) and 5 (b). In FIG. 5 (a), U1 is the peripheral velocity of the blade 14, V1 is the absolute inflow velocity of the portion where the ventilation resistance is small and the inflow of wind is fast, and W1 is the relative velocity between the wind and the blade, which is U1 and V1.
The vector sum α1 is the inflow angle of the fast inflow portion, which is the angle formed by W1 and U1. Further, in FIG. 5B, U2 (= U1) is the peripheral velocity of the blade 14, V2 is the absolute inflow velocity of the portion where the ventilation resistance is large and the inflow of the wind is slow, and W2 is the relative velocity between the wind and the blade. The vector sum of U2 and V2, α2 is the inflow angle of the part where the inflow of the wind is slow, and is the angle formed by W2 and U2.

【0036】風の流入の速い部分とは、図3に示した熱
交換器13側(入口開口部9)において、フィン13a
を主とする後流にて図5(a)の速度三角形のように、
翼14の入口角Bb1に対して風の流入角α1を従来の
Ba1よりもδBa1だけ大きくして入りにくくし、流
入量を少なくさせる働きする。風の流入の遅い部分と
は、熱交換器のパイプ13bを主とする後流にて、図5
(b)の速度三角形のように、翼14の入口角Bb1に
対して風の流入角α2を従来のBa1よりもδBa2小
さくして入口角Bb1に近づけて入り易くし、流入量を
多くさせる働きをする。
The part where the inflow of wind is fast means the fin 13a on the heat exchanger 13 side (inlet opening 9) shown in FIG.
As shown in the velocity triangle of FIG.
The air inflow angle α1 with respect to the inlet angle Bb1 of the blade 14 is increased by δBa1 as compared with the conventional Ba1 to make it difficult to enter, and the inflow amount is reduced. The part where the flow of air is slow is the wake mainly consisting of the pipe 13b of the heat exchanger, and
As in the velocity triangle of (b), the inflow angle α2 of the wind with respect to the inlet angle Bb1 of the blade 14 is smaller than the conventional Ba1 by δBa2 to make the inlet angle Bb1 closer to the entrance, and to increase the inflow amount. do.

【0037】すなわち、翼先端の部分的前傾化は、図3
に示す熱交換器13のフィン13aを主とする後流速度
aとパイプ13bを主とする後流速度bとを平均化し、
翼14に対する流入量を平均化して翼通過時の圧力変動
および乱れ変動を少なくし、それにより、特に熱交換器
13の近接配置による干渉の回転二次音2NZの発生を
少なくする。また、平均化により回転音二次音2NZの
ほかに広い周波数帯域の翼部の流体音を低減する効果を
得ることができる。また、前ケ−シングの前縁6a部か
ら発生する自由渦12および急激な流れ込みによる翼1
4への干渉に対しても、上記熱交換器後流の場合と同様
な作用が得られ、回転一次音1NZの発生を少なくする
効果を得ることができる。また、翼14の部分的な前傾
増しは、翼はもとより羽根車としての強度を向上でき
る。
That is, the partial forward inclination of the blade tip is shown in FIG.
The wake velocity a mainly consisting of the fins 13a of the heat exchanger 13 and the wake velocity b mainly consisting of the pipe 13b are averaged,
The amount of inflow to the blades 14 is averaged to reduce pressure fluctuations and turbulence fluctuations when passing through the blades, thereby reducing the occurrence of rotating secondary sound 2NZ due to interference particularly due to the close arrangement of the heat exchanger 13. Further, by averaging, it is possible to obtain the effect of reducing the fluid sound of the wing portion in a wide frequency band in addition to the secondary sound of rotation 2NZ. In addition, the free vortex 12 generated from the front edge 6a of the front casing and the blade 1 due to a sudden inflow.
The effect similar to that in the case of the heat exchanger wake is also obtained with respect to the interference with No. 4, and the effect of reducing the generation of the rotating primary sound 1NZ can be obtained. Further, the partial increase of the forward inclination of the blade 14 can improve the strength of the impeller as well as the blade.

【0038】図4に示す実施例の翼形状のものについ
て、前述と同様に、外径90mm、軸方向長さ634m
m、翼数34枚、翼14の傾斜角度θが2.6°、ラン
ダム度δが1.43で、断面二重円弧を主とする外周側
翼先端を13°増しに前傾(前歴の26から13°に)
させた樹脂製貫流ファンを組み込み、毎分1242回転
で行ない、それを10Hzピッチで騒音分析を行なっ
た。図9は、横軸に周波数(Hz)、縦軸に音圧レベル
(dB)をとり、等曲率翼ファンのデータを実線、先端
曲げファンのデータを破線で示したものである。
As for the blade shape of the embodiment shown in FIG. 4, the outer diameter is 90 mm and the axial length is 634 m, as described above.
m, the number of blades is 34, the inclination angle θ of the blades 14 is 2.6 °, the randomness δ is 1.43, and the tip of the outer peripheral blade, which is mainly a double circular arc in section, is inclined forward by 13 ° (previous history: 26). From 13 °)
The resin-made once-through fan was installed, the rotation was performed at 1242 rpm, and the noise was analyzed at a 10 Hz pitch. FIG. 9 shows the frequency (Hz) on the horizontal axis and the sound pressure level (dB) on the vertical axis, and shows the data of the equal curvature blade fan with a solid line and the data of the tip bending fan with a broken line.

【0039】その結果、図9中に破線で示すように、特
に、回転二次音2NZのピ−クが、通常の等曲率翼の先
の実施例のファンが20dBあったのに対して、翼先端
曲げのファンは15dBと5dB低減できて、スペクト
ル上では周辺音との差がほとんど無くピ−クが無くなっ
た。また、回転二次音2NZの低下に付随して回転一次
音1NZも2dB低下した。、騒音のオ−バ−オ−ル値
では39,5dBであったものが37,5dBになり、
2dBの低減効果と聴感の良好なることを確認できた。
なお、翼の前傾により、風量は同一回転数で3%少なく
なり、しかし、回転音2NZ、1NZ以外の広い周波数
帯域にわたり流体音も低下して、同一風量で実質の効果
を比較するとオ−バ−オ−ル値で1,2dBの低減効果
を得たことになる。
As a result, as shown by the broken line in FIG. 9, in particular, the peak of the rotating secondary sound 2NZ was 20 dB in comparison with the fan of the previous embodiment of the normal equal curvature blade, whereas The fan with the blade tip bent was able to reduce it by 15 dB to 5 dB, and there was almost no difference from the ambient sound on the spectrum, and the peak disappeared. Further, accompanying the decrease in the secondary rotating sound 2NZ, the primary rotating sound 1NZ also decreased by 2 dB. , The noise over-all value was 39.5 dB instead of 39,5 dB,
It was confirmed that the reduction effect of 2 dB and the audibility were improved.
It should be noted that due to the forward inclination of the blades, the air volume is reduced by 3% at the same number of revolutions, but the fluid noise is also reduced over a wide frequency band other than the rotation noises 2NZ and 1NZ, and when comparing the actual effects with the same air volume, This means that a reduction effect of 1,2 dB in bar-hole value was obtained.

【0040】〔実施例 1−3〕図6は、第一の発明の
さらに他の実施例に係る貫流ファンの翼の拡大断面図で
ある。図6は、図1に示した貫流ファンの翼形状、翼先
端に改良を加えた実施例である。破線は従来形状を示
し、実線は本実施例の形状を示すものである。図6に示
す翼15は、樹脂成型品でよく用いられる断面がほぼ三
日月形のものであり、図4の例と同様に、先端を曲率R
b´に曲げて外周側入口角を従来のBa´より約10°
あまり小さくしてBb´にしたものである。
[Embodiment 1-3] FIG. 6 is an enlarged sectional view of a blade of a once-through fan according to still another embodiment of the first invention. FIG. 6 shows an embodiment in which the blade shape and blade tip of the cross-flow fan shown in FIG. 1 are improved. The broken line shows the conventional shape, and the solid line shows the shape of this embodiment. The blade 15 shown in FIG. 6 has a substantially crescent-shaped cross section that is often used in resin molded products, and the tip has a curvature R as in the example of FIG.
Bent to b'and the entrance angle on the outer peripheral side is about 10 ° compared to conventional Ba '
It is too small to be Bb '.

【0041】図6に示すような断面がほぼ三日月形のも
のについても、翼先端を部分的にキャンバ−ラインに沿
って曲率Rb´で余分に曲げた翼15とすることにより
図4の例と同様な効果を得ることができる。
Even in the case of a substantially crescent-shaped cross section as shown in FIG. 6, the blade tip is partially bent along the camber line with an extra curvature of Rb 'to form the blade 15 shown in FIG. Similar effects can be obtained.

【0042】〔実施例 2〕図10は、第二の発明の一
実施例に係る貫流ファンの正面図である。図10に示す
貫流ファン21は、支え円板23の外周寄りの一面に翼
22を周方向に多数配列してなる樹脂製の小羽根車21
aについて、軸方向側で開口する側の翼22の先端を他
の小羽根車21aの支え円板23の背面溝に挿入し、超
音波振動により溶着して複数個連結して横長な篭状羽根
車としたものである。ここで、個々の小羽根車21aの
翼22は軸方向平行線に対して所定の傾斜角度θを有し
ており、翼22が支え円板23を経て左端の支え円板2
3から右端の支え円板23に至り軸方向平行線に対して
所定の傾斜角度θで直線状で各翼が同一方向に向いてい
るものである。
[Embodiment 2] FIG. 10 is a front view of a cross-flow fan according to an embodiment of the second invention. The cross-flow fan 21 shown in FIG. 10 is a resin-made small impeller 21 in which a large number of blades 22 are arranged in the circumferential direction on one surface of the support disk 23 near the outer circumference.
Regarding a, the tip of the blade 22 on the side opening in the axial direction is inserted into the back groove of the supporting disk 23 of another small impeller 21a, welded by ultrasonic vibration, and a plurality of them are connected to form a horizontally elongated cage shape. It is an impeller. Here, the blades 22 of the individual small impellers 21a have a predetermined inclination angle θ with respect to the parallel lines in the axial direction, and the blades 22 pass through the support disk 23 and the support disk 2 at the left end.
3 to the supporting disc 23 at the right end, the blades are linear and are oriented in the same direction at a predetermined inclination angle θ with respect to the parallel line in the axial direction.

【0043】本実施例においては、特に成形が小羽根車
21a単位で行なえるので、小さな成形型で済む。翼2
2の傾斜成形に対しては、翼22間側に入る型を若干回
転しつつ出し入れすることにより行なえるので、容易に
成形できる利点がある。また、性能的にも、前記実施例
と同じく回転音および流体音の低減に効果が得られる。
また、翼について、翼列のランダム化、外周側先端の部
分前傾曲げにより二次回転音の低減を含めて第一の発明
の実施例と同様の効果を高めることができる。
In this embodiment, since the molding can be carried out in units of the small impeller 21a, a small molding die is sufficient. Wings 2
The inclined molding of No. 2 can be performed by slightly moving the mold that enters between the blades 22 while taking it in and out, so that there is an advantage that molding can be performed easily. Further, in terms of performance, the effect of reducing the rotation noise and the fluid noise can be obtained as in the above-mentioned embodiment.
Further, with respect to the blade, the same effects as those of the first embodiment of the invention can be enhanced including randomization of the blade row and reduction of the secondary rotation sound by partially bending the tip of the outer peripheral side forward.

【0044】なお、図10に示す実施例では、支え円板
23を経て翼22が直線状に並ぶ構成としたが、支え円
板を境に翼の位相をずらして連結しても、従来の軸方向
に平行な翼の階段状位相ずれの連結品に比較して、本実
施例ではあらかじめ翼22自身に傾斜を有しているため
に、羽根車全体において流れの相を分散する形態になっ
ている分、支え円板周りの悪影響を少なくし、流れのス
ム−ズ化と、羽根車体としての回転に伴う低周波の振動
およびその回転音を低減することができる。
In the embodiment shown in FIG. 10, the blades 22 are arranged in a straight line via the supporting discs 23. However, even if the blades are connected with the supporting discs being deviated in phase from each other, the conventional blades may be connected. In this embodiment, since the blades 22 themselves have an inclination in advance as compared with a connected product in which the blades parallel to the axial direction have a stepwise phase shift, the flow phases are dispersed in the entire impeller. As a result, it is possible to reduce adverse effects around the supporting disk, to smooth the flow, and to reduce low-frequency vibration and its rotating sound accompanying rotation of the blade body.

【0045】[0045]

【発明の効果】以上詳細に説明したように、本発明によ
れば、翼の支え円板近辺の不連続な流体音を低減し、風
量変動を少なくし、羽根車としての回転に伴う低周波数
の回転音を低減し、また、これにより周波数の高い翼数
に関係する回転一次音を主体に低減し、付随して翼数に
関する回転二次音を低減し、聴感のよい低騒音の貫流フ
ァンを提供することができる。また、本発明によれば、
上記貫流ファンを用いることにより、熱交換器の後流に
発生する回転二次音を主体に低減して製品の低騒音化と
コンパクト化をはかり、それにより、省資源化あるいは
省エネルギ−化にも貢献できる空気調和機を提供するこ
とができる。
As described in detail above, according to the present invention, the discontinuous fluid noise near the supporting disk of the blade is reduced, the air volume fluctuation is reduced, and the low frequency associated with the rotation of the impeller is reduced. This reduces the rotating sound of the fan, and mainly reduces the rotating primary sound related to the number of blades with a high frequency, and accompanying it reduces the rotating secondary sound related to the number of blades. Can be provided. Further, according to the present invention,
By using the above-mentioned cross-flow fan, the secondary noise generated in the downstream of the heat exchanger is mainly reduced to reduce the noise and the size of the product, thereby saving resources or energy. It is possible to provide an air conditioner that can also contribute.

【図面の簡単な説明】[Brief description of drawings]

【図1】第一の発明の一実施例に係る貫流ファンの正面
図である。
FIG. 1 is a front view of a cross-flow fan according to an embodiment of the first invention.

【図2】図1の羽根車のA−A矢視断面図である。FIG. 2 is a sectional view of the impeller of FIG. 1 taken along the line AA.

【図3】図1,4,6に示す貫流ファンを備えた空気調
和機の縦断面図である。
FIG. 3 is a vertical cross-sectional view of an air conditioner including the cross-flow fan shown in FIGS.

【図4】第一の発明の他の実施例に係る貫流ファンの翼
の拡大断面図である。
FIG. 4 is an enlarged sectional view of a blade of a cross-flow fan according to another embodiment of the first invention.

【図5】図4の翼への流入状況を説明する速度三角形の
図である。
FIG. 5 is a velocity triangle diagram for explaining an inflow situation into the blade of FIG. 4;

【図6】第一の発明のさらに他の実施例に係る貫流ファ
ンの翼の拡大断面図である。
FIG. 6 is an enlarged sectional view of a blade of a cross-flow fan according to still another embodiment of the first invention.

【図7】図1の実施例の貫流ファンの、翼に連続スキュ
ーをしたものの効果を示す騒音分析結果の線図である。
7 is a diagram of noise analysis results showing the effect of the blade having continuous skew in the cross-flow fan of the embodiment of FIG. 1. FIG.

【図8】図1の実施例の貫流ファンの、二重円弧の翼で
ランダムピッチにしたものの効果を示す騒音分析結果の
線図である。
FIG. 8 is a diagram of noise analysis results showing the effect of the cross-flow fan of the embodiment of FIG. 1 having a double-arc blade with a random pitch.

【図9】図4の実施例の貫流ファンの、翼先端曲げ増し
を加えた効果を示す騒音分析結果の線図である。
9 is a diagram of noise analysis results showing the effect of adding additional blade tip bending to the once-through fan of the embodiment of FIG.

【図10】第二の発明の一実施例に係る貫流ファンの正
面図である。
FIG. 10 is a front view of a cross-flow fan according to an embodiment of the second invention.

【図11】従来の貫流ファンの正面図である。FIG. 11 is a front view of a conventional cross-flow fan.

【図12】図11のB−B矢視断面図である。12 is a cross-sectional view taken along the line BB of FIG.

【図13】図11の貫流ファンを備えた従来の空気調和
機の縦断面図である。
13 is a vertical cross-sectional view of a conventional air conditioner including the cross-flow fan of FIG.

【符号の説明】[Explanation of symbols]

1…貫流ファン、2…翼、3…支え円板、4…軸、6…
前ケ−シング、7…後ケ−シング、9…入口開口部、1
0…出口開口部、13…熱交換器、13a…フィン部、
13b…パイプ部、14,15…翼。
1 ... Once-through fan, 2 ... Wing, 3 ... Supporting disc, 4 ... Shaft, 6 ...
Front casing, 7 ... Rear casing, 9 ... Entrance opening, 1
0 ... Exit opening, 13 ... Heat exchanger, 13a ... Fin portion,
13b ... pipe part, 14,15 ... wing.

Claims (13)

【特許請求の範囲】[Claims] 【請求項1】 軸方向に所定間隔に並べた複数の支え円
板の外周寄りの周方向に、多数の翼を配列してなる貫流
ファンにおいて、 前記の個々の翼を、前記複数の支え円板の一端の円板か
ら他端の円板に至る軸方向平行線に対して所定角度で同
一方向に傾斜させるとともに、 前記多数の翼は、周方向にランダムなピッチで配列した
ものであることを特徴とする貫流ファン。
1. A cross-flow fan in which a large number of blades are arranged in the circumferential direction near the outer circumference of a plurality of supporting discs arranged at predetermined intervals in the axial direction, wherein each of the individual blades is provided in the plurality of supporting circles. The plate is inclined in the same direction at a predetermined angle with respect to the parallel line in the axial direction from the disc at one end to the disc at the other end, and the multiple blades are arranged at a random pitch in the circumferential direction. A once-through fan featuring.
【請求項2】 個々の翼は、その翼の断面形状における
外周側先端を、それより内側の曲率よりわずかに強くし
た曲率で回転方向に傾けたことを特徴とする請求項1記
載の貫流ファン。
2. The cross-flow fan according to claim 1, wherein each of the blades has a tip on the outer peripheral side in the cross-sectional shape of the blade inclined in the rotational direction with a curvature slightly stronger than the curvature inside thereof. .
【請求項3】 軸方向に所定間隔に並べた複数の支え円
板の外周寄りの周方向に、多数の翼を配列してなる貫流
ファンにおいて、 前記の個々の翼を、前記複数の支え円板の一端の円板か
ら他端の円板に至る軸方向平行線に対して所定角度で同
一方向に傾斜させるとともに、 その翼の断面形状における外周側先端を、それより内側
の曲率よりわずかに強くした曲率で回転方向に傾けたこ
とを特徴とする貫流ファン。
3. A cross-flow fan in which a large number of blades are arranged in the circumferential direction near the outer circumference of a plurality of supporting discs arranged at predetermined intervals in the axial direction, wherein the individual blades are provided in the plurality of supporting circles. The blade is inclined in the same direction at a predetermined angle with respect to the parallel line in the axial direction from the disc at one end to the disc at the other end, and the tip of the blade on the outer peripheral side in the cross-sectional shape is slightly smaller than the inner curvature. A cross-flow fan characterized by being tilted in the direction of rotation with a strong curvature.
【請求項4】 軸方向に所定間隔に並べた複数の支え円
板の外周寄りの周方向に、多数の翼を配列してなる貫流
ファンにおいて、 前記多数の翼は、周方向にランダムなピッチで配列した
ものであるとともに、 その翼の断面形状における外周側先端を、それより内側
の曲率よりわずかに強くした曲率で回転方向に傾けたこ
とを特徴とする貫流ファン。
4. A cross-flow fan in which a large number of blades are arranged in the circumferential direction near the outer circumference of a plurality of support discs arranged at predetermined intervals in the axial direction, wherein the plurality of blades have a random pitch in the circumferential direction. The cross-flow fan is characterized by arranging in the above, and the tip on the outer peripheral side in the cross-sectional shape of the blade is inclined in the rotation direction with a curvature slightly stronger than the curvature inside thereof.
【請求項5】 支え円板の外周寄りの一面に、周方向に
多数の翼を配列してなる一体成形の小羽根車を、軸方向
に複数個連結してなる貫流ファンにおいて、 前記多数の翼は、支え円板を介して、その複数の支え円
板の一端の円板から他端の円板に至る軸方向平行線に対
して、所定角度で直線状ならびに同一方向に傾斜したも
のであることを特徴とする貫流ファン。
5. A cross-flow fan in which a plurality of integrally-formed small impellers, each of which has a plurality of blades arranged in the circumferential direction, are axially connected to one surface near the outer circumference of a supporting disk in the cross-flow fan. The blades are those that, through the supporting discs, are inclined linearly and in the same direction at a predetermined angle with respect to the axial parallel line extending from the disc at one end to the disc at the other end of the plurality of supporting discs. A once-through fan characterized by being present.
【請求項6】 支え円板の外周寄りの一面に、周方向に
多数の翼を配列してなる一体成形の小羽根車を、軸方向
に複数個連結してなる貫流ファンにおいて、 各々の小羽根車の多数の翼は、軸方向に対して、所定角
度で同一方向に傾斜したものであることを特徴とする貫
流ファン。
6. A cross-flow fan comprising a plurality of integrally-formed small impellers, each of which is formed by arranging a number of blades in the circumferential direction, on one surface near the outer circumference of a supporting disk in an axial direction. A cross-flow fan, characterized in that a large number of blades of the impeller are inclined in the same direction at a predetermined angle with respect to the axial direction.
【請求項7】 多数の翼は、周方向にランダムなピッチ
で配列したものであることを特徴とする請求項5または
6記載のいずれかの貫流ファン。
7. The cross-flow fan according to claim 5, wherein the plurality of blades are arranged in a circumferential direction at a random pitch.
【請求項8】 多数の翼は、その翼の断面形状における
外周側先端を、それより内側の曲率よりわずかに強くし
た曲率で回転方向に傾けたことを特徴とする請求項5ま
たは6記載のいずれかの貫流ファン。
8. The blade according to claim 5, wherein a large number of blades are inclined in a rotational direction with a curvature slightly larger than a curvature on the outer peripheral side in a cross-sectional shape of the blade. One-through fan.
【請求項9】 多数の翼は、周方向にランダムなピッチ
で配列したものであるとともに、その翼の断面形状にお
ける外周側先端を、それより内側の曲率よりわずかに強
くした曲率で回転方向に傾けたことを特徴とする請求項
5または6記載のいずれかの貫流ファン。
9. A large number of blades are arranged at a random pitch in a circumferential direction, and a tip end on an outer peripheral side in a cross-sectional shape of the blade has a curvature slightly larger than a curvature inside thereof in a rotational direction. The cross-flow fan according to claim 5, wherein the cross-flow fan is inclined.
【請求項10】 個々の翼は、羽根車の軸方向に対する
傾斜角度θを1〜4.5°としたことを特徴とする請求
項1,3,5,6記載のいずれかの貫流ファン。
10. The cross-flow fan according to claim 1, wherein each blade has an inclination angle θ of 1 to 4.5 ° with respect to the axial direction of the impeller.
【請求項11】 多数の翼は、周方向のランダム度δ
(最大ピッチ/最小ピッチ)を1.2〜1.5としたこ
とを特徴とする請求項1,4,7,9記載のいずれかの
貫流ファン。
11. A large number of blades have a circumferential randomness δ.
The cross-flow fan according to claim 1, 4, 7, or 9, wherein (maximum pitch / minimum pitch) is set to 1.2 to 1.5.
【請求項12】 翼は、羽根車の軸方向に対する傾斜角
度θを1〜4.5°とするとともに、周方向のランダム
度δ(最大ピッチ/最小ピッチ)を1.2〜1.5とし
たことを特徴とする請求項1ないし9記載のいずれかの
貫流ファン。
12. The blade has an inclination angle θ of 1 to 4.5 ° with respect to the axial direction of the impeller and a circumferential randomness δ (maximum pitch / minimum pitch) of 1.2 to 1.5. The cross-flow fan according to any one of claims 1 to 9, characterized in that.
【請求項13】 請求項1ないし12記載のいずれかの
貫流ファンを用い、その貫流ファンの入口開口部側に、
少なくとも2個所の曲げ部を有して前記貫流ファンを包
囲する断面構成のクロスフィンパイプ形熱交換器を配設
し、ケーシングに前記熱交換器に見合う位置に吸込開口
部を設けたことを特徴とする空気調和機。
13. The cross-flow fan according to claim 1, wherein the cross-flow fan is provided on the inlet opening side thereof.
A cross fin pipe type heat exchanger having a cross-sectional configuration having at least two bent portions and surrounding the cross-flow fan is disposed, and a suction opening is provided in a casing at a position corresponding to the heat exchanger. And an air conditioner.
JP7012721A 1995-01-30 1995-01-30 Cross-flow fan and air conditioner provided with it Pending JPH08200283A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7012721A JPH08200283A (en) 1995-01-30 1995-01-30 Cross-flow fan and air conditioner provided with it

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7012721A JPH08200283A (en) 1995-01-30 1995-01-30 Cross-flow fan and air conditioner provided with it

Publications (1)

Publication Number Publication Date
JPH08200283A true JPH08200283A (en) 1996-08-06

Family

ID=11813301

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7012721A Pending JPH08200283A (en) 1995-01-30 1995-01-30 Cross-flow fan and air conditioner provided with it

Country Status (1)

Country Link
JP (1) JPH08200283A (en)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002029331A1 (en) * 2000-09-29 2002-04-11 Mitsubishi Denki Kabushiki Kaisha Air conditioner
WO2004029463A1 (en) * 2002-09-24 2004-04-08 Toshiba Carrier Corporation Cross flow fan and air conditioner with the fan
KR20040042933A (en) * 2002-11-14 2004-05-22 엘지전자 주식회사 Blade structure of sirocco fan impeller
KR100459179B1 (en) * 2002-04-16 2004-12-03 엘지전자 주식회사 cross-flow fan
EP1632725A1 (en) * 2004-03-25 2006-03-08 Mitsubishi Denki Kabushiki Kaisha Air conditioner
WO2007063768A1 (en) * 2005-11-29 2007-06-07 Ishikawajima-Harima Heavy Industries Co., Ltd. Cascade of stator vane of turbo fluid machine
JP2007292405A (en) * 2006-04-26 2007-11-08 Mitsubishi Electric Corp Air conditioner
JP2008274961A (en) * 2001-05-11 2008-11-13 Snecma Structure with rotor and fixed turbulence source, and method of reducing vibration of structure
JP2012007473A (en) * 2010-06-22 2012-01-12 Panasonic Corp Cross-flow fan and air conditioner equipped with the cross-flow fan
US8814522B2 (en) 2007-06-15 2014-08-26 Cymer, Llc Cross-flow fan impeller for a transversley excited, pulsed, gas discharge laser
CN104589015A (en) * 2014-11-21 2015-05-06 余姚天超通风设备有限公司 Automatic central disc separation device for assembling of cross-flow fan impeller
JP2017215563A (en) * 2016-01-06 2017-12-07 パナソニックIpマネジメント株式会社 Cooling unit and projection-type image display device
US11384765B2 (en) 2017-09-27 2022-07-12 Daikin Industries, Ltd. Air conditioner

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2002029331A1 (en) * 2000-09-29 2002-04-11 Mitsubishi Denki Kabushiki Kaisha Air conditioner
AU767078B2 (en) * 2000-09-29 2003-10-30 Mitsubishi Denki Kabushiki Kaisha Air conditioner
US6692223B2 (en) 2000-09-29 2004-02-17 Mitsubishi Denki Kabushiki Kaisha Air conditioner
JP2008274961A (en) * 2001-05-11 2008-11-13 Snecma Structure with rotor and fixed turbulence source, and method of reducing vibration of structure
KR100459179B1 (en) * 2002-04-16 2004-12-03 엘지전자 주식회사 cross-flow fan
WO2004029463A1 (en) * 2002-09-24 2004-04-08 Toshiba Carrier Corporation Cross flow fan and air conditioner with the fan
KR20040042933A (en) * 2002-11-14 2004-05-22 엘지전자 주식회사 Blade structure of sirocco fan impeller
EP1632725A1 (en) * 2004-03-25 2006-03-08 Mitsubishi Denki Kabushiki Kaisha Air conditioner
US7673671B2 (en) 2004-03-25 2010-03-09 Mitsubishi Denki Kabushiki Kaisha Air conditioner
EP1632725A4 (en) * 2004-03-25 2007-11-28 Mitsubishi Electric Corp Air conditioner
US7891943B2 (en) 2005-11-29 2011-02-22 Ishikawajima-Harima Heavy Industries, Co. Ltd. Stator cascade of turbo type fluid machine
JPWO2007063768A1 (en) * 2005-11-29 2009-05-07 株式会社Ihi Stator blade row of turbo fluid machine
WO2007063768A1 (en) * 2005-11-29 2007-06-07 Ishikawajima-Harima Heavy Industries Co., Ltd. Cascade of stator vane of turbo fluid machine
JP4678406B2 (en) * 2005-11-29 2011-04-27 株式会社Ihi Stator blade row of turbo fluid machine
JP2007292405A (en) * 2006-04-26 2007-11-08 Mitsubishi Electric Corp Air conditioner
JP4678327B2 (en) * 2006-04-26 2011-04-27 三菱電機株式会社 Air conditioner
US8814522B2 (en) 2007-06-15 2014-08-26 Cymer, Llc Cross-flow fan impeller for a transversley excited, pulsed, gas discharge laser
JP2012007473A (en) * 2010-06-22 2012-01-12 Panasonic Corp Cross-flow fan and air conditioner equipped with the cross-flow fan
CN104589015A (en) * 2014-11-21 2015-05-06 余姚天超通风设备有限公司 Automatic central disc separation device for assembling of cross-flow fan impeller
JP2017215563A (en) * 2016-01-06 2017-12-07 パナソニックIpマネジメント株式会社 Cooling unit and projection-type image display device
US11384765B2 (en) 2017-09-27 2022-07-12 Daikin Industries, Ltd. Air conditioner

Similar Documents

Publication Publication Date Title
EP1979623B1 (en) Improved impeller and fan
KR100937929B1 (en) Stator of Axial flow fan shroud
JP5097201B2 (en) Axial fan assembly
EP2230407B1 (en) Propeller fan
US6027307A (en) Fan and shroud assembly adopting the fan
US4184804A (en) Rotary electric machine having a cooling fan
EP1624193A1 (en) Multi-vane centrifugal blower
JP3507758B2 (en) Multi-wing fan
JPH08200283A (en) Cross-flow fan and air conditioner provided with it
JP2000240590A (en) Multiblade forward fan
EP2006610B1 (en) Unit for treating air with controlled flow
KR20040078934A (en) Axial Flow Fan
JP3516909B2 (en) Centrifugal blower
JP4697132B2 (en) Air conditioner
JP3918207B2 (en) Air conditioner
JP3137897B2 (en) Once-through fan
JP2003184792A (en) Blower
JPH01193099A (en) Impeller of centrifugal flower
KR100669917B1 (en) Assembly of fan and shroud
JP2001280288A (en) Impeller structure of multiblade blower
JP2978150B2 (en) Air conditioner indoor unit
JPH0742692A (en) Cross flow fan and air conditioner using this fan
CN113027815B (en) Impeller comprising partial stepped blades and design method thereof
JP3315840B2 (en) Centrifugal blower and refrigerator centrifugal blower
JP3520017B2 (en) Cross flow fan