JPH08200291A - Impeller for cross flow blower - Google Patents

Impeller for cross flow blower

Info

Publication number
JPH08200291A
JPH08200291A JP1274395A JP1274395A JPH08200291A JP H08200291 A JPH08200291 A JP H08200291A JP 1274395 A JP1274395 A JP 1274395A JP 1274395 A JP1274395 A JP 1274395A JP H08200291 A JPH08200291 A JP H08200291A
Authority
JP
Japan
Prior art keywords
blade
blower
impeller
cross
axial direction
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
Application number
JP1274395A
Other languages
Japanese (ja)
Other versions
JP3504363B2 (en
Inventor
Atsushi Yoshihashi
淳 吉橋
Masayuki Oishi
雅之 大石
Katsuyuki Aoki
克之 青木
Teru Takamori
輝 高守
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.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
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 Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP01274395A priority Critical patent/JP3504363B2/en
Publication of JPH08200291A publication Critical patent/JPH08200291A/en
Application granted granted Critical
Publication of JP3504363B2 publication Critical patent/JP3504363B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

PURPOSE: To improve efficiency and to reduce noise by suppressing an acceleration rate as small as possible at passing time between blades, and decreasing a dynamic friction loss. CONSTITUTION: Relating to an impeller for a cross flow blower, it has a partitioning plate arranged with a prescribed space in a blower axial direction and a blade 1 positioned between these partitioning plates to direct a lengthwise direction in the blower axial direction also to be arranged in a peripheral direction with a prescribed space apart in the vicinity of a peripheral end of the partitioning plate. Accordingly, the blade 1 is formed in a blade shape where its maximum warped position agrees with the center of a blade chord, also a thickness (2Ya ) of the maximum warped position of the blade 1 and a length (t) of a circular arc, connecting between middle points of a circular arc-shaped neutral line of the blades 1 adjacent to each other by the circular are with a blower axis serving as the center, satisfy a relation where 0.1178<=2Ya /t<=0.1330.

Description

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

【0001】[0001]

【産業上の利用分野】この発明は、空気調和機等に用い
られる横断流送風機(クロスフローファン)の羽根車に
関するものである。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an impeller of a cross flow fan (cross flow fan) used in an air conditioner or the like.

【0002】[0002]

【従来の技術】図4は例えば実開昭63−54892号
公報に示された従来の横断流送風機の羽根車の要部拡大
断面図である。図において、1は羽根車の軸方向に所定
間隔で設けられた仕切板(図示せず)の間に周方向に多
数配された羽根、9は羽根車の外周、10は羽根車の外
周、15は隣り合う羽根1の間に形成された羽根間流路
である。
2. Description of the Related Art FIG. 4 is an enlarged cross-sectional view of an essential part of an impeller of a conventional cross flow fan disclosed in, for example, Japanese Utility Model Laid-Open No. 63-54892. In the figure, 1 is a blade arranged in a large number in the circumferential direction between partition plates (not shown) provided at predetermined intervals in the axial direction of the impeller, 9 is the outer circumference of the impeller, 10 is the outer circumference of the impeller, Reference numeral 15 is an inter-blade flow path formed between the adjacent blades 1.

【0003】次に動作について説明する。羽根車の羽根
1を内周10から外周9近傍にかけて羽根間流路15の
断面積が等しくなるように徐々に肉厚にし、その後外周
10にかけて徐々に肉薄にして羽根1の後方及び羽根間
流路15内での負圧領域を少なくして、空気が流路を通
過する際及び通過した直後に渦流の発生を抑え、渦流に
よる風圧の損失を少なくして送風機の効率を改善するよ
うにしている。
Next, the operation will be described. The blade 1 of the impeller is gradually thickened from the inner circumference 10 to the vicinity of the outer circumference 9 so that the cross-sectional area of the inter-blade flow path 15 becomes equal, and then gradually thinned toward the outer circumference 10 to the rear of the blade 1 and the inter-blade flow. By reducing the negative pressure region in the passage 15 to suppress the generation of a vortex when the air passes through the flow passage and immediately after the passage, the loss of wind pressure due to the vortex is reduced and the efficiency of the blower is improved. There is.

【0004】[0004]

【発明が解決しようとする課題】従来の横断流送風機の
羽根車は以上のように構成されているので、送風機の性
能を高めるために、例えば羽根車の直径を大きくすると
か、又羽根1の翼弦長を長くする場合、羽根1の肉厚部
が厚くなりすぎて、羽根車が重くなり運転時振動を発生
するという問題点があった。
Since the impeller of the conventional cross flow fan is constructed as described above, in order to improve the performance of the blower, for example, the diameter of the impeller is increased or the impeller of the impeller 1 is increased. When the chord length is increased, there is a problem in that the thick portion of the blade 1 becomes too thick and the impeller becomes heavy, which causes vibration during operation.

【0005】この発明は上記のような問題点を解消する
ためになされたもので、羽根車を軽量化できると共に、
低騒音かつ高静圧タイプの横断流送風機の羽根車を提供
することを目的とする。
The present invention has been made in order to solve the above problems, and can reduce the weight of the impeller and
An object is to provide an impeller of a low noise and high static pressure type cross-flow blower.

【0006】[0006]

【課題を解決するための手段】請求項1の横断流送風機
の羽根車は、送風機軸方向に所定間隔あけて配設された
仕切板と、この仕切板間に位置し長手方向が送風機軸方
向に向くと共に仕切板の外周端近傍に所定間隔おきに周
方向に配設された羽根とを有する横断流送風機の羽根車
において、羽根は最大反り位置が羽根弦の中心に一致す
る翼形状とすると共に、羽根の最大反り位置の肉厚(2
a )及び隣り合う羽根の円弧状の中立線の中点間を送
風機軸を中心に円弧で結んだ円弧の長さ(t)とが、
0.1178≦2Ya /t≦0.1330の関係を満た
すことを特徴とする。
According to another aspect of the present invention, there is provided an impeller of a cross-flow fan, comprising partition plates arranged at a predetermined interval in the axial direction of the blower, and a longitudinal direction located between the partition plates. In the impeller of a cross-flow fan, which has a vane arranged in the circumferential direction at predetermined intervals in the vicinity of the outer peripheral edge of the partition plate, the vane has a blade shape in which the maximum warp position coincides with the center of the chord chord. At the same time, the thickness (2
Y a ) and the length (t) of the arc connecting the midpoints of the arc-shaped neutral lines of the adjacent blades with an arc centered on the blower axis,
It is characterized in that the relationship of 0.1178 ≦ 2Y a /t≦0.1330 is satisfied.

【0007】請求項2の横断流送風機の羽根車は、送風
機軸方向に所定間隔あけて配設された仕切板と、この仕
切板間に位置し長手方向が送風機軸方向に向くと共に仕
切板の外周端近傍に所定間隔おきに周方向に配設された
羽根とを有する横断流送風機の羽根車において、羽根は
最大反り位置が該羽根弦の中心に一致する翼形状とし、
羽根の外周側端縁部を形成する円の半径(RA )と羽根
の最大反り位置の肉厚半分(Ya )とが、0.5646
≦RA /Ya ≦0.6860の関係を満たし、同時に羽
根の内周側端縁部を形成する円の半径(RB )と羽根の
最大反り位置の肉厚の半分(Ya )とが、0.5646
≦RB /Ya ≦0.6860の関係を満たすことを特徴
とする。
According to another aspect of the present invention, there is provided an impeller of a cross flow fan, comprising partition plates arranged at a predetermined interval in the axial direction of the blower, and a partition plate located between the partition plates and having a longitudinal direction oriented in the axial direction of the blower. In an impeller of a cross-flow blower having a blade arranged in the circumferential direction at predetermined intervals in the vicinity of the outer peripheral end, the blade has a blade shape in which the maximum warp position matches the center of the blade chord,
The radius (R A ) of the circle forming the outer peripheral edge of the blade and the half thickness (Y a ) of the maximum warp position of the blade are 0.5646.
≦ R A / Y satisfies the a ≦ .6860 relationship, at the same time the radius of the circle forming the inner peripheral side edge portion of the blade (R B) and the thickness of the half of the maximum warpage position of the blade and (Y a) But 0.5646
≦ characterized by satisfying the relation of R B / Y a ≦ 0.6860.

【0008】[0008]

【作用】請求項1の横断流送風機の羽根車は、翼間通過
時は増速率を極力抑え込み動摩擦損失が減少する。
In the impeller of the cross flow fan according to the first aspect, the speed increase rate is suppressed as much as possible when passing between the blades, and the dynamic friction loss is reduced.

【0009】請求項2の横断流送風機の羽根車は、翼間
通過時の仕事量及び効率が最適化される。
In the impeller of the cross flow fan according to the second aspect, the work amount and the efficiency when passing between the blades are optimized.

【0010】[0010]

【実施例】【Example】

実施例1.以下、この発明の実施例1を図について説明
する。図1はこの発明の実施例1による横断流送風機の
羽根車の要部拡大断面図である。図において、1は送風
機の軸方向に所定間隔あけて配設された仕切板(図示せ
ず)の間に周方向に多数設けられた羽根(翼)、3は流
れが直接当たる面である圧力面、4は流れが直接当たら
ない負圧面、5は羽根1の前縁、6は羽根1の後縁、7
は羽根1の最大反り位置の肉厚(2Ya )、8は隣り合
う羽根間の最大反り位置での円弧長さであるピッチ
(t)、9は羽根車の外周、10は羽根車の内周、11
は羽根1の反り線である。そして肉厚(2Ya )と羽根
間ピッチ(t)は0.1178≦2Ya /t≦0.13
30の関係を満たす配置とする。
Example 1. Embodiment 1 of the present invention will be described below with reference to the drawings. 1 is an enlarged sectional view of an essential part of an impeller of a cross flow fan according to a first embodiment of the present invention. In the figure, 1 is a number of blades (blades) provided in the circumferential direction between partition plates (not shown) arranged at predetermined intervals in the axial direction of the blower, and 3 is a pressure which is a surface directly contacted with the flow. Surface 4 is a suction surface where the flow does not directly contact, 5 is the leading edge of blade 1, 6 is the trailing edge of blade 1, 7
Is the wall thickness of the blade 1 at the maximum warp position (2Y a ), 8 is the pitch (t) which is the arc length at the maximum warp position between adjacent blades, 9 is the outer circumference of the impeller, and 10 is the inside of the impeller. Zhou, 11
Is a warp line of the blade 1. The wall thickness (2Y a ) and the blade pitch (t) are 0.1178 ≦ 2Y a /t≦0.13.
The arrangement satisfies the relationship of 30.

【0011】翼1をより翼型にすると、翼の最大そり位
置7の肉厚部から翼の後縁6にかけての静圧上昇に比
べ、翼の前縁5から翼の最大そり位置7の肉厚部までの
翼間流速の増加による損失が大きくなる値0.1178
から同一風量時での翼間流速が遅くなり、翼の負圧面4
から流れがはがれ損失を大きくする値0.1330の範
囲内に翼間のピッチ8と翼の最大そり位置7の肉厚の比
t/2Ya が配置されることにより、翼間通過時は増速
率を極力抑え込み動摩擦損失を減らし、効率が良く、低
騒音の横断流送風機を実現している。
When the blade 1 is made to have a more airfoil shape, compared with the static pressure increase from the thick portion of the blade at the maximum sled position 7 to the trailing edge 6 of the blade, the thickness of the blade from the leading edge 5 to the blade maximum sled position 7 is increased. Value that increases loss due to increase in blade-to-blade flow velocity up to the thick part 0.1178
From the above, the flow velocity between blades at the same air flow becomes slower and the suction surface 4
The flow ratio between the blades 8 and the wall thickness ratio t / 2Y a at the maximum warp position 7 of the blades are arranged within the range of 0.1330 that increases the flow separation loss and increases the loss when passing between the blades. The speed factor is suppressed as much as possible to reduce the dynamic friction loss, and a highly efficient and low noise cross flow fan is realized.

【0012】この実施例における横断流送風機は、羽根
車の翼1を最大そり位置が翼弦の中心になることによ
り、図2に示す様に横断流送風機特有の、一回目翼間を
通過する際の流れ方向(外周側から内周側へ)と、二回
目翼間を通過する流れ方向(内周側から外周側へ)が逆
転するという現象において双方の仕事量及び効率、一回
目翼間通過時には減速流れ状態とし、静圧上昇させ、揚
力として得た運動エネルギーを図2に示す流れを支配す
る渦21に供給、二回目翼間通過時は、増速率を極力抑
え込み動摩擦損失を減らす。さらに、断面の円弧上の中
立線の中点と隣接翼の同様の中点をファン軸を中心に円
弧で線んだ長さと翼の最大そり位置の肉厚との比を最適
化し、上述の一回目翼間通過時、並びに二回目翼間通過
時の仕事量及び効率の最適化が達成される。
In the cross flow blower in this embodiment, the blade 1 of the impeller passes between the first blades peculiar to the cross flow blower as shown in FIG. 2 because the maximum sled position is at the center of the chord. In the phenomenon that the flow direction at the time (outer peripheral side to the inner peripheral side) and the flow direction passing between the second blades (from the inner peripheral side to the outer peripheral side) are reversed, both work and efficiency, between the first blades At the time of passage, the flow is in a decelerated state, the static pressure is increased, and the kinetic energy obtained as a lift is supplied to the vortex 21 that governs the flow shown in FIG. Furthermore, by optimizing the ratio between the length of the midpoint of the neutral line on the circular arc of the cross section and the similar midpoint of the adjacent blades in the circular arc centered on the fan axis and the thickness of the maximum warp position of the blade, Optimization of work and efficiency during the first blade-to-blade passage as well as the second blade-to-blade passage is achieved.

【0013】実施例2.以下、この発明の実施例2を図
について説明する。図3はこの発明の実施例2による横
断流送風機の羽根車の要部拡大断面である。図におい
て、符号1〜11(2,8を除く)は図1と全く同一の
ものである。RA は羽根1の外周側端縁部を形成する円
の半径、RB は内周側端縁部を形成する円の半径であ
る。
Example 2. Embodiment 2 of the present invention will be described below with reference to the drawings. FIG. 3 is an enlarged cross-sectional view of a main part of an impeller of a cross flow fan according to a second embodiment of the present invention. In the figure, reference numerals 1 to 11 (excluding 2 and 8) are exactly the same as those in FIG. R A is a circle forming the outer peripheral side edge portion of the blade 1 radius, R B is the radius of the circle forming the inner peripheral side edge portions.

【0014】翼1の前縁5で剥離を発生し、回転音が大
きくなる値、或いは、翼1の最大そり位置7の肉厚部か
ら翼1の後縁6へかけて、翼間流速の減速が大き過ぎる
為、翼の負圧面4から流れが剥れ損失が大きくなる値
0.546から翼1を翼形にする事による効果が小さく
なる値、或いは、翼間流速が減少する値0.686の範
囲内に翼1の外周端縁の円の半径RA と翼1の最大そり
位置7の肉厚の半分の比RA /Ya 、及び翼1の内周端
縁の円の半径RB と翼1の最大そり位置7の肉厚の半分
の比RB /Ya が配置されることにより、翼間通過時の
仕事量及び効率の最適化が達成され、効率が良く、低騒
音の横断流送風機を実現している。
A value at which separation noise occurs at the leading edge 5 of the blade 1 and the rotation noise increases, or the blade-to-blade flow velocity changes from the thick portion at the maximum warp position 7 of the blade 1 to the trailing edge 6 of the blade Since the deceleration is too large, the flow separation from the suction surface 4 of the blade becomes large, and the loss becomes large. The ratio of the radius R A of the circle of the outer peripheral edge of the blade 1 to the half of the wall thickness of the maximum sled position 7 of the blade 1 R A / Y a within the range of .686, and the circle of the inner peripheral edge of the blade 1 By arranging the radius R B and the ratio R B / Y a that is half the wall thickness of the maximum warp position 7 of the blade 1, optimization of the work amount and efficiency when passing between the blades is achieved, and the efficiency is good, It realizes a low-noise cross-flow blower.

【0015】[0015]

【発明の効果】請求項1の横断流送風機の羽根車は、送
風機軸方向に所定間隔あけて配設された仕切板と、この
仕切板間に位置し長手方向が送風機軸方向に向くと共に
仕切板の外周端近傍に所定間隔おきに周方向に配設され
た羽根とを有する横断流送風機の羽根車において、羽根
は最大反り位置が羽根弦の中心に一致する翼形状とする
と共に、羽根の最大反り位置の肉厚(2Ya )及び隣り
合う羽根の円弧状の中立線の中点間を送風機軸を中心に
円弧で結んだ円弧の長さ(t)とが、0.1178≦2
a /t≦0.1330の関係を満たす構成にしたの
で、翼間通過時は増速率を極力抑え込み動摩擦損失が減
少することにより、効率が良く低騒音になる。
The impeller of the cross-flow fan according to the first aspect of the present invention includes partition plates arranged at a predetermined interval in the axial direction of the blower, and the partition plates located between the partition plates and having the longitudinal direction oriented in the axial direction of the blower. In an impeller of a cross-flow fan having blades arranged in the circumferential direction at predetermined intervals in the vicinity of the outer peripheral edge of the plate, the blade has a blade shape whose maximum warp position matches the center of the blade chord, and The thickness (2Y a ) at the maximum warp position and the length (t) of the arc connecting the midpoints of the arc-shaped neutral lines of the adjacent blades with the arc of the blower axis as a center are 0.1178 ≦ 2
Since a configuration which satisfies the relationship of Y a /t≦0.1330, by the time of the inter-blade passage is as much as possible Osaekomi dynamic friction losses speed increasing ratio is reduced, efficient becomes low noise.

【0016】請求項2の横断流送風機の羽根車は、送風
機軸方向に所定間隔あけて配設された仕切板と、この仕
切板間に位置し長手方向が送風機軸方向に向くと共に仕
切板の外周端近傍に所定間隔おきに周方向に配設された
羽根とを有する横断流送風機の羽根車において、羽根は
最大反り位置が該羽根弦の中心に一致する翼形状とし、
羽根の外周側端縁部を形成する円の半径(RA )と羽根
の最大反り位置の肉厚半分(Ya )とが、0.5646
≦RA /Ya ≦0.6860の関係を満たし、同時に羽
根の内周側端縁部を形成する円の半径(RB )と羽根の
最大反り位置の肉厚の半分(Ya )とが、0.5646
≦RB /Ya ≦0.6860の関係を満たす構成にした
ので、翼間通過時の仕事量及び効率が最適化され、効率
が良く低騒音になる。
An impeller of a cross flow fan according to a second aspect of the present invention is a partition plate which is disposed at a predetermined interval in the axial direction of the blower, and a partition plate which is located between the partition plates and whose longitudinal direction is oriented in the axial direction of the blower. In an impeller of a cross-flow blower having a blade arranged in the circumferential direction at predetermined intervals in the vicinity of the outer peripheral end, the blade has a blade shape in which the maximum warp position matches the center of the blade chord,
The radius (R A ) of the circle forming the outer peripheral edge of the blade and the half thickness (Y a ) of the maximum warp position of the blade are 0.5646.
≦ R A / Y satisfies the a ≦ .6860 relationship, at the same time the radius of the circle forming the inner peripheral side edge portion of the blade (R B) and the thickness of the half of the maximum warpage position of the blade and (Y a) But 0.5646
Since ≦ R B / Y was satisfied the relationship structure of a ≦ 0.6860, it is optimized workload and efficiency at between blades pass, efficient becomes low noise.

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

【図1】 この発明の実施例1による横断流送風機の羽
根車の要部拡大断面図である。
FIG. 1 is an enlarged sectional view of essential parts of an impeller of a cross flow fan according to a first embodiment of the present invention.

【図2】 この発明の実施例1による横断流送風機の羽
根車の動作を説明する図である。
FIG. 2 is a diagram illustrating the operation of the impeller of the cross flow fan according to the first embodiment of the present invention.

【図3】 この発明の実施例2による横断流送風機の羽
根車の要部拡大断面図である。
FIG. 3 is an enlarged sectional view of a main part of an impeller of a cross flow fan according to a second embodiment of the present invention.

【図4】 従来の横断流送風機の羽根車の要部拡大断面
図である。
FIG. 4 is an enlarged cross-sectional view of a main part of a conventional impeller of a cross flow fan.

【符号の説明】[Explanation of symbols]

1 羽根(翼)、7 羽根の最大反り位置の肉厚(2Y
a )、8 羽根の最大反り位置での羽根間ピッチ、RA
羽根の前縁部の半径、RB 羽根の後縁部の半径。
1 blade (blade), 7 blade maximum warp position wall thickness (2Y
a ), 8 blade pitch at maximum warp position, RA
The radius of leading edge of the blade, the radius of the trailing edge of the R B blade.

───────────────────────────────────────────────────── フロントページの続き (72)発明者 高守 輝 静岡市小鹿三丁目18番1号 三菱電機株式 会社静岡製作所内 ─────────────────────────────────────────────────── ─── Continuation of the front page (72) Inventor Teru Takamori 3-18-1, Oga, Shizuoka City Mitsubishi Electric Corporation Shizuoka Factory

Claims (2)

【特許請求の範囲】[Claims] 【請求項1】 送風機軸方向に所定間隔あけて配設され
た仕切板と、この仕切板間に位置し、長手方向が前記送
風機軸方向に向くと共に前記仕切板の外周端近傍に所定
間隔おきに周方向に配設された羽根とを有する横断流送
風機の羽根車において、前記羽根は最大反り位置が該羽
根弦の中心に一致する翼形状とすると共に、該羽根の最
大反り位置の肉厚(2Ya )及び隣り合う羽根の円弧状
の中立線の中点間を前記送風機軸を中心に円弧で結んだ
該円弧の長さ(t)とが、0.1178≦2Ya /t≦
0.1330の関係を満たすことを特徴とする横断流送
風機の羽根車。
1. A partition plate arranged at a predetermined interval in the axial direction of the blower, and a partition plate located between the partition plates, the longitudinal direction of which is in the axial direction of the blower, and a predetermined interval near the outer peripheral end of the partition plate. In the impeller of a cross-flow fan having a blade arranged in the circumferential direction, the blade has a blade shape in which the maximum warp position matches the center of the blade chord, and the wall thickness of the maximum warp position of the blade is (2Y a ) and the length (t) of the arc connecting the midpoints of the arc-shaped neutral lines of the adjacent blades with the arc of the blower axis as the center, 0.1178 ≦ 2Y a / t ≦
An impeller of a cross-flow fan, which satisfies the relationship of 0.1330.
【請求項2】 送風機軸方向に所定間隔あけて配設され
た仕切板と、この仕切板間に位置し、長手方向が前記送
風機軸方向に向くと共に前記仕切板の外周端近傍に所定
間隔おきに周方向に配設された羽根とを有する横断流送
風機の羽根車において、前記羽根は最大反り位置が該羽
根弦の中心に一致する翼形状とし、前記羽根の外周側縁
端部を形成する円の半径(RA )と前記羽根の最大反り
位置の肉厚半分(Ya )とが、0.5646≦RA /Y
a ≦0.6860の関係を満たし、同時に前記羽根の内
周側端縁部を形成する円の半径(RB )と前記羽根の最
大反り位置の肉厚の半分(Ya )とが、0.5646≦
B /Ya ≦0.6860の関係を満たすことを特徴と
する横断流送風機の羽根車。
2. A partition plate disposed at a predetermined interval in the blower axial direction, and a partition plate located between the partition plates, the longitudinal direction being oriented in the blower axial direction, and a predetermined interval near the outer peripheral end of the partition plate. In an impeller of a cross-flow fan having a blade arranged in the circumferential direction, the blade has a blade shape whose maximum warp position coincides with the center of the blade chord, and forms an outer peripheral edge portion of the blade. The radius (R A ) of the circle and the half thickness (Y a ) at the maximum warp position of the blade are 0.5646 ≦ R A / Y
satisfy the relationship of a ≦ .6860, the inner circumference of a circle to form a side edge portion radius of the blade (R B) and the maximum warpage position of the thickness of half of the vane and (Y a) but at the same time, 0 0.5646 ≦
An impeller of a cross flow blower, which satisfies the relationship of R B / Y a ≦ 0.6860.
JP01274395A 1995-01-30 1995-01-30 Cross-flow blower impeller Expired - Fee Related JP3504363B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP01274395A JP3504363B2 (en) 1995-01-30 1995-01-30 Cross-flow blower impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP01274395A JP3504363B2 (en) 1995-01-30 1995-01-30 Cross-flow blower impeller

Publications (2)

Publication Number Publication Date
JPH08200291A true JPH08200291A (en) 1996-08-06
JP3504363B2 JP3504363B2 (en) 2004-03-08

Family

ID=11813910

Family Applications (1)

Application Number Title Priority Date Filing Date
JP01274395A Expired - Fee Related JP3504363B2 (en) 1995-01-30 1995-01-30 Cross-flow blower impeller

Country Status (1)

Country Link
JP (1) JP3504363B2 (en)

Cited By (4)

* 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
JP2006037839A (en) * 2004-07-27 2006-02-09 Toshiba Kyaria Kk Cross flow fan
WO2015098689A1 (en) * 2013-12-27 2015-07-02 ダイキン工業株式会社 Cross-flow fan blade
WO2020143153A1 (en) * 2019-01-08 2020-07-16 广东美的制冷设备有限公司 Cross-flow wind wheel and air conditioner

Cited By (6)

* 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
JP2006037839A (en) * 2004-07-27 2006-02-09 Toshiba Kyaria Kk Cross flow fan
JP4583095B2 (en) * 2004-07-27 2010-11-17 東芝キヤリア株式会社 Cross flow fan
WO2015098689A1 (en) * 2013-12-27 2015-07-02 ダイキン工業株式会社 Cross-flow fan blade
CN105849417A (en) * 2013-12-27 2016-08-10 大金工业株式会社 Cross-flow fan blade
WO2020143153A1 (en) * 2019-01-08 2020-07-16 广东美的制冷设备有限公司 Cross-flow wind wheel and air conditioner

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