JP2000145685A - Centrifugal blower - Google Patents

Centrifugal blower

Info

Publication number
JP2000145685A
JP2000145685A JP10322061A JP32206198A JP2000145685A JP 2000145685 A JP2000145685 A JP 2000145685A JP 10322061 A JP10322061 A JP 10322061A JP 32206198 A JP32206198 A JP 32206198A JP 2000145685 A JP2000145685 A JP 2000145685A
Authority
JP
Japan
Prior art keywords
impeller
side plate
blade
blades
centrifugal blower
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
JP10322061A
Other languages
Japanese (ja)
Other versions
JP3830287B2 (en
Inventor
Muneyuki Kawase
宗之 河瀬
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.)
Kubota Corp
Original Assignee
Kubota 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 Kubota Corp filed Critical Kubota Corp
Priority to JP32206198A priority Critical patent/JP3830287B2/en
Publication of JP2000145685A publication Critical patent/JP2000145685A/en
Application granted granted Critical
Publication of JP3830287B2 publication Critical patent/JP3830287B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Abstract

PROBLEM TO BE SOLVED: To improve blowing performance of a centrifugal blower mounted with blades in the cantilevered supporting state. SOLUTION: In a centrifugal blower in which many blades 41, 42 are juxtaposedly arranged supporting in the rotational circumferential direction in the cantilevered supporting state in relation to an impeller side plate 40, the outer end edges 41a, 42a of the blades 41, 42 in the rotational radial direction are so formed in an inclined attitude that the blade free ends on the opposite sides to the supporting sides to the impeller side plate 40 may be closer to the rotational axis p.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は遠心送風機に関し、
詳しくは、多数の羽根を羽根車側板に対する片持ち支持
状態で回転周方向に並設して羽根車を形成してある遠心
送風機、及び、回転軸芯近くから羽根車側板の外周部に
わたる主羽根の多数を、羽根車側板に対する片持ち支持
状態で回転周方向に並設するとともに、羽根車側板の外
周部にのみ位置する補助羽根を、羽根車側板に対する片
持ち支持状態で主羽根どうしの間に設けて羽根車を形成
してある遠心送風機に関する。
The present invention relates to a centrifugal blower,
More specifically, a centrifugal blower in which a number of blades are arranged side by side in the rotating circumferential direction in a cantilevered state with respect to the impeller side plate to form an impeller, and a main blade extending from near the rotation axis to the outer peripheral portion of the impeller side plate Are arranged side by side in the rotating circumferential direction in a cantilevered state with respect to the impeller side plate, and auxiliary blades located only on the outer peripheral portion of the impeller side plate are arranged between the main blades in a cantilevered state with respect to the impeller side plate. And a centrifugal blower having an impeller formed therein.

【0002】[0002]

【従来の技術】従来、この種の遠心送風機では、各羽根
を2枚の羽根車側板どうしの間にわたらせて両持ち支持
状態に設ける形式のものと同様、図18に示す如く、回
転半径方向における各羽根41,42の外側端縁41
a,42aを回転軸芯Pと平行な姿勢の端縁にし、ま
た、羽根車29を内装するケーシング31のうち、回転
半径方向において各羽根41,42の外側端縁41a,
42aに対向するケーシング内周面31aも回転軸芯P
と平行な姿勢の面にし、これにより、各羽根41,42
の外側端縁41a,42aとそれに対向するケーシング
内周面31aとの間に、回転軸芯方向で幅が一定のクリ
アランスを確保するようにしていた。
2. Description of the Related Art Conventionally, this type of centrifugal blower has a rotating radial direction as shown in FIG. 18 similarly to a centrifugal blower in which each blade is provided between two impeller side plates in a double-supported state. Outer edge 41 of each blade 41, 42 at
a and 42a are edges in a posture parallel to the rotation axis P, and the outer edges 41a and 42a of the respective blades 41 and 42 in the radial direction of rotation of the casing 31 in which the impeller 29 is installed.
The inner circumferential surface 31a of the casing opposing the rotating shaft core 42a
, So that each of the blades 41, 42
Between the outer edges 41a and 42a and the inner peripheral surface 31a of the casing facing the outer edges 41a and 42a.

【0003】[0003]

【発明が解決しようとする課題】しかし、この種の遠心
送風機は、各羽根41,42を両持ち支持状態に設ける
形式に比べ、羽根車側板40が1枚で済むことから製作
面及びコスト面で有利であり、また、羽根車29を軽量
化し得ることで必要動力を低減し得るメリットもある
が、羽根41,42が片持ち支持状態であることから、
羽根車29の回転において遠心力や気体抵抗で羽根車側
板40や羽根自身41,42が撓んで、片持ち支持状態
の羽根41,42の遊端部(詳しくは、羽根車側板40
に対する支持側とは反対側の羽根遊端縁41b,42b
と回転半径方向における羽根外側端縁41a,42aと
の交差箇所近傍部分)が、図18において一点鎖線で示
す如く羽根車側板40の外周からはみ出す状態に変位
し、この為、最悪の場合、高速回転時に羽根41,42
がケーシング内周面31aに接触して破損を招く危険性
があり、その接触回避のために使用回転速度が低く制限
されて送風性能が制限される問題があった。
However, this type of centrifugal blower requires only one impeller side plate 40 as compared with a type in which the blades 41 and 42 are supported in a double-supported state, so that manufacturing and cost are reduced. In addition, there is an advantage that the required power can be reduced by reducing the weight of the impeller 29. However, since the blades 41 and 42 are in a cantilever support state,
During rotation of the impeller 29, the impeller side plate 40 and the blades 41 and 42 are bent by centrifugal force and gas resistance, and the free ends of the cantilevered blades 41 and 42 (specifically, the impeller side plate 40
Free ends 41b, 42b on the side opposite to the support side for
18 and the blade outer edges 41a and 42a in the rotational radius direction) are displaced so as to protrude from the outer periphery of the impeller side plate 40 as shown by a one-dot chain line in FIG. The blades 41, 42 when rotating
However, there is a danger that the contact with the inner peripheral surface 31a of the casing may cause breakage. In order to avoid such contact, there has been a problem that the rotational speed used is limited to a low value and the blowing performance is limited.

【0004】また、ケーシング内周面31aとの接触に
は至らずとも、回転半径方向における羽根41,42の
外側端縁41a,42aとそれに対向するケーシング内
周面31aとの間のクリアランスが、羽根遊端部の上記
の如き変位により不適切なものとなり、これが原因で送
風性能が低下する問題もあった。
In addition, even if the clearance does not come into contact with the casing inner peripheral surface 31a, the clearance between the outer edges 41a, 42a of the blades 41, 42 in the rotational radial direction and the casing inner peripheral surface 31a opposed thereto is reduced. The displacement of the free end of the blade as described above makes the blade unsuitable, and there is also a problem that the blowing performance is reduced due to this.

【0005】この実情に鑑み、本発明の主たる課題は、
羽根を片持ち支持状態に設ける形式のメリットを活かし
ながら、合理的な改良により上記問題を解消する点にあ
る。
[0005] In view of this situation, the main problems of the present invention are:
The problem is to solve the above problem by rational improvement while taking advantage of the form of providing the blade in a cantilevered support state.

【0006】[0006]

【課題を解決するための手段】〔1〕請求項1に係る発
明では、多数の羽根を羽根車側板に対する片持ち支持状
態で回転周方向に並設して羽根車を形成する構成におい
て、回転半径方向における前記羽根の外側端縁を、前記
羽根車側板に対する支持側とは反対側の羽根遊端側ほど
回転軸芯寄りとなる傾斜姿勢に形成する。
Means for Solving the Problems [1] In the invention according to the first aspect, in a configuration in which a large number of blades are arranged side by side in a rotating circumferential direction in a cantilevered state with respect to an impeller side plate, a rotating blade is formed. The outer edge of the blade in the radial direction is formed so as to be inclined toward the rotation axis closer to the blade free end side opposite to the support side with respect to the impeller side plate.

【0007】この構成によれば、羽根車の回転において
遠心力や気体抵抗により羽根車側板や羽根自身が撓んで
羽根の遊端部が変位することを予め見込んで、回転半径
方向における羽根の外側端縁を、非回転時の初期姿勢と
して、羽根遊端側ほど回転軸芯寄りとなる傾斜姿勢にし
ておくから、回転半径方向における羽根の外側端縁を単
に回転軸芯と平行な姿勢に形成する従来の構造に比べ、
羽根が上記の如き変位によりケーシング内周面に接触す
るといった事態をより確実に回避することができ、これ
により従来構造に比べ羽根車の使用回転速度を高めるこ
とができる。
[0007] According to this configuration, it is anticipated that the impeller side plate and the blade itself bend due to centrifugal force and gas resistance during the rotation of the impeller and the free end of the blade is displaced. Since the edge is set as an initial attitude at the time of non-rotation, the outer edge of the blade in the radial direction of rotation is simply formed in a posture parallel to the axis of the rotation because the blade is inclined toward the rotation axis closer to the free end of the blade. Compared to the conventional structure
It is possible to more reliably prevent the blade from contacting the inner peripheral surface of the casing due to the displacement as described above, so that the rotational speed of the impeller can be increased as compared with the conventional structure.

【0008】また、回転半径方向における羽根の外側端
縁とそれに対向するケーシング内周面との間のクリアラ
ンスを、回転による羽根遊端部の変位によって逆に適正
化する運転形態となり、これらのことから、この種の遠
心送風機の送風性能を効果的に高めることができる。
In addition, the clearance between the outer edge of the blade in the radial direction of rotation and the inner peripheral surface of the casing facing the blade is inversely optimized by the displacement of the free end of the blade due to the rotation. Therefore, the blowing performance of this type of centrifugal blower can be effectively improved.

【0009】〔2〕請求項2に係る発明では、回転軸芯
近くから羽根車側板の外周部にわたる主羽根の多数を、
前記羽根車側板に対する片持ち支持状態で回転周方向に
並設するとともに、前記羽根車側板の外周部にのみ位置
する補助羽根を、前記羽根車側板に対する片持ち支持状
態で前記主羽根どうしの間に設けて羽根車を形成する構
成において、回転半径方向における前記補助羽根の外側
端縁を、前記羽根車側板に対する支持側とは反対側の羽
根遊端側ほど回転軸芯寄りとなる傾斜姿勢に形成する。
[2] In the invention according to claim 2, a large number of the main blades extending from near the rotation axis center to the outer peripheral portion of the impeller side plate are formed.
Along with being arranged side by side in the rotational circumferential direction in a cantilevered state with respect to the impeller side plate, auxiliary blades located only on the outer peripheral portion of the impeller side plate are placed between the main blades in a cantilevered state with respect to the impeller side plate. In the configuration in which the impeller is formed, the outer edge of the auxiliary blade in the rotational radial direction is inclined toward the rotation axis closer to the blade free end side opposite to the support side with respect to the impeller side plate. Form.

【0010】つまり、主羽根どうしの間で羽根車側板の
外周部に設ける補助羽根は、吸入抵抗を小さく維持しな
がら羽根群全体としての遠心加速性能を高めて送風能力
を向上させる機能を有するが、この補助羽根は羽根車側
板の外周部にのみ位置させるもの(すなわち、回転軸芯
近くから羽根車側板の外周部にわたる主羽根に比べ回転
半径方向の羽根長さが短いもの)であることから、主羽
根に比べ撓み易くて羽根車側板の外周から羽根の遊端部
がはみ出す状態の変位が起こり易く、この為、この補助
羽根のケーシング内周面に対する接触を回避する上で使
用回転速度が低く制限されるといったことが生じ易く、
また、接触に至らずとも、回転半径方向における補助羽
根の外側端縁とそれに対向するケーシング内周面との間
のクリアランスが不適切になって送風性能が低下すると
いったことが生じ易い。
That is, the auxiliary blade provided on the outer peripheral portion of the impeller side plate between the main blades has a function of improving the centrifugal acceleration performance of the entire blade group and improving the blowing ability while keeping the suction resistance small. However, since the auxiliary blade is located only on the outer peripheral portion of the impeller side plate (that is, the length of the blade in the radial direction of rotation is shorter than the main blade extending from near the rotation axis to the outer peripheral portion of the impeller side plate). However, the blade is more likely to bend than the main blade, and the free end of the blade is likely to be displaced from the outer periphery of the impeller side plate, so that the rotation speed used to avoid contact of the auxiliary blade with the inner peripheral surface of the casing is increased. It is easy to be restricted low,
Even without contact, the clearance between the outer edge of the auxiliary blade in the radial direction of rotation and the inner circumferential surface of the casing facing the outer edge is likely to be inappropriate, and the blowing performance is likely to be reduced.

【0011】これに対し、上記の構成によれば、回転に
より補助羽根の遊端部が大きく変位することを予め見込
んで、回転半径方向における補助羽根の外側端縁を、非
回転時の初期姿勢として、補助羽根の遊端側ほど回転軸
芯寄りとなる傾斜姿勢にしておくから、回転半径方向に
おける補助羽根の外側端縁を単に回転軸芯と平行な姿勢
に形成する従来の構造に比べ、補助羽根が上記の如き変
位によりケーシング内周面に接触するといった事態をよ
り確実に回避することができ、これにより従来構造に比
べ羽根車の使用回転速度を高めることができる。
On the other hand, according to the above configuration, the outer edge of the auxiliary blade in the radial direction of rotation is set to the initial posture when not rotating, in anticipation that the free end of the auxiliary blade is largely displaced by rotation. As the free end side of the auxiliary blade is inclined toward the rotation axis closer to the free end side, compared to a conventional structure in which the outer edge of the auxiliary blade in the rotational radius direction is simply formed in a position parallel to the rotation axis. Such a situation that the auxiliary blades come into contact with the inner peripheral surface of the casing due to the displacement as described above can be more reliably avoided, so that the rotational speed of the impeller can be increased as compared with the conventional structure.

【0012】また、回転半径方向における補助羽根の外
側端縁とそれに対向するケーシング内周面との間のクリ
アランスを、回転による補助羽根の遊端部の変位をもっ
て逆に適正化する運転形態となり、これらのことから、
補助羽根の装備による送風性能の向上と相俟って、この
種の遠心送風機の送風性能を効果的に高めることができ
る。
[0012] Further, there is provided an operation mode in which the clearance between the outer edge of the auxiliary blade in the radial direction of rotation and the inner peripheral surface of the casing opposite thereto is appropriately adjusted by the displacement of the free end of the auxiliary blade due to rotation. from these things,
The air blowing performance of this type of centrifugal blower can be effectively improved in combination with the improvement of the air blowing performance due to the provision of the auxiliary blades.

【0013】〔3〕請求項3に係る発明では、上記した
請求項2に係る発明の実施において、回転半径方向にお
ける前記補助羽根及び前記主羽根夫々の外側端縁を、前
記羽根車側板に対する支持側とは反対側の羽根遊端側ほ
ど回転軸芯寄りとなる傾斜姿勢に形成するとともに、前
記補助羽根の回転半径方向における外側端縁の傾斜角度
を、前記主羽根の回転半径方向における外側端縁の傾斜
角度よりも大きくする。
[3] According to a third aspect of the present invention, in the embodiment of the second aspect of the present invention, the outer edges of the auxiliary blade and the main blade in the rotational radial direction are supported by the impeller side plate. And the inclination angle of the outer edge in the rotational radius direction of the auxiliary blade is set to the outer end in the rotational radius direction of the main blade. Make it larger than the edge inclination angle.

【0014】この構成によれば、回転により主羽根の遊
端部が変位して、主羽根の回転半径方向における外側端
縁とそれに対向するケーシング内周面との間のクリアラ
ンスが不適切になることも防止できる。
According to this configuration, the free end of the main blade is displaced by the rotation, and the clearance between the outer edge in the rotation radial direction of the main blade and the inner peripheral surface of the casing facing the outer edge becomes inappropriate. Can also be prevented.

【0015】そしてまた、前述の如く主羽根よりも補助
羽根の方が撓み易いことに対し、補助羽根の回転半径方
向における外側端縁の傾斜角度を、主羽根の回転半径方
向における外側端縁の傾斜角度よりも大きくしておくこ
とにより、回転による各羽根の遊端部の変位をもって、
補助羽根についての上記クリアランスと主羽根について
の上記クリアランスとが同等のものとなるようにするこ
とができ、これにより、補助羽根についての上記クリア
ランスと主羽根についての上記クリアランスとが互いに
異なることに原因する脈動的な圧力変化で振動や騒音が
発生することも効果的に抑制した状態で、各羽根につい
ての上記クリアランスの適正化をもって送風性能の向上
を一層効果的に達成できる。
Further, as described above, the auxiliary blade is more flexible than the main blade, but the inclination angle of the outer edge in the rotational radius direction of the auxiliary blade is determined by changing the inclination angle of the outer edge in the rotational radius direction of the main blade. By making it larger than the inclination angle, with the displacement of the free end of each blade due to rotation,
The clearance for the auxiliary blade and the clearance for the main blade can be made equivalent, thereby causing the clearance for the auxiliary blade and the clearance for the main blade to be different from each other. In a state where the generation of vibration and noise due to the pulsating pressure change is effectively suppressed, the improvement of the ventilation performance can be more effectively achieved by optimizing the clearance for each blade.

【0016】〔4〕請求項4に係る発明では、回転軸芯
近くから羽根車側板の外周部にわたる主羽根の多数を、
前記羽根車側板に対する片持ち支持状態で回転周方向に
並設するとともに、前記羽根車側板の外周部にのみ位置
する補助羽根を、前記羽根車側板に対する片持ち支持状
態で前記主羽根どうしの間に設けて羽根車を形成する構
成において、前記羽根車側板に対する片持ち支持状態
で、かつ、前記羽根車側板からの回転軸芯方向における
突出寸法が前記補助羽根よりも小さい状態で、回転半径
方向における前記補助羽根の内側端縁部から連なって回
転軸芯側に延びる羽根延長リブを設ける。
[4] In the invention according to claim 4, a large number of the main blades extending from near the rotation axis to the outer peripheral portion of the impeller side plate are formed.
Along with being arranged side by side in the rotational circumferential direction in a cantilevered state with respect to the impeller side plate, auxiliary blades located only on the outer peripheral portion of the impeller side plate are placed between the main blades in a cantilevered state with respect to the impeller side plate. In the configuration in which the impeller is formed to be provided in a cantilevered state with respect to the impeller side plate, and in a state in which a protrusion dimension in the rotation axis center direction from the impeller side plate is smaller than the auxiliary blade, the rotational radial direction And a blade extension rib extending from the inner edge of the auxiliary blade toward the rotation axis.

【0017】この構成によれば、回転により補助羽根が
撓み易いことに対し、上記の羽根延長リブにより補助羽
根そのものの撓み及び羽根車側板の撓みを抑制して、補
助羽根の遊端部が羽根車側板の外周からはみ出す状態に
変位することを効果的に防止でき、これにより、補助羽
根がケーシングの内周面に接触するといった事態をより
確実に回避することができて羽根車の使用回転速度を高
めることができ、また、回転半径方向における補助羽根
の外側端縁とそれに対向するケーシング内周面との間の
クリアランスも適正な状態により安定的に維持すること
ができる。
According to this structure, the auxiliary blade is easily bent by the rotation, but the bending of the auxiliary blade itself and the bending of the impeller side plate are suppressed by the blade extending rib, so that the free end portion of the auxiliary blade becomes the blade. It is possible to effectively prevent displacement to a state of protruding from the outer periphery of the vehicle side plate, thereby more reliably avoiding a situation in which the auxiliary blade comes into contact with the inner peripheral surface of the casing. And the clearance between the outer edge of the auxiliary blade in the radial direction of rotation and the inner peripheral surface of the casing opposed thereto can be stably maintained in an appropriate state.

【0018】しかも、上記の羽根延長リブは、回転半径
方向における補助羽根の内側端縁部から連なって回転軸
芯側に延びるものではあるが、羽根車側板からの回転軸
芯方向における突出寸法が補助羽根よりも小さいことか
ら、この羽根延長リブの付設によって吸入抵抗が増大す
るといったことは回避できて、吸入抵抗を小さく維持し
ながら羽根群全体としての遠心加速性能を高めるという
補助羽根の機能は維持でき、これらのことから、この種
の遠心送風機の送風性能を効果的に高めることができ
る。
Further, the above-mentioned blade extending ribs extend from the inner edge of the auxiliary blade in the rotational radius direction toward the rotation axis side, but have a protrusion dimension from the impeller side plate in the rotation axis direction. Since the auxiliary blade is smaller than the auxiliary blade, it is possible to avoid an increase in suction resistance due to the provision of the blade extension rib, and the function of the auxiliary blade to enhance the centrifugal acceleration performance of the entire blade group while maintaining a low suction resistance. It can be maintained, and from these, the blowing performance of this type of centrifugal blower can be effectively improved.

【0019】〔5〕請求項5に係る発明では、多数の羽
根を羽根車側板に対する片持ち支持状態で回転周方向に
並設して羽根車を形成する構成において、前記羽根車を
内装するケーシングのうち、回転半径方向において前記
羽根の外側端縁に対向するケーシング内周面を、前記羽
根の前記羽根車側板に対する支持側とは反対側の羽根遊
端側ほど回転軸芯から離れる傾斜姿勢に形成する。
[5] In the invention according to claim 5, in the configuration in which a number of blades are arranged side by side in the rotating circumferential direction in a cantilevered support state with respect to the impeller side plate, a casing in which the impeller is provided is provided. The inner peripheral surface of the casing facing the outer edge of the blade in the radial direction of rotation is inclined such that the free side of the blade, which is opposite to the support side of the blade with respect to the impeller side plate, is further away from the rotation axis. Form.

【0020】この構成によれば、羽根車の回転において
遠心力や気体抵抗により羽根車側板や羽根自身が撓んで
羽根の遊端部が変位することを予め見込んで、回転半径
方向における羽根の外側端縁に対向するケーシング内周
面を、羽根の遊端側ほど回転軸芯から離れる傾斜姿勢に
しておくから、このケーシング内周面を単に回転軸芯と
平行な姿勢に形成する従来の構造に比べ、羽根が上記の
如き変位によりケーシング内周面に接触するといった事
態をより確実に回避することができ、これにより従来構
造に比べ羽根車の使用回転速度を高めることができる。
According to this configuration, it is anticipated that the impeller side plate or the blade itself is bent by the centrifugal force or the gas resistance during the rotation of the impeller and the free end of the blade is displaced. Since the inner peripheral surface of the casing facing the edge is inclined away from the axis of rotation toward the free end of the blade, the conventional structure in which the inner peripheral surface of the casing is simply formed in an attitude parallel to the axis of rotation is used. In comparison, it is possible to more reliably avoid a situation in which the blade comes into contact with the inner peripheral surface of the casing due to the displacement as described above, and thus, it is possible to increase the operating rotational speed of the impeller as compared with the conventional structure.

【0021】また、回転半径方向における羽根の外側端
縁とそれに対向するケーシング内周面との間のクリアラ
ンスを、回転による羽根遊端部の変位によって逆に適正
化する運転形態となり、これらのことから、前記した請
求項1に係る発明と同様、この種の遠心送風機の送風性
能を効果的に高めることができる。
In addition, the operation mode is such that the clearance between the outer edge of the blade in the radial direction of rotation and the inner peripheral surface of the casing opposed thereto is appropriately optimized by the displacement of the free end of the blade due to the rotation. Therefore, similarly to the above-described invention according to claim 1, the blowing performance of this type of centrifugal blower can be effectively improved.

【0022】〔6〕請求項6に係る発明では、多数の羽
根を羽根車側板に対する片持ち支持状態で回転周方向に
並設して羽根車を形成する構成において、前記羽根車側
板の板厚を回転軸芯側ほど大きくする。
[6] In the invention according to claim 6, in the configuration in which a large number of blades are arranged side by side in the circumferential direction of rotation in a cantilever support state with respect to the impeller side plate, the plate thickness of the impeller side plate is provided. Is increased toward the rotation axis.

【0023】この構成によれば、片持ち支持状態の羽根
を設けた羽根車側板の遠心力による撓みを羽根車側板自
身の上記の如き板厚設定により抑制して、羽根の遊端部
が羽根車側板の外周からはみ出す状態に変位することを
効果的に防止でき、これにより、羽根がケーシング内周
面に接触するといった事態をより確実に回避することが
できて羽根車の使用回転速度を高めることができ、ま
た、回転半径方向における羽根の外側端縁とそれに対向
するケーシング内周面との間のクリアランスも適正な状
態により安定的に維持することができ、これらのことか
ら、この種の遠心送風機の送風性能を効果的に高めるこ
とができる。
According to this configuration, the deflection of the impeller side plate provided with the cantilevered blades due to the centrifugal force is suppressed by the above-described plate thickness setting of the impeller side plate itself, so that the free end of the blade becomes the blade. It is possible to effectively prevent displacement to a state of protruding from the outer periphery of the vehicle side plate, whereby it is possible to more reliably avoid a situation where the blade contacts the inner peripheral surface of the casing, and to increase the rotational speed of the impeller. In addition, the clearance between the outer edge of the blade in the radial direction of rotation and the inner peripheral surface of the casing facing the same can be more stably maintained in an appropriate state. The blowing performance of the centrifugal blower can be effectively improved.

【0024】〔7〕請求項7に係る発明では、多数の羽
根を羽根車側板に対する片持ち支持状態で回転周方向に
並設して羽根車を形成する構成において、前記羽根車側
板に、回転軸芯近くから前記羽根車側板の外周部にわた
って回転半径方向に延びる凸条リブを回転軸芯方向視で
放射状に複数設ける。
[7] In the invention according to claim 7, in the configuration in which a large number of blades are arranged side by side in the circumferential direction of rotation in a cantilever support state with respect to the impeller side plate, the impeller side plate is A plurality of ridge ribs are provided radially extending from the vicinity of the shaft center to the outer peripheral portion of the impeller side plate in the rotation radial direction as viewed in the rotation shaft center direction.

【0025】この構成によれば、片持ち支持状態の羽根
を設けた羽根車側板の遠心力による撓みを上記の如き放
射状配置の複数の凸条リブにより抑制して、羽根の遊端
部が羽根車側板の外周からはみ出す状態に変位すること
を効果的に防止でき、これにより、上記の請求項6に係
る発明と同様、羽根がケーシング内周面に接触するとい
った事態をより確実に回避することができて羽根車の使
用回転速度を高めることができ、また、回転半径方向に
おける羽根の外側端縁とそれに対向するケーシング内周
面との間のクリアランスも適正な状態により安定的に維
持することができ、これらのことから、この種の遠心送
風機の送風性能を効果的に高めることができる。
According to this configuration, the deflection due to the centrifugal force of the impeller side plate provided with the cantilever-supported blades is suppressed by the plurality of radially arranged ribs as described above, and the free end of the blade becomes the blade. It is possible to effectively prevent the vehicle from being displaced so as to protrude from the outer periphery of the vehicle side plate, thereby more reliably avoiding a situation in which the blade contacts the inner peripheral surface of the casing, similarly to the invention according to claim 6 described above. To increase the operating speed of the impeller, and to maintain a stable clearance between the outer edge of the blade in the radial direction of rotation and the inner peripheral surface of the casing in an appropriate state. Therefore, the blowing performance of this type of centrifugal blower can be effectively improved.

【0026】〔8〕請求項8に係る発明では、多数の羽
根を羽根車側板に対する片持ち支持状態で回転周方向に
並設して羽根車を形成する構成において、回転軸に対す
る前記羽根車のボス部を、前記回転軸に対し外嵌する内
筒部と、前記羽根及び前記羽根車側板に対する連結基部
としての外筒部と、これら内筒部と外筒部との回転軸芯
方向における一端部どうしにわたらせる環状底板部とで
形成するのに、前記環状底板部を前記羽根車側板と同一
面上又はほぼ同一面上に配置した状態で、前記内筒部及
び前記外筒部を前記環状底板部に対して、前記羽根車側
板に対する前記羽根の連設側と同じ側に位置させた構造
にする。
[8] In the invention according to claim 8, in the configuration in which a number of blades are arranged side by side in the circumferential direction of rotation in a cantilevered state with respect to the impeller side plate, the impeller of the impeller with respect to the rotating shaft is formed. A boss portion, an inner cylinder portion fitted externally to the rotation shaft, an outer cylinder portion as a connection base for the blades and the impeller side plate, and one end of the inner cylinder portion and the outer cylinder portion in a rotation axis center direction. The inner tubular portion and the outer tubular portion are formed in such a manner that the annular bottom plate portion is formed on the same surface or substantially the same surface as the impeller side plate to be formed with the annular bottom plate portion extending between the portions. With respect to the annular bottom plate portion, the structure is such that it is located on the same side as the side where the blades are connected to the impeller side plate.

【0027】この構成によれば、例えば、上記構造とは
逆に内筒部と外筒部の他端部(すなわち、両筒部どうし
の間の空洞部が開口する側のボス端部)を回転軸芯方向
で羽根車側板に対応位置させた状態で、環状底板部を回
転軸芯方向で羽根車側板に対する羽根の連設側と同じ側
に羽根車側板から離間させた位置に配置する構造に比
べ、羽根車側板と同一面上又はほぼ同一面上に位置する
環状底板部の存在をもって、遠心力による羽根車側板の
撓み(すなわち、片持ち支持状態の羽根に原因する羽根
車側板の背面側への撓み)に対する連結基部側の剛性を
高くすることができる。
According to this configuration, for example, contrary to the above structure, the other end of the inner cylinder and the outer cylinder (that is, the end of the boss on the side where the cavity between the two cylinders opens) is formed. A structure in which the annular bottom plate is arranged at a position separated from the impeller side plate on the same side as the side where the blades are connected to the impeller side plate in the direction of the rotation axis, in a state corresponding to the impeller side plate in the rotation axis center direction. In comparison with the above, the presence of the annular bottom plate located on the same plane or substantially the same plane as the impeller side plate causes the impeller side plate to bend due to centrifugal force (that is, the back surface of the impeller side plate caused by the cantilevered blade). (Bending to the side), the rigidity of the connection base side can be increased.

【0028】そして、このことにより、片持ち支持状態
の羽根を設けた羽根車側板の遠心力による撓みを抑制し
て、羽根の遊端部が羽根車側板の外周からはみ出す状態
に変位することを効果的に防止でき、これにより、上記
した請求項6,7に係る発明と同様、羽根がケーシング
内周面に接触するといった事態をより確実に回避するこ
とができて羽根車の使用回転速度を高めることができ、
また、回転半径方向における羽根の外側端縁とそれに対
向するケーシング内周面との間のクリアランスも適正な
状態により安定的に維持することができ、これらのこと
から、この種の遠心送風機の送風性能を効果的に高める
ことができる。
By this, the deflection of the impeller side plate provided with the cantilevered blades due to centrifugal force is suppressed, and the free end of the blade is displaced so as to protrude from the outer periphery of the impeller side plate. It is possible to effectively prevent the occurrence of such a situation that the blade contacts the inner peripheral surface of the casing, as in the case of the above-described inventions. Can be enhanced,
In addition, the clearance between the outer edge of the blade in the radial direction of rotation and the inner peripheral surface of the casing opposed thereto can be more stably maintained in an appropriate state. Performance can be effectively improved.

【0029】なお、同一面上又はほぼ同一面上に配置す
る羽根車側板と環状底板部とを一連の一体部材で形成す
れば、羽根車側板の撓みに対する連結基部側の剛性を一
層高めることができ、片持ち支持状態の羽根を設けた羽
根車側板の遠心力による撓みを更に効果的に抑制でき
る。
If the impeller side plate and the annular bottom plate are disposed on the same plane or substantially on the same plane and formed as a series of integral members, the rigidity of the connection base side against the deflection of the impeller side plate can be further increased. Thus, it is possible to more effectively suppress deflection of the impeller side plate provided with the cantilevered blades due to centrifugal force.

【0030】以上の如く、請求項1〜8のいずれかに係
る発明によれば、羽根を片持ち支持状態に設ける形式の
遠心送風機において、片持ち支持による先述の如き製作
面、コスト面、並びに、必要動力面での利点を活かしな
がら、その送風性能を効果的に高めることができ、特に
施肥装置用の送風機(肥料の空気搬送に用いる送風機)
など高速回転が要求される送風機や、撓みの生じ易い樹
脂製送風機の性能向上に極めて有効である。
As described above, according to the invention according to any one of the first to eighth aspects, in the centrifugal blower of the type in which the blades are provided in a cantilever support state, the manufacturing, cost, and cost aspects as described above by cantilever support are provided. It can effectively increase the air blowing performance while taking advantage of the required power, especially for air blowers for fertilizer application equipment (air blowers used for air transport of fertilizer)
For example, it is extremely effective for improving the performance of a blower that requires high-speed rotation or a resin blower that is easily bent.

【0031】[0031]

【発明の実施の形態】以下、実施の形態を図面に基づい
て説明する。
Embodiments of the present invention will be described below with reference to the drawings.

【0032】〔第1実施形態〕図1には施肥装置付き田
植機の全体側面が示されている。この田植機は、乗用型
の走行機体1の後部に昇降リンク機構2を介して昇降自
在に苗植付装置3が連結されるとともに、走行機体1の
後部に施肥装置4が搭載されている。
[First Embodiment] FIG. 1 shows an overall side view of a rice transplanter with a fertilizer application device. In this rice transplanter, a seedling planting device 3 is connected to a rear portion of a riding type traveling machine 1 via a lifting link mechanism 2 so as to be able to move up and down freely, and a fertilizer device 4 is mounted at a rear portion of the traveling machine 1.

【0033】走行機体1は、その前部に搭載されたエン
ジン5、エンジン5からの動力が伝達される変速装置
6、変速装置6を経由した変速後の動力が伝達される左
右一対の前輪7と後輪8、前輪7を操向するステアリン
グハンドル9、及び、運転座席10などによって構成さ
れている。
The traveling body 1 has an engine 5 mounted on its front part, a transmission 6 to which power from the engine 5 is transmitted, and a pair of left and right front wheels 7 to which power after shifting via the transmission 6 is transmitted. And a steering wheel 9 for steering the rear wheels 8 and the front wheels 7, and a driver's seat 10.

【0034】苗植付装置3は、変速装置6を経由した変
速後の動力が伝達されるフィードケース11、植付伝動
ケース12、植付伝動ケース12の後部左右両側に軸支
されたロータリ式の植付機構13、所定のストロークで
往復横移動される苗載台14、及び、整地フロート15
などによって構成されている。
The seedling planting device 3 includes a feed case 11, a planting transmission case 12, and a rotary type that is pivotally supported on the left and right sides of the rear of the planting transmission case 12 to which the power after shifting via the transmission 6 is transmitted. Planting mechanism 13, seedling table 14 which is reciprocated and laterally moved by a predetermined stroke, and leveling float 15
It is constituted by such as.

【0035】図1〜図3に示すように、施肥装置4は、
粉粒状の肥料を貯留するホッパー16、ホッパー16内
の肥料を所定量ずつ繰り出す繰出機構17、整地フロー
ト15の左右両部に装着された作溝器18、繰出機構1
7と作溝器18とを連通接続する供給ホース19、繰出
機構17から繰り出された肥料を供給ホース19を介し
て作溝器18に圧送する遠心送風機20、及び、走行機
体1に装備された動力分配機構21の出力軸21aから
繰出機構17の入力軸17aに亘って架設された施肥用
伝動機構22などによって構成されており、ホッパ16
と繰出機構17が走行機体1における運転座席10の後
部箇所に配設されている。
As shown in FIGS. 1 to 3, the fertilizer applicator 4
A hopper 16 for storing powdered and granular fertilizer, a feeding mechanism 17 for feeding a predetermined amount of fertilizer in the hopper 16, a groove forming device 18 attached to both left and right portions of the leveling float 15, a feeding mechanism 1
A supply hose 19 for communicating and connecting the 7 with the groove generator 18, a centrifugal blower 20 for feeding fertilizer fed from the feeding mechanism 17 to the groove generator 18 via the supply hose 19, and the traveling machine 1. The hopper 16 is composed of a fertilizer application transmission mechanism 22 and the like that extends from an output shaft 21a of the power distribution mechanism 21 to an input shaft 17a of the feeding mechanism 17.
And a feeding mechanism 17 are disposed at a rear portion of the driving seat 10 in the traveling body 1.

【0036】施肥用伝動機構22は、動力分配機構21
における出力軸21aの両端に位相が異なる状態で一体
回転可能に連結された左右一対の回転アーム23、各繰
出機構17に亘るように架設された単一の駆動軸24、
駆動軸24と各入力軸17aとの間に介装された断続ク
ラッチ機構25、駆動軸24にワンウェイクラッチ26
を介して連結された左右一対の揺動アーム27、及び、
対応する回転アーム23と揺動アーム27とを連係する
ロッド28などにより、回転運動を往復揺動運動に変換
した後、ワンウェイクラッチ26を介して往復揺動運動
の一方向のみを伝動することで各繰出機構17を間歇駆
動するように構成されている。
The fertilizer application transmission mechanism 22 includes a power distribution mechanism 21.
, A pair of left and right rotating arms 23 connected to both ends of the output shaft 21a so as to be integrally rotatable in different phases, a single drive shaft 24 spanned over each feeding mechanism 17,
An intermittent clutch mechanism 25 interposed between the drive shaft 24 and each input shaft 17a, and a one-way clutch 26
A pair of left and right swing arms 27 connected via
By converting the rotational motion into a reciprocating oscillating motion by a rod 28 or the like that links the corresponding rotating arm 23 and the oscillating arm 27, only one direction of the reciprocating oscillating motion is transmitted via the one-way clutch 26. Each feeding mechanism 17 is configured to be driven intermittently.

【0037】図2〜図5に示すように、施肥用の遠心送
風機20は、羽根車29、これを回転駆動する電動モー
タ30、及び、羽根車29を外囲する周部がスパイラル
状のケーシング31などによって構成されており、ケー
シング31の周部に接線方向に向けて開口された吐出口
aが、各繰出機構17の導風口17bに接続されるよう
に各繰出機構17に亘って横架された大径の給気パイプ
32の左端部に接続されている。
As shown in FIGS. 2 to 5, the centrifugal blower 20 for applying fertilizer includes an impeller 29, an electric motor 30 for rotating the impeller 29, and a casing surrounding the impeller 29 having a spiral shape. 31 and the like, and a discharge port a opened in a tangential direction on a peripheral portion of the casing 31 is horizontally laid across the respective feeding mechanisms 17 so as to be connected to the air guide ports 17b of the respective feeding mechanisms 17. The large diameter air supply pipe 32 is connected to the left end.

【0038】つまり、この施肥装置4は、各繰出機構1
7がホッパ16から所定量の肥料を繰り出し、繰り出さ
れた肥料を遠心送風機20からの送出風にのせて各供給
ホース19を介して各作溝器18へ空気搬送し、作溝器
18によって圃場に形成された施肥溝に肥料を埋設する
ようになっている。
That is, the fertilizer applicator 4 is provided with each feeding mechanism 1
7 feeds out a predetermined amount of fertilizer from the hopper 16, puts the fed out fertilizer on the air blown from the centrifugal blower 20, and conveys the air through the supply hoses 19 to the respective groove generators 18. The fertilizer is buried in the fertilizer groove formed in the area.

【0039】尚、遠心送風機20と各繰出機構17とに
亘らせる給気パイプ32は、各繰り出し機構17におけ
る短パイプ32aどうし、及び、端の短パイプ32aと
遠心送風機20とを、着脱自在なゴム製の繋ぎホース3
2bにより連結することで形成してあり、保守点検時な
どには繋ぎホース32bを外すことで分解できるように
してある。
The air supply pipe 32 extending between the centrifugal blower 20 and each feeding mechanism 17 is configured such that the short pipes 32a in each feeding mechanism 17 and the short pipe 32a at the end and the centrifugal blower 20 are detachable. Rubber connecting hose 3
2b, and can be disassembled by removing the connecting hose 32b at the time of maintenance and inspection.

【0040】図2及び図3における符号17cは、各繰
出機構17に形成された肥料供給口であり、この肥料供
給口17cに対応する供給ホース19が接続されるよう
になっている。図2における符号33は、供給ホース1
9が接続されない肥料供給口17cを閉塞するキャップ
である。図3における符号17dは、各繰出機構17に
形成された残肥排出口部、又、符号34は、この残肥排
出口部17dに接続される残肥排出ホースであり、ホッ
パー16内の余剰肥料を残肥排出口部17dから残肥排
出ホース34を介して外部に排出できるようになってい
る。
Reference numeral 17c in FIGS. 2 and 3 denotes a fertilizer supply port formed in each feeding mechanism 17, and a supply hose 19 corresponding to the fertilizer supply port 17c is connected thereto. Reference numeral 33 in FIG.
Reference numeral 9 denotes a cap for closing the fertilizer supply port 17c that is not connected. Reference numeral 17d in FIG. 3 denotes a residual manure discharge port formed in each feeding mechanism 17, and reference numeral 34 denotes a residual manure discharge hose connected to the residual manure discharge port 17d. The fertilizer can be discharged from the residual fertilizer discharge port 17d to the outside via the residual fertilizer discharge hose 34.

【0041】遠心送風機20は、その吐出口aが、走行
機体1における運転座席10の後部箇所に配設された各
繰出機構17に亘って架設される給気パイプ32の左端
部に接続されることにより、操縦部1Aの近傍箇所とな
る運転座席10の左後部における左側の後輪8の左上方
箇所に位置するようになっている。そのため、遠心送風
機20は、ケーシング31の一方の側壁に形成した吸気
口bが後ろ側に位置する姿勢で配設されるとともに、そ
のケーシング31には、吸気口bを下向きに変向する吸
気ダクト35が接続されており、これによって、吸気口
bから漏出する送風機20の騒音を操縦部1Aから遠ざ
けるようになっている。
The centrifugal blower 20 has its discharge port a connected to the left end of an air supply pipe 32 spanning each of the feeding mechanisms 17 disposed at the rear part of the driving seat 10 in the traveling body 1. Thereby, it is located at the upper left position of the left rear wheel 8 in the rear left portion of the driver's seat 10 which is a position near the control section 1A. Therefore, the centrifugal blower 20 is disposed such that the intake port b formed on one side wall of the casing 31 is located on the rear side, and the casing 31 has an intake duct that turns the intake port b downward. 35 is connected so that the noise of the blower 20 leaking from the intake port b is kept away from the control section 1A.

【0042】また、吸気ダクト35の入口側端部には、
吸気口bに面する障壁体36が、その後輪8側ほど吸気
口bに近接する傾斜姿勢で配設されており、この障壁体
36によって左側の後輪8により跳ね上げられた泥土や
泥水などの吸気ダクト35内への入り込みを防止するよ
うになっている。
At the inlet end of the intake duct 35,
A barrier body 36 facing the intake port b is disposed in an inclined position closer to the intake port b toward the rear wheel 8 side, and muddy soil, muddy water, etc., which are flipped up by the rear wheel 8 on the left side by the barrier body 36. Is prevented from entering the intake duct 35.

【0043】障壁体36は、吸気ダクト35における吸
気口bの周縁部を形成する周縁部材38の縦壁部38A
に取り付けられている。周縁部材38は、その周壁38
Bが、吸気口bの周囲に降る雨水を受け止めるととも
に、受け止めた雨水を縦壁部38Aにおける吸気口bの
反対側から障壁体36の下方へ流下させるようになって
おり、もって、雨天作業時に遠心送風機20が外気とと
もに雨水を吸気口bから取り入れることに起因して、肥
料詰まりなどの施肥不良が発生することを回避するよう
になっている。また、障壁体36の周縁と周縁部材38
の周壁部38Bとに亘って、周方向に所定間隔をもって
多数の縦向きルーバ39が架設されており、これによっ
て、吸気口bと障壁体36の間を通って他物が吸気口b
から入り込むことを防止するようにしている。
The barrier 36 is formed by a vertical wall portion 38A of a peripheral member 38 forming a peripheral portion of the intake port b in the intake duct 35.
Attached to. The peripheral member 38 has a peripheral wall 38.
B receives rainwater falling around the intake port b, and causes the received rainwater to flow downward from the side opposite to the intake port b in the vertical wall portion 38A below the barrier body 36, so that during rainy weather work Due to the centrifugal blower 20 taking in rainwater together with the outside air from the intake port b, it is possible to avoid occurrence of fertilization failure such as clogging of fertilizer. Further, the peripheral edge of the barrier body 36 and the peripheral edge member 38
A number of vertically oriented louvers 39 are provided at predetermined intervals in the circumferential direction over the peripheral wall portion 38B, thereby allowing other objects to pass between the intake port b and the barrier body 36 and allow other objects to pass therethrough.
We try to prevent from entering from.

【0044】図6〜図8に示すように、遠心送風機20
の羽根車29には、ケーシング31内でモータ30の側
に位置する一枚の羽根車側板40に多数の羽根41,4
2を片持ち支持状態に設けて吸気口b側を開放したオー
プンタイプを採用してあり、そして具体的には、回転軸
芯P近くから外周に亘る湾曲放射状の主羽根41の多数
を羽根車側板40に対する片持ち支持状態で回転周方向
に並設するとともに、外周部近くにのみ位置する補助羽
根42を同様に羽根車側板40に対する片持ち支持状態
で主羽根41どうしの間に設けて羽根車29を形成して
ある。
As shown in FIGS. 6 to 8, the centrifugal blower 20
The impeller 29 has a large number of blades 41 and 4 attached to one impeller side plate 40 located on the motor 30 side in the casing 31.
2 is provided in a cantilevered support state, and an open type in which the intake port b side is opened is adopted. Specifically, a large number of curved radial main blades 41 extending from the vicinity of the rotation axis P to the outer circumference are used. The auxiliary blades 42 which are arranged side by side in the rotating circumferential direction in a cantilevered state with respect to the side plate 40 and are similarly provided between the main blades 41 in a cantilevered state with respect to the impeller side plate 40 only in the vicinity of the outer periphery. A wheel 29 is formed.

【0045】つまり、オープンタイプであれば、各羽根
を2枚の羽根車側板どうしの間にわたらせて両持ち支持
状態に設ける形式に比べ、羽根車側板40が1枚で済む
ことから製作面及びコスト面で有利となり、また、羽根
車を軽量化し得ることで必要動力も低減し得る。そして
また、上記の如き補助羽根42を設けることにより、羽
根車29の吸気側となる中心部では羽根枚数は少なく、
吸入気を遠心加速する外周部近くでは羽根枚数が多くな
り、このことから、吸気抵抗を増すことなく羽根群によ
る遠心加速機能を高めて送風性能を向上させることがで
きる。
That is, in the case of the open type, since only one impeller side plate 40 is required as compared with a type in which each blade is spread between two impeller side plates and supported in a double-supported state, the manufacturing surface and This is advantageous in terms of cost, and the required power can be reduced by reducing the weight of the impeller. Further, by providing the auxiliary blades 42 as described above, the number of blades is small at the central portion on the intake side of the impeller 29,
The number of blades increases near the outer peripheral portion where the intake air is centrifugally accelerated. Therefore, the centrifugal acceleration function of the blade group can be enhanced without increasing the intake resistance to improve the blowing performance.

【0046】なお、本例においては、羽根車側板40,
主羽根41,補助羽根42,及び、回転軸43に対する
ボス部44からなる上記羽根車29を樹脂製の一体成形
品にしてあり、また、ケーシング31は回転軸芯方向で
の2つ割り構造の樹脂成形品にしてある。
In this embodiment, the impeller side plate 40,
The impeller 29 composed of the main blade 41, the auxiliary blade 42, and the boss portion 44 for the rotary shaft 43 is an integrally molded product made of resin, and the casing 31 has a split structure in the rotary shaft core direction. It is a resin molded product.

【0047】各羽根41,42の回転半径方向における
外側端縁41a,42aは、羽根車29の回転において
遠心力や気体抵抗により羽根車側板40や羽根自身4
1,42が撓んで各羽根41,42の遊端部(詳しく
は、羽根車側板40に対する支持側とは反対側の羽根遊
端縁41b,42bと回転半径方向における羽根外側端
縁41a,42aとの交差箇所の近傍部分)が変位する
ことを予め見込んで、羽根車側板40に対する支持側と
は反対側の羽根遊端側ほど回転軸芯P寄りとなる傾斜姿
勢に形成してあり、また、羽根車側板40の外周部にの
み位置させる補助羽根42は主羽根41に比べ回転半径
方向の羽根長さが短くて撓み易いことから、上記の如き
傾斜端縁41a,42aの形成において、補助羽根42
の回転半径方向における外側端縁42aの傾斜角度はθ
2は、主羽根42の回転半径方向における外側端縁41
aの傾斜角度θ1よりも大きくしてある。
The outer edges 41a, 42a of the respective blades 41, 42 in the rotational radius direction are formed by the centrifugal force and the gas resistance during the rotation of the impeller 29 and the impeller side plate 40 and the blade 4
The free ends of the blades 41, 42 are bent (specifically, the blade free end edges 41b, 42b opposite to the support side of the impeller side plate 40 and the blade outer edges 41a, 42a in the rotational radius direction). In the vicinity of the intersection with the impeller), the blade is formed in an inclined position closer to the rotation axis P as the free end of the blade on the side opposite to the support side with respect to the impeller side plate 40 is shifted. Since the auxiliary blade 42 located only on the outer peripheral portion of the impeller side plate 40 has a shorter blade length in the radius of rotation direction than the main blade 41 and is more easily bent, the auxiliary blades 42 are not necessary for forming the inclined edges 41a and 42a as described above. Feather 42
The inclination angle of the outer edge 42a in the rotational radius direction is θ
2 is an outer edge 41 of the main blade 42 in the radial direction of rotation.
a is larger than the inclination angle θ1.

【0048】つまり、このように主羽根41及び補助羽
根42の外側端縁41a,42aを傾斜端縁にすること
で、前記の如き撓みによる羽根遊端部の変位に原因する
各羽根41,42とケーシング内周面31a(ケーシン
グ31におけるスパイラル状周部の内周面)との接触干
渉を確実に防止して、羽根車29の使用回転速度を高め
られるように、また、主羽根41の外側端縁41aとそ
れに対向するケーシング内周面31aとの間のクリアラ
ンス、及び、補助羽根42の外側端縁42aとそれに対
向するケーシング内周面31aとの間のクリアランスが
ともに、羽根車29の回転運転時において図8に一点鎖
線で示す如き羽根変位により互いに同等の適正なクリア
ランスになるようにしてある。
That is, by making the outer edges 41a, 42a of the main blade 41 and the auxiliary blades 42 be inclined edges in this manner, the respective blades 41, 42 caused by the displacement of the free blade end due to the bending described above. Interference with the inner peripheral surface 31a of the casing (the inner peripheral surface of the spiral peripheral portion of the casing 31) is reliably prevented, so that the rotation speed of the impeller 29 can be increased. The clearance between the end edge 41a and the casing inner peripheral surface 31a opposed thereto, and the clearance between the outer edge 42a of the auxiliary blade 42 and the opposed casing inner peripheral surface 31a both rotate the impeller 29. During operation, the blades are displaced as shown by a chain line in FIG.

【0049】そしてまた、羽根車側板40には、それに
対する片持ち支持状態で、かつ、羽根車側板40からの
回転軸芯方向における突出寸法が補助羽根42よりも小
さい状態で、回転半径方向における補助羽根42の内側
端縁部から連なってドーナツ板形状の羽根車側板40に
おける中央孔40aの孔縁まで延びる羽根延長リブ45
を設けてあり、これにより、補助羽根42の撓み及び羽
根車側板40の撓みそのものを極力抑制するようにして
ある。
In addition, the impeller side plate 40 is supported in a cantilevered state with respect to the impeller side plate 40, and the protrusion dimension in the rotation axis center direction from the impeller side plate 40 is smaller than the auxiliary blade 42, so that A blade extension rib 45 extending from the inner edge of the auxiliary blade 42 and extending to the edge of the central hole 40a in the donut-shaped impeller side plate 40
, Whereby the bending of the auxiliary blades 42 and the bending of the impeller side plate 40 are suppressed as much as possible.

【0050】〔第2実施形態〕上記の第1実施形態で
は、主羽根41及び補助羽根42夫々の外側端縁41
a,42aを羽根遊端側ほど回転軸芯P寄りとなる傾斜
姿勢に形成する例を示したが、これに代え、図9に示す
如く、撓みによる変位の生じ難い主羽根41について
は、その回転半径方向における外側端縁41aを回転軸
芯Pと平行な姿勢に形成し、そして、撓みによる変位の
生じ易い補助羽根42についてのみ、その回転半径方向
における外側端縁42aを羽根遊端側ほど回転軸芯P寄
りとなる傾斜姿勢に形成するようにしてもよい。
[Second Embodiment] In the first embodiment, the outer edge 41 of each of the main blade 41 and the auxiliary blade 42 is provided.
Although an example is shown in which the a and 42a are formed in an inclined position closer to the rotation axis P toward the free end of the blade, the main blade 41, which is unlikely to be displaced by bending as shown in FIG. The outer edge 41a in the rotation radius direction is formed in a posture parallel to the rotation axis P, and the outer edge 42a in the rotation radius direction of the auxiliary blade 42, which is likely to be displaced by bending, is set closer to the free end of the blade. It may be formed in an inclined posture closer to the rotation axis P.

【0051】〔第3実施形態〕前記の第1及び第2実施
形態では、各羽根41,42の外側端縁41a,42a
に対向するケーシング内周面31aを回転軸芯Pと平行
な姿勢にするのに対し、補助羽根41や主羽根42の外
側端縁41a,42aを羽根遊端側ほど回転軸芯P寄り
となる傾斜姿勢にする例を示したが、これに代え、図1
0に示す如く、回転半径方向において各羽根41,42
の外側端縁41a,42aに対向するケーシング内周面
31aの方を、羽根遊端側ほど回転軸芯Pから離れる傾
斜姿勢に形成し、これにより、撓みによる羽根遊端部の
変位に原因する各羽根41,42とケーシング内周面3
1aとの接触干渉を確実に防止して羽根車29の使用回
転速度を高められるように、また、各羽根41,42の
外側端縁41a,42aとそれに対向するケーシング内
周面31aとの間のクリアランスが羽根車29の回転運
転時において同図10に一点鎖線で示す如き羽根変位に
より極力適正なクリアランスになるようにする。
[Third Embodiment] In the first and second embodiments, the outer edges 41a, 42a of the blades 41, 42 are provided.
The inner peripheral surface 31a of the casing opposing to the axis is parallel to the rotation axis P, whereas the outer edges 41a, 42a of the auxiliary blades 41 and the main blades 42 are closer to the rotation axis P toward the free ends of the blades. Although the example in which the inclination posture is set is shown, instead of this, FIG.
As shown in FIG.
The inner peripheral surface 31a of the casing facing the outer edges 41a, 42a is formed so as to be inclined away from the rotation axis P toward the free end of the blade, thereby causing displacement of the free end of the blade due to bending. Each blade 41, 42 and casing inner peripheral surface 3
In order to reliably prevent contact interference with the blade 1a and increase the rotational speed of use of the impeller 29, between the outer edges 41a and 42a of the blades 41 and 42 and the casing inner peripheral surface 31a opposed thereto. During the rotation operation of the impeller 29, the clearance is set as appropriate as possible by the displacement of the blade as shown by the one-dot chain line in FIG.

【0052】〔第4実施形態〕前記の第1〜第3実施形
態では、羽根41,42の外側端縁41a,42aと、
それに対向するケーシング内周面31aとのいずれか一
方のみを傾斜姿勢に形成する例を示したが、これに代
え、図11に示す如く、各羽根41,42の回転半径方
向における外側端縁41a,42aを羽根遊端側ほど回
転軸芯P寄りとなる傾斜姿勢にするとともに、これら各
羽根41,42の外側端縁41a,42aに対向するケ
ーシング内周面31aを羽根遊端側ほど回転軸芯Pから
離れる傾斜姿勢に形成する。
[Fourth Embodiment] In the first to third embodiments, the outer edges 41a and 42a of the blades 41 and 42 are
An example is shown in which only one of the casing inner peripheral surface 31a opposed thereto is formed in an inclined posture. Instead, as shown in FIG. 11, the outer edge 41a of each of the blades 41, 42 in the rotational radius direction is provided. , 42a are inclined closer to the rotation axis P toward the blade free end, and the casing inner peripheral surface 31a facing the outer edge 41a, 42a of each of the blades 41, 42 is rotated closer to the blade free end. It is formed in an inclined posture away from the core P.

【0053】あるいはまた、図12に示す如く、撓みに
よる変位が生じ難い主羽根41の外側端縁41aは回転
軸芯Pと平行姿勢に形成し、これに対し、各羽根41,
42の外側端縁41a,42aに対向するケーシング内
周面31aを羽根遊端側ほど回転軸芯Pから離れる傾斜
姿勢にするとともに、撓みによる変位の生じ易い補助羽
根42の外側端縁42aを羽根遊端側ほど回転軸芯P寄
りとなる傾斜姿勢にし、これにより、撓みによる羽根遊
端部の変位に原因する各羽根41,42とケーシング内
周面31aとの接触干渉を確実に防止して羽根車29の
使用回転速度を高められるように、また、各羽根41,
42の外側端縁41a,42aとそれに対向するケーシ
ング内周面31aとの間のクリアランスが羽根車29の
回転運転時において同図11や図12に一点鎖線で示す
如き羽根変位により極力適正なクリアランスになるよう
にする。
Alternatively, as shown in FIG. 12, the outer edge 41a of the main blade 41, which is unlikely to be displaced by bending, is formed in a posture parallel to the rotation axis P. On the other hand, each blade 41,
The inner peripheral surface 31a of the casing facing the outer edges 41a, 42a is inclined away from the rotation axis P toward the free end of the blade, and the outer edge 42a of the auxiliary blade 42, which is liable to be displaced by bending, is changed to the blade. The free end side has an inclined posture closer to the rotation axis P, thereby reliably preventing contact interference between the blades 41 and 42 and the inner peripheral surface 31a of the casing caused by displacement of the free end portion of the blade due to bending. In order to increase the use rotation speed of the impeller 29, the blades 41,
When the impeller 29 rotates, the clearance between the outer edges 41a, 42a and the casing inner peripheral surface 31a opposed to the outer edges 41a, 42a is as appropriate as possible due to the displacement of the blade as shown by the one-dot chain line in FIGS. So that

【0054】〔第5実施形態〕前述の第1実施形態で
は、補助羽根42の内側端縁部から回転軸芯Pの側に延
びる羽根延長リブ45を羽根車側板40に設けて、補助
羽根42の撓み及び羽根車側板40の撓みを抑制するよ
うにしたが、この羽根延長リブ45の付設に代えて、あ
るいは、この羽根延長リブ45の付設とともに、図13
に示す如く、羽根車側板40の板厚を回転軸芯Pの側ほ
ど大きくする構造や、図14に示す如く、羽根車側板4
0に回転半径方向に延びる凸条リブ46を回転軸芯方向
視で放射状に複数設ける構造を採用し、これにより、羽
根車側板40の撓みを抑制して、その撓みに原因する各
羽根41,42とケーシング内周面31aとの接触干渉
を防止するとともに、各羽根41,42の外側端縁41
a,42aとそれに対向するケーシング内周面31aと
の間のクリアランスを適正な状態に安定的に保つように
する。
[Fifth Embodiment] In the first embodiment described above, a blade extension rib 45 extending from the inner edge of the auxiliary blade 42 toward the rotation axis P is provided on the impeller side plate 40, and the auxiliary blade 42 13 and the deflection of the impeller side plate 40 are suppressed, but instead of the addition of the blade extension ribs 45, or together with the addition of the blade extension ribs 45, FIG.
As shown in FIG. 14, a structure in which the plate thickness of the impeller side plate 40 is increased toward the rotation axis P, and as shown in FIG.
A structure is provided in which a plurality of convex ribs 46 extending radially in the rotational radius direction are provided in a radial manner as viewed in the direction of the rotational axis, thereby suppressing the bending of the impeller side plate 40, and causing the blades 41, 42 and the inner peripheral surface 31a of the casing are prevented from contacting with each other, and the outer edge 41 of each of the blades 41, 42 is prevented.
The clearance between the a, 42a and the casing inner peripheral surface 31a opposed thereto is stably maintained in an appropriate state.

【0055】〔第6実施形態〕前述の第1実施形態で示
した例では、回転軸43に対する羽根車29のボス部4
4を、回転軸43に対し外嵌する内筒部44aと、羽根
41,42及び羽根車側板40に対する連結基部として
の外筒部44bと、これら内筒部44aと外筒部44b
との回転軸芯方向における一端部どうしにわたらせる環
状底板部44cとで形成するのに、内筒部44aと外筒
部44bの他端部(すなわち、両筒部44a,44bど
うしの間の空洞部が開口する側のボス端部)を回転軸芯
方向で羽根車側板40に対応位置させた状態で、環状底
板部44cを回転軸芯方向で羽根車側板40に対する羽
根41,42の連設側と同じ側に羽根車側板40から離
間させた位置に配置する構造を示したが、これに代え、
図15に示す如く、環状底板部44cを羽根車側板40
と同一面上又はほぼ同一面上に配置した状態で、内筒部
44a及び外筒部44bを環状底板部44cに対して、
羽根車側板40に対する羽根41,42の連設側と同じ
側に位置させた構造にする。
[Sixth Embodiment] In the example shown in the first embodiment, the boss 4 of the impeller 29 with respect to the rotating shaft 43 is used.
4, an inner cylindrical portion 44a externally fitted to the rotating shaft 43, an outer cylindrical portion 44b as a connection base for the blades 41, 42 and the impeller side plate 40, and an inner cylindrical portion 44a and an outer cylindrical portion 44b.
And an annular bottom plate portion 44c extending over one end portion in the direction of the axis of rotation, the other end portion of the inner cylinder portion 44a and the outer cylinder portion 44b (that is, between the two cylinder portions 44a and 44b). The annular bottom plate portion 44c is connected to the impeller side plate 40 in the rotation axis direction with the blades 41 and 42 connected to the impeller side plate 40 in a state where the boss end on the side where the cavity is opened) is positioned corresponding to the impeller side plate 40 in the rotation axis direction. Although the structure which arrange | positions in the position spaced apart from the impeller side plate 40 on the same side as the installation side was shown, instead of this,
As shown in FIG. 15, the annular bottom plate portion 44c is
In the state where it is arranged on the same plane or almost on the same plane, the inner cylinder part 44a and the outer cylinder part 44b are
The structure is such that it is located on the same side as the side where the blades 41 and 42 are connected to the impeller side plate 40.

【0056】つまり、このボス構造では、羽根車側板4
0と同一面上又はほぼ同一面上に位置する環状底板部4
4cの存在により、羽根車側板40の撓み(片持ち支持
状態の羽根41,42に原因する羽根車側板40の背面
側への撓み)に対する連結基部側の剛性を高くして羽根
車側板40の撓みを抑制し、これにより、その撓みに原
因する各羽根41,42とケーシング内周面31aとの
接触干渉を防止するとともに、各羽根41,42の外側
端縁41a,42aとそれに対向するケーング内周面3
1aとの間のクリアランスを適正な状態に安定的に保つ
ようにする。
That is, in this boss structure, the impeller side plate 4
An annular bottom plate portion 4 located on the same plane as, or substantially on the same plane as,
Due to the presence of 4c, the rigidity of the connecting base side against bending of the impeller side plate 40 (bending to the rear side of the impeller side plate 40 due to the blades 41 and 42 in the cantilever support state) is increased, and the impeller side plate 40 is The bending is suppressed, thereby preventing the interference between the blades 41, 42 and the inner peripheral surface 31a of the casing caused by the bending, and the outer edges 41a, 42a of the blades 41, 42 and the casing facing thereto. Inner circumference 3
1a so as to stably maintain a proper clearance.

【0057】〔その他の実施形態〕次に、その他の実施
形態を列記する。補助羽根42の外側端縁42aや主羽
根41の外側端縁41aを、羽根遊端側ほど回転軸芯P
寄りとなる傾斜姿勢に形成するのに、これら外側端縁4
2a,41aを羽根基端から羽根先端にわたって一律の
傾斜角度の傾斜姿勢に形成するに代え、図16に示す如
く、羽根遊端側ほど傾斜角度が大きくなる傾斜姿勢に形
成し、これにより、回転時の撓みによる羽根遊端部の変
位において、それら羽根42,41の外側端縁42a,
41aとそれに対向するケーシング内周面31aとの間
のクリアランスが一層適切なものとなるようにしてもよ
い。
[Other Embodiments] Next, other embodiments will be listed. The outer edge 42a of the auxiliary blade 42 and the outer edge 41a of the main blade 41
These outer edges 4 are used to form a leaning posture that is closer.
Instead of forming the inclined surfaces 2a and 41a in a uniform inclination angle from the blade base end to the blade tip, as shown in FIG. 16, they are formed in an inclination posture in which the inclination angle increases toward the free end of the blade. When the free ends of the blades are displaced due to bending at the time, the outer edges 42a, 42a,
The clearance between 41a and the casing inner peripheral surface 31a opposed thereto may be made more appropriate.

【0058】前述の各実施形態では、補助羽根42を設
ける場合の例を示したが、請求項1又は請求項5〜8に
係る発明は、補助羽根を設けない図17に示す如き遠心
送風機についても適用できる。
In each of the embodiments described above, the example in which the auxiliary blades 42 are provided has been described. However, the invention according to claim 1 or claims 5 to 8 relates to a centrifugal blower as shown in FIG. Can also be applied.

【0059】本発明は、施肥装置用の遠心送風機に限ら
ず、羽根を羽根車側板に対して片持ち支持状態に設ける
形式のものであれば、種々の用途の遠心送風機に適用で
き、また、羽根車を樹脂製の一体成形品とするものに限
らず、種々の材質及び組み立て構造の遠心送風機に適用
できる。
The present invention is not limited to a centrifugal blower for a fertilizer, but can be applied to a centrifugal blower for various uses as long as the blade is provided in a cantilevered state with respect to an impeller side plate. The impeller is not limited to a resin integrally molded product, and can be applied to centrifugal blowers having various materials and assembled structures.

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

【図1】施肥装置付き田植機の全体側面図FIG. 1 is an overall side view of a rice transplanter with a fertilizer application device.

【図2】施肥装置の構成及びブロワの配置を示す背面図FIG. 2 is a rear view showing the configuration of the fertilizer application and the arrangement of the blowers.

【図3】施肥装置の構成を示す要部の縦断側面図FIG. 3 is a longitudinal sectional side view of a main part showing a configuration of a fertilizer application device.

【図4】遠心ブロワの全体側面図FIG. 4 is an overall side view of a centrifugal blower.

【図5】遠心ブロワの全体背面図FIG. 5 is an overall rear view of the centrifugal blower.

【図6】遠心ブロワの横断面図FIG. 6 is a cross-sectional view of a centrifugal blower.

【図7】遠心ブロアの縦断面図FIG. 7 is a longitudinal sectional view of a centrifugal blower.

【図8】(イ)主羽根部分における羽根車の縦断面図 (ロ)補助羽根部分における羽根車の縦断面図8A is a longitudinal sectional view of an impeller in a main blade portion. FIG. 8B is a longitudinal sectional view of an impeller in an auxiliary blade portion.

【図9】(イ)主羽根部分における羽根車の縦断面図 (ロ)補助羽根部分における羽根車の縦断面図9A is a longitudinal sectional view of an impeller in a main blade portion, and FIG. 9B is a longitudinal sectional view of an impeller in an auxiliary blade portion.

【図10】羽根車の縦断面図FIG. 10 is a longitudinal sectional view of an impeller.

【図11】(イ)主羽根部分における羽根車の縦断面図 (ロ)補助羽根部分における羽根車の縦断面図11A is a longitudinal sectional view of an impeller in a main blade portion. FIG. 11B is a longitudinal sectional view of an impeller in an auxiliary blade portion.

【図12】(イ)主羽根部分における羽根車の縦断面図 (ロ)補助羽根部分における羽根車の縦断面図12A is a longitudinal sectional view of an impeller in a main blade portion. FIG. 12B is a longitudinal sectional view of an impeller in an auxiliary blade portion.

【図13】羽根車の縦断面図FIG. 13 is a longitudinal sectional view of an impeller.

【図14】(イ)羽根車の背面図 (ロ)羽根車の縦断面図 (ハ)要部の拡大断面図14A is a rear view of the impeller. FIG. 14B is a longitudinal sectional view of the impeller.

【図15】羽根車の縦断面図FIG. 15 is a longitudinal sectional view of an impeller.

【図16】(イ)主羽根部分における羽根車の縦断面図 (ロ)補助羽根部分における羽根車の縦断面図16A is a longitudinal sectional view of an impeller in a main blade part, and FIG. 16B is a longitudinal sectional view of an impeller in an auxiliary blade part.

【図17】(イ)羽根車の正面図 (ロ)羽根車の縦断面図FIG. 17 (a) Front view of impeller (b) Longitudinal sectional view of impeller

【図18】従来構造を示す縦断面図FIG. 18 is a longitudinal sectional view showing a conventional structure.

【符号の説明】[Explanation of symbols]

29 羽根車 31 ケーシング 31a ケーシング内周面 40 羽根車側板 41 主羽根 41a 主羽根の外側端縁 42 補助羽根 42a 補助羽根の外側端縁 43 回転軸 44 ボス部 44a 内筒部 44b 外筒部 44c 環状底板部 45 羽根延長リブ 46 凸条リブ P 回転軸芯 θ1 主羽根の外側端縁の傾斜角度 θ2 補助羽根の外側端縁の傾斜角
29 Impeller 31 Casing 31a Casing inner peripheral surface 40 Impeller side plate 41 Main blade 41a Outer edge of main blade 42 Auxiliary blade 42a Outer edge of auxiliary blade 43 Rotating shaft 44 Boss 44a Inner cylinder 44b Outer cylinder 44c Annular Bottom plate part 45 Blade extension rib 46 Convex rib P Rotation axis θ1 Angle of inclination of outer edge of main blade θ2 Angle of inclination of outer edge of auxiliary blade

Claims (8)

【特許請求の範囲】[Claims] 【請求項1】 多数の羽根を羽根車側板に対する片持ち
支持状態で回転周方向に並設して羽根車を形成してある
遠心送風機であって、 回転半径方向における前記羽根の外側端縁を、前記羽根
車側板に対する支持側とは反対側の羽根遊端側ほど回転
軸芯寄りとなる傾斜姿勢に形成してある遠心送風機。
1. A centrifugal blower in which a number of blades are arranged side by side in a rotating circumferential direction in a cantilevered state with respect to an impeller side plate to form an impeller, wherein an outer edge of the blade in a radial direction of rotation is formed. A centrifugal blower is formed in an inclined posture in which the blade free end side opposite to the support side with respect to the impeller side plate is closer to the rotation axis.
【請求項2】 回転軸芯近くから羽根車側板の外周部に
わたる主羽根の多数を、前記羽根車側板に対する片持ち
支持状態で回転周方向に並設するとともに、前記羽根車
側板の外周部にのみ位置する補助羽根を、前記羽根車側
板に対する片持ち支持状態で前記主羽根どうしの間に設
けて羽根車を形成してある遠心送風機であって、 回転半径方向における前記補助羽根の外側端縁を、前記
羽根車側板に対する支持側とは反対側の羽根遊端側ほど
回転軸芯寄りとなる傾斜姿勢に形成してある遠心送風
機。
2. A large number of main blades extending from a position near a rotation axis to an outer peripheral portion of an impeller side plate are arranged side by side in a rotational circumferential direction in a cantilevered state with respect to the impeller side plate, and are provided on an outer peripheral portion of the impeller side plate. A centrifugal blower in which an auxiliary impeller is provided between the main impellers in a cantilevered state with respect to the impeller side plate to form an impeller, wherein an outer edge of the auxiliary impeller in a radial direction of rotation is provided. A centrifugal blower, which is formed in such a manner as to be closer to the axis of rotation as the free end of the blade is opposite to the support side of the impeller side plate.
【請求項3】 請求項2記載の遠心送風機であって、 回転半径方向における前記補助羽根及び前記主羽根夫々
の外側端縁を、前記羽根車側板に対する支持側とは反対
側の羽根遊端側ほど回転軸芯寄りとなる傾斜姿勢に形成
するとともに、 前記補助羽根の回転半径方向における外側端縁の傾斜角
度を、前記主羽根の回転半径方向における外側端縁の傾
斜角度よりも大きくしてある遠心送風機。
3. The centrifugal blower according to claim 2, wherein the outer edge of each of the auxiliary blade and the main blade in the rotational radius direction is a blade free end side opposite to a support side with respect to the impeller side plate. And the inclination angle of the outer edge in the radial direction of rotation of the auxiliary blade is larger than the inclination angle of the outer edge in the radial direction of rotation of the main blade. Centrifugal blower.
【請求項4】 回転軸芯近くから羽根車側板の外周部に
わたる主羽根の多数を、前記羽根車側板に対する片持ち
支持状態で回転周方向に並設するとともに、前記羽根車
側板の外周部にのみ位置する補助羽根を、前記羽根車側
板に対する片持ち支持状態で前記主羽根どうしの間に設
けて羽根車を形成してある遠心送風機であって、 前記羽根車側板に対する片持ち支持状態で、かつ、前記
羽根車側板からの回転軸芯方向における突出寸法が前記
補助羽根よりも小さい状態で、回転半径方向における前
記補助羽根の内側端縁部から連なって回転軸芯側に延び
る羽根延長リブを設けてある遠心送風機。
4. A large number of main blades extending from near the rotation axis to the outer peripheral portion of the impeller side plate are arranged side by side in the rotational circumferential direction in a cantilevered state with respect to the impeller side plate, and are provided on the outer peripheral portion of the impeller side plate. A centrifugal blower provided with only the auxiliary blades positioned only between the main blades in a cantilevered support state with respect to the impeller side plate to form an impeller, in a cantilevered support state with respect to the impeller side plate, And, in a state where the protrusion dimension in the rotation axis direction from the impeller side plate is smaller than the auxiliary blade, a blade extension rib extending from the inner edge of the auxiliary blade in the rotation radial direction and extending toward the rotation axis side. Centrifugal blower provided.
【請求項5】 多数の羽根を羽根車側板に対する片持ち
支持状態で回転周方向に並設して羽根車を形成してある
遠心送風機であって、 前記羽根車を内装するケーシングのうち、回転半径方向
において前記羽根の外側端縁に対向するケーシング内周
面を、前記羽根の前記羽根車側板に対する支持側とは反
対側の羽根遊端側ほど回転軸芯から離れる傾斜姿勢に形
成してある遠心送風機。
5. A centrifugal blower in which a number of blades are arranged side by side in a rotating circumferential direction in a cantilevered state with respect to an impeller side plate to form an impeller, wherein a rotating part of a casing inside the impeller is provided. An inner peripheral surface of the casing that faces the outer edge of the blade in the radial direction is formed so as to be inclined away from the axis of rotation as the free end of the blade is opposite to the support side of the blade with respect to the impeller side plate. Centrifugal blower.
【請求項6】 多数の羽根を羽根車側板に対する片持ち
支持状態で回転周方向に並設して羽根車を形成してある
遠心送風機であって、 前記羽根車側板の板厚を回転軸芯側ほど大きくしてある
遠心送風機。
6. A centrifugal blower in which a number of blades are arranged side by side in a rotating circumferential direction in a cantilevered state with respect to an impeller side plate to form an impeller, wherein the plate thickness of the impeller side plate is determined by a rotation axis. Centrifugal blower enlarged toward the side.
【請求項7】 多数の羽根を羽根車側板に対する片持ち
支持状態で回転周方向に並設して羽根車を形成してある
遠心送風機であって、 前記羽根車側板に、回転軸芯近くから前記羽根車側板の
外周部にわたって回転半径方向に延びる凸条リブを回転
軸芯方向視で放射状に複数設けてある遠心送風機。
7. A centrifugal blower in which a number of blades are arranged side by side in a rotating circumferential direction in a cantilevered state with respect to an impeller side plate to form an impeller. A centrifugal blower provided with a plurality of radially extending ribs extending in a rotation radial direction over an outer peripheral portion of the impeller side plate.
【請求項8】 多数の羽根を羽根車側板に対する片持ち
支持状態で回転周方向に並設して羽根車を形成してある
遠心送風機であって、 回転軸に対する前記羽根車のボス部を、前記回転軸に対
し外嵌する内筒部と、前記羽根及び前記羽根車側板に対
する連結基部としての外筒部と、これら内筒部と外筒部
との回転軸芯方向における一端部どうしにわたらせる環
状底板部とで形成するのに、 前記環状底板部を前記羽根車側板と同一面上又はほぼ同
一面上に配置した状態で、前記内筒部及び前記外筒部を
前記環状底板部に対して、前記羽根車側板に対する前記
羽根の連設側と同じ側に位置させてある遠心送風機。
8. A centrifugal blower in which a number of blades are arranged side by side in a rotating circumferential direction in a cantilevered state with respect to an impeller side plate to form an impeller, wherein a boss portion of the impeller with respect to a rotating shaft is provided. An inner cylinder portion that fits over the rotation shaft, an outer cylinder portion as a connection base for the blades and the impeller side plate, and one end of the inner cylinder portion and the outer cylinder portion in the rotation axis center direction. The inner cylindrical portion and the outer cylindrical portion are formed on the annular bottom plate portion in a state where the annular bottom plate portion is formed on the same surface or substantially the same surface as the impeller side plate. On the other hand, a centrifugal blower located on the same side as the side where the blades are connected to the impeller side plate.
JP32206198A 1998-11-12 1998-11-12 Centrifugal blower Expired - Fee Related JP3830287B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP32206198A JP3830287B2 (en) 1998-11-12 1998-11-12 Centrifugal blower

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP32206198A JP3830287B2 (en) 1998-11-12 1998-11-12 Centrifugal blower

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JP2000145685A true JP2000145685A (en) 2000-05-26
JP3830287B2 JP3830287B2 (en) 2006-10-04

Family

ID=18139486

Family Applications (1)

Application Number Title Priority Date Filing Date
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Country Link
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006177286A (en) * 2004-12-24 2006-07-06 Matsushita Electric Ind Co Ltd Air blowing device

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JPS5461306A (en) * 1977-10-21 1979-05-17 Toshiba Corp Blower
JPS5557698A (en) * 1978-10-20 1980-04-28 Hitachi Ltd Cooling fan device
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JPS57112100U (en) * 1980-12-27 1982-07-10
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JPS6013999A (en) * 1983-07-04 1985-01-24 Matsushita Electric Ind Co Ltd Motor fan
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JPH03107348A (en) * 1989-09-14 1991-05-07 Ford Motor Co Fan for low noise cooling as well as variable speed machine
JPH03130598A (en) * 1989-10-16 1991-06-04 Eiichi Sugiura Impeller for fluid machine
JPH062698A (en) * 1992-06-18 1994-01-11 Mitsubishi Heavy Ind Ltd Centrifugal blower
JPH1037893A (en) * 1996-07-26 1998-02-13 Japan Servo Co Ltd Centrifugal fan
JPH10288196A (en) * 1997-04-16 1998-10-27 Daikin Ind Ltd Turbo fan device

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Publication number Priority date Publication date Assignee Title
JPS5034321Y1 (en) * 1970-12-28 1975-10-06
JPS5240808A (en) * 1975-09-26 1977-03-30 Toshiba Corp Fun made of plastic
JPS5457210A (en) * 1977-10-14 1979-05-08 Toshiba Corp Radial fan with rear-faced vanes
JPS5461306A (en) * 1977-10-21 1979-05-17 Toshiba Corp Blower
JPS5557698A (en) * 1978-10-20 1980-04-28 Hitachi Ltd Cooling fan device
JPS5576495U (en) * 1978-11-14 1980-05-26
JPS5740692U (en) * 1980-08-21 1982-03-04
JPS57112100U (en) * 1980-12-27 1982-07-10
JPS58195098A (en) * 1982-05-11 1983-11-14 Matsushita Electric Ind Co Ltd Vaccum cleaner
JPS6013999A (en) * 1983-07-04 1985-01-24 Matsushita Electric Ind Co Ltd Motor fan
JPH0267099U (en) * 1988-11-08 1990-05-21
JPH03107348A (en) * 1989-09-14 1991-05-07 Ford Motor Co Fan for low noise cooling as well as variable speed machine
JPH03130598A (en) * 1989-10-16 1991-06-04 Eiichi Sugiura Impeller for fluid machine
JPH062698A (en) * 1992-06-18 1994-01-11 Mitsubishi Heavy Ind Ltd Centrifugal blower
JPH1037893A (en) * 1996-07-26 1998-02-13 Japan Servo Co Ltd Centrifugal fan
JPH10288196A (en) * 1997-04-16 1998-10-27 Daikin Ind Ltd Turbo fan device

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006177286A (en) * 2004-12-24 2006-07-06 Matsushita Electric Ind Co Ltd Air blowing device

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Publication number Publication date
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