JPS6332200A - Turbo-blower - Google Patents
Turbo-blowerInfo
- Publication number
- JPS6332200A JPS6332200A JP17298086A JP17298086A JPS6332200A JP S6332200 A JPS6332200 A JP S6332200A JP 17298086 A JP17298086 A JP 17298086A JP 17298086 A JP17298086 A JP 17298086A JP S6332200 A JPS6332200 A JP S6332200A
- Authority
- JP
- Japan
- Prior art keywords
- casing
- impeller
- discharge port
- cover
- end plate
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000009423 ventilation Methods 0.000 abstract description 15
- 230000002093 peripheral effect Effects 0.000 abstract description 4
- 238000005422 blasting Methods 0.000 abstract 2
- 238000007664 blowing Methods 0.000 description 3
- 238000005266 casting Methods 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000007599 discharging Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000003110 molding sand Substances 0.000 description 1
- 125000006850 spacer group Chemical group 0.000 description 1
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
【発明の詳細な説明】
〔発明の属する技術分野〕
この発明はターボブロワにおいて、送5虱効率を向上さ
せることができるようにしたものに関する。DETAILED DESCRIPTION OF THE INVENTION [Technical Field to Which the Invention Pertains] The present invention relates to a turbo blower that is capable of improving the efficiency of the feeding section.
ターボブロワの従来例を第3図にもとづいて説明する。 A conventional example of a turbo blower will be explained based on FIG.
この図は多段プロワを示し、吐出路1を形成する円筒状
ケーンング2の両端板3,4で軸受5を介して回転軸6
が支持され、一方の端板3から突出する回転軸6の端部
Gこ中心部から吸気して外周部から径方向に排出するタ
ーボ形羽根車7が複数固着されている。この羽根車7は
それぞれ個別のカバー8.?、10で包囲され、第1段
のカバー8は端面中心部に吸込み口8aが段けられてい
る。第2段3よび第3段のカバー9.lOはそれぞれ外
側端面に整流ガイド11が複数放射状に設けられ、端面
中心部に吸込み口9 a+ 10 aが設けられてい
る。隣接する前記カバー8,9゜10は外周端部を相互
にはめ込んで結合され、最終段のカバー10は前記端板
3の外周に取付けられる。前記羽根車7は回転軸6の端
面に押えボルト12をねじ込むことにより環状押え板1
3および間隔管14.15を介して軸受5の内輪端面に
押しつけ固定され、前記整流ガイド11の軸方向先端部
には環状の画板16がその内周と間隔管14の外周との
間(こ細隙gをおいて一体形成されている。This figure shows a multi-stage blower, in which both end plates 3 and 4 of a cylindrical caning 2 forming a discharge passage 1 are connected to a rotating shaft 6 via a bearing 5.
is supported, and a plurality of turbo-type impellers 7 are fixed to an end G of a rotating shaft 6 protruding from one end plate 3, which takes in air from the center and discharges air from the outer circumference in the radial direction. The impellers 7 each have separate covers 8. ? , 10, and the first stage cover 8 has a suction port 8a arranged at the center of the end surface. 2nd stage 3 and 3rd stage covers 9. A plurality of rectifying guides 11 are provided radially on the outer end face of each IO, and a suction port 9 a + 10 a is provided at the center of the end face. Adjacent covers 8, 9 and 10 are connected by fitting their outer peripheral ends into each other, and the final stage cover 10 is attached to the outer periphery of the end plate 3. The impeller 7 is attached to the annular holding plate 1 by screwing a holding bolt 12 into the end face of the rotating shaft 6.
3 and spacer tubes 14 and 15 to the inner ring end surface of the bearing 5, and an annular drawing plate 16 is provided at the axial tip of the rectifying guide 11 between its inner periphery and the outer periphery of the spacing tube 14. They are integrally formed with a gap g between them.
前記プロワは回転軸6の回転蚤こ伴う羽根車7の作用で
吸込み口8aがら空気を吸入し、第1段の羽根車7で加
圧して外周部から排出した空気は隣接する整流ガイド1
1により中心部に向かって送り込まれる。この空気は第
2段のカバー9の吸込み口9aから羽根車7の作用で吸
入し【さらに加圧され、この加圧を繰り返し最終的に高
圧空気となって前記吐出路1を通りケーシング2の外周
部に設けた吐出口17から送り出される。The blower sucks air through the suction port 8a by the action of the impeller 7 as the rotary shaft 6 rotates, and the air pressurized by the first stage impeller 7 and discharged from the outer circumferential portion flows into the adjacent rectifying guide 1.
1, it is sent toward the center. This air is sucked in through the suction port 9a of the second stage cover 9 by the action of the impeller 7, is further pressurized, and this pressurization is repeated until it becomes high-pressure air, passes through the discharge passage 1, and is heated to the casing 2. It is sent out from a discharge port 17 provided on the outer periphery.
このような構造では最終段の羽根車7の外周部から吐出
路1に送り込まれる高圧空気が端板3の外周部付近で急
激にほぼ1800転回しこれに伴って大きな圧力損失を
生じるので送風効率が低下するという欠点があった。In such a structure, the high-pressure air sent into the discharge passage 1 from the outer periphery of the final stage impeller 7 suddenly turns around 1800° near the outer periphery of the end plate 3, resulting in a large pressure loss, which reduces the blowing efficiency. The disadvantage was that it decreased.
この発明は前記の欠点を除去するためそこ、送風効率を
向上させることができるようにしたターボブロワを提供
することを目的とする。SUMMARY OF THE INVENTION In order to eliminate the above-mentioned drawbacks, it is an object of the present invention to provide a turbo blower that can improve air blowing efficiency.
〔発明の要点〕
この発明は前記の目的を達成するために、円筒状ゲージ
ングの羽根車を包囲するカバーの取付は部(こ隣接する
羽根車外周部とケーシング÷こ設け1こ吐出口とを連通
ずる渦巻き形通風路を円周方向にほぼ一周させかつ断面
積を漸増させて形成するようにしたものである。[Summary of the Invention] In order to achieve the above-mentioned object, the present invention installs a cover that surrounds a cylindrical gauging impeller by dividing the outer periphery of the adjacent impeller and the casing by one discharging port. The communicating spiral ventilation passage is formed by making approximately one turn in the circumferential direction and gradually increasing the cross-sectional area.
第1図および第2図はこの発明の実施例を示すもので、
第3図と同一符号で示すものは同一部品である。この図
において、円筒状ケーシング22の両端板23.24で
回転軸6が支持され、一方の端板23の外周に羽根車7
を包囲するカバー10が取付けられている。端板23の
カバー取付は部には隣接する羽根車7の外周部とケーシ
ング22の外周部に接線方向に設けた吐出口27とを連
通ずる渦巻き形通風路21が円周方向にほぼ一周して形
成され、その断面積は吐出口27に向かって通風方向に
漸増するよう(こなっている。前記通風路21の断面形
状はほぼ三角形をなし、羽根車7の外周部から、径方向
に排出した高圧空気を転回しながら通風路211こ導入
する開口部21aが外周側に設けられている。この開口
部21aは端板23の外周に取付けたカバー10で覆わ
れ、通風路21の前記高圧空気の転回部は急激な転回を
避けるために適当な角度αで斜めに形成されている。こ
の傾斜面は湾曲面でも差し支えない。前記ケーシング2
2と端板23は鋳物等で一体形成される。FIG. 1 and FIG. 2 show an embodiment of this invention.
Components designated by the same reference numerals as in FIG. 3 are the same parts. In this figure, a rotating shaft 6 is supported by both end plates 23 and 24 of a cylindrical casing 22, and an impeller 7 is attached to the outer periphery of one end plate 23.
A cover 10 is attached to surround the. When attaching the cover to the end plate 23, the spiral air passage 21 that connects the outer periphery of the adjacent impeller 7 and the discharge port 27 provided tangentially on the outer periphery of the casing 22 goes around the circumferential direction almost once. The cross-sectional area of the ventilation passage 21 gradually increases in the ventilation direction toward the discharge port 27. An opening 21a is provided on the outer circumferential side through which the discharged high-pressure air is introduced into the ventilation passage 211 while being rotated.This opening 21a is covered with a cover 10 attached to the outer circumference of the end plate 23, and The high-pressure air turning section is formed obliquely at an appropriate angle α to avoid sudden turning.This inclined surface may be a curved surface.The casing 2
2 and the end plate 23 are integrally formed by casting or the like.
前記実施例によれば羽根車7の外周部から排出した高圧
空気は通風方向に断面積の漸増する通風路21に円周方
向にほぼ一周する間に順次送り込まれて合流するので通
風抵抗を減らすことができ、また羽根車7から径方向に
排出した高圧空気の転回角度はほぼ90° となるので
転回を二伴う圧力損失を従来例で説明したものよりほぼ
半減して送風効率を向上させることができる。前記通風
路21は開口部21aが外周部(こ大きく設けられてい
るのでケーシング22と端板23を鋳物で一体形成する
lp Hこ鋳物砂の除去作業を容易に行うことができる
。According to the embodiment, the high-pressure air discharged from the outer periphery of the impeller 7 is sequentially fed into the ventilation passage 21 whose cross-sectional area gradually increases in the ventilation direction and merges therewith while making approximately one circumference in the circumferential direction, thereby reducing ventilation resistance. In addition, since the turning angle of the high-pressure air discharged radially from the impeller 7 is approximately 90°, the pressure loss caused by the turning is reduced by almost half compared to that described in the conventional example, and the blowing efficiency is improved. Can be done. Since the opening 21a of the ventilation passage 21 is larger than the outer periphery, the casing 22 and the end plate 23 are integrally formed by casting, so that it is possible to easily remove the molding sand.
この発明によればターボブロワにおいて、円筒状ゲージ
ングの羽根車を包囲するカバーの取付は部(こ隣接する
羽根車外周部とケーシングに設けた吐出口とを連通ずる
渦巻き形通風路を円周方向に(土ぼ一周させかつ断面積
を漸増させて形成するようにしたので、通風抵抗および
高圧空気の通風方向転回に伴う圧力損失を減らして送風
効率を向上させることがでさるという効果が得られる。According to the present invention, in the turbo blower, the cover surrounding the cylindrical gauging impeller is installed in the circumferential direction of the spiral air passage that communicates the outer periphery of the adjacent impeller with the discharge port provided in the casing. (Since the earthen pot is formed so as to go around it and gradually increase the cross-sectional area, it is possible to reduce ventilation resistance and pressure loss due to rotation of the ventilation direction of high-pressure air, thereby improving ventilation efficiency.
第1図はこの発明の実施例の縦断面図、第2図は第1図
の■−■線に沿う縦断面図、第3図は従来例の縦断面図
である。
6・・・回転軸、7・・・羽根車、10・・・カバー、
10a・・・吸込み口、21・・・通風路、22・・・
ケーシング、23.24・・・端板、27・・・吐出口
。
be人−#d士当山口云゛FIG. 1 is a longitudinal sectional view of an embodiment of the present invention, FIG. 2 is a longitudinal sectional view taken along the line -■ in FIG. 1, and FIG. 3 is a longitudinal sectional view of a conventional example. 6... Rotating shaft, 7... Impeller, 10... Cover,
10a... Suction port, 21... Ventilation path, 22...
Casing, 23.24... End plate, 27... Discharge port. Be person - #d Shito Yamaguchi Yuu
Claims (1)
を支持するとともに、端板から突出する回転軸の端部に
ターボ形羽根車を取付け、この羽根車を包囲してケーシ
ングに取付けたカバーの中心部に吸込み口を設けてなる
ターボブロワにおいて、前記ケーシングのカバー取付け
部に隣接する羽根車外周部と吐出口を連通する渦巻き形
通風路を円周方向にほぼ一周させかつ断面積を漸増させ
て形成したことを特徴とするターボブロワ。1) A rotating shaft is supported by both end plates of a cylindrical casing having a discharge port, a turbo-type impeller is attached to the end of the rotating shaft protruding from the end plate, and a cover is attached to the casing to surround this impeller. In a turbo blower having a suction port provided in the center of the casing, a spiral air passage communicating the discharge port with the outer circumferential portion of the impeller adjacent to the cover attachment portion of the casing is arranged around one circumference in the circumferential direction and has a cross-sectional area that gradually increases. A turbo blower characterized by being formed by
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP17298086A JPH0680319B2 (en) | 1986-07-23 | 1986-07-23 | Turbo blower |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP17298086A JPH0680319B2 (en) | 1986-07-23 | 1986-07-23 | Turbo blower |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS6332200A true JPS6332200A (en) | 1988-02-10 |
JPH0680319B2 JPH0680319B2 (en) | 1994-10-12 |
Family
ID=15951935
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP17298086A Expired - Lifetime JPH0680319B2 (en) | 1986-07-23 | 1986-07-23 | Turbo blower |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPH0680319B2 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009008298A (en) * | 2007-06-27 | 2009-01-15 | Hitachi Appliances Inc | Heating cooker |
-
1986
- 1986-07-23 JP JP17298086A patent/JPH0680319B2/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2009008298A (en) * | 2007-06-27 | 2009-01-15 | Hitachi Appliances Inc | Heating cooker |
Also Published As
Publication number | Publication date |
---|---|
JPH0680319B2 (en) | 1994-10-12 |
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