JPH0634198U - Blower or compressor - Google Patents

Blower or compressor

Info

Publication number
JPH0634198U
JPH0634198U JP6985192U JP6985192U JPH0634198U JP H0634198 U JPH0634198 U JP H0634198U JP 6985192 U JP6985192 U JP 6985192U JP 6985192 U JP6985192 U JP 6985192U JP H0634198 U JPH0634198 U JP H0634198U
Authority
JP
Japan
Prior art keywords
flow
nozzle
flow guide
impeller
compressor
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
JP6985192U
Other languages
Japanese (ja)
Other versions
JP2534592Y2 (en
Inventor
弘高 東森
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 Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP6985192U priority Critical patent/JP2534592Y2/en
Publication of JPH0634198U publication Critical patent/JPH0634198U/en
Application granted granted Critical
Publication of JP2534592Y2 publication Critical patent/JP2534592Y2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

(57)【要約】 【目的】 遠心送風機または遠心圧縮機において、イン
レットガイドベーンを廃し、しかも羽根車入口流れに旋
回を与えること。 【構成】 フローガイド(10)の両側、すなわちスク
ロール内(16)と羽根車入口(17)の差圧を利用
し、フローガイド(10)に開孔(11)を明けるとと
もに、接線方向に傾斜したノズル流路(13)を有する
ノズルリング(12)を開孔(11)の外側に設け、ス
クロール内(16)の気体を旋回させて羽根車入口(1
7)に導く。旋回の強さは、ノズルリング(12)を回
動して調節する。
(57) [Summary] [Purpose] To eliminate the inlet guide vanes in a centrifugal blower or centrifugal compressor and to impart swirl to the impeller inlet flow. [Composition] By utilizing the pressure difference between the both sides of the flow guide (10), that is, the inside of the scroll (16) and the impeller inlet (17), an opening (11) is opened in the flow guide (10) and it is inclined tangentially. The nozzle ring (12) having the nozzle flow channel (13) is provided outside the opening (11), and the gas in the scroll (16) is swirled to make the impeller inlet (1
Lead to 7). The swirl strength is adjusted by rotating the nozzle ring (12).

Description

【考案の詳細な説明】[Detailed description of the device]

【0001】[0001]

【産業上の利用分野】[Industrial applications]

本考案は遠心送風機または遠心圧縮機に適用される。 The present invention is applied to a centrifugal blower or a centrifugal compressor.

【0002】[0002]

【従来の技術】[Prior art]

図3は従来の遠心送風機の一例を示す縦断面図である。従来はフローガイド( 20)の内側にインレットガイドベーン(21)を設け、このインレットガイド ベーンの取付角を変えることにより羽根車(22)に吸込まれる流れに予旋回を 与えて、送風機または圧縮機の流量,圧力を調整していた。 FIG. 3 is a vertical sectional view showing an example of a conventional centrifugal blower. Conventionally, an inlet guide vane (21) is provided inside the flow guide (20), and by changing the mounting angle of the inlet guide vane, a pre-swirl is given to the flow sucked into the impeller (22), so that the blower or the compressor is compressed. The flow rate and pressure of the machine were adjusted.

【0003】[0003]

【考案が解決しようとする課題】[Problems to be solved by the device]

前記従来の遠心送風機等には次のような解決すべき課題があった。 インレットガイドベーン(21)を流れが通過するとき圧損が生じ、インレ ットガイドベーン(21)が無い場合に比べて効率が最小でも1〜2%低下する 。 インレットガイドベーン(21)はベーン(23),ボス(24),リンク 機構(25)を有し重量が大きいこと、特に両吸込形の遠心ファンの場合には、 これらを両方の軸受の内側に設けるため軸長が長くなり、羽根車・軸から成る回 転部の重量が重くなるだけでなく、支持構造重量も重くなり、遠心送風機全体の 重量が増加する。 The conventional centrifugal blower and the like have the following problems to be solved. When the flow passes through the inlet guide vanes (21), pressure loss occurs, and efficiency is reduced by at least 1 to 2% as compared with the case without the inlet guide vanes (21). The inlet guide vane (21) has a vane (23), a boss (24), and a link mechanism (25) and has a large weight. Especially, in the case of a double-suction type centrifugal fan, these are installed inside both bearings. Since the shaft length becomes longer due to the provision, not only the rotating part consisting of the impeller and the shaft becomes heavier, but also the weight of the supporting structure becomes heavier, and the total weight of the centrifugal fan increases.

【0004】[0004]

【課題を解決するための手段】[Means for Solving the Problems]

本考案は、前記従来の課題を解決するために、羽根車,スクロールおよびフロ ーガイドを具えた遠心式の送風機または圧縮機において、上記フローガイドには 円周方向に沿って等間隔に複数の開孔が明けられ、同開孔の外側に上記フローガ イドの壁面に沿って円周方向に回動できるノズルリングが設けられるとともに、 同ノズルリングは上記開孔と同数のノズル流路が円周方向に沿って等間隔に明け られ、かつ同ノズル流路の方向は上記羽根車の回転軸線を含む平面に対して傾斜 していることを特徴とする送風機または圧縮機を提案するものである。 In order to solve the above-mentioned conventional problems, the present invention provides a centrifugal blower or compressor having an impeller, a scroll and a flow guide, wherein the flow guide has a plurality of openings at equal intervals along the circumferential direction. A hole is opened, and a nozzle ring that can rotate in the circumferential direction along the wall surface of the flow guide is provided outside the opening, and the nozzle ring has the same number of nozzle channels as the openings in the circumferential direction. The present invention proposes a blower or a compressor characterized in that the nozzle channels are opened at equal intervals and the direction of the nozzle flow channel is inclined with respect to the plane including the rotation axis of the impeller.

【0005】[0005]

【作用】[Action]

本考案においては、吸込流れの中に構造物が無いので、損失の発生を防止でき る。特にインレットガイドベーンを有する両吸込遠心送風機の場合には、軸受位 置に制約が少なくなり軽量化できる。 In the present invention, since there is no structure in the suction flow, loss can be prevented. In particular, in the case of a double suction centrifugal blower having an inlet guide vane, there are less restrictions on the bearing position and the weight can be reduced.

【0006】[0006]

【実施例】【Example】

図1は本考案の一実施例を示す縦断面図,図2は図1のII−II断面図である。 本実施例では、フローガイド(10)に円周方向に沿って等間隔に複数の開孔( 11)を設け、その外側にフローガイド(10)の壁面に沿って周方向に回動で きるノズルリング(12)を設けている。このノズルリング(12)には、上記 開孔(11)と同数のノズル流路(13)とノズル壁(14)が設けられている 。そして、それらノズル流路(13)の方向は羽根車(22)の回転軸線を含む 平面に対して傾斜している。このノズル壁(14)の内側はフローガイド(10 )に接しているので、このノズルリング(12)を回動してノズル流路(13) を図2(b)に示されるようにフローガイドの開孔(11)に重ねると、スクロ ール(16)内から羽根車(22)入口(17)に至る流れ(15)が生じる。 そうすると、ノズル流路(13)の方向が、回転軸線を含む平面に対して傾斜し ているので、羽根車(22)入口(17)の流れに旋回流を与えることができる 。またノズル壁(14)を図2(a)に示されるようにフローガイドの開孔(1 1)に重ねると、開孔が閉鎖される。またノズル流路(13)は図1に示される ように軸方向への傾斜を持っているので、旋回しながら羽根車(22)に向う流 れを生じさせることができる。 1 is a vertical sectional view showing an embodiment of the present invention, and FIG. 2 is a sectional view taken along line II-II of FIG. In this embodiment, the flow guide (10) is provided with a plurality of apertures (11) at equal intervals along the circumferential direction, and can be rotated in the circumferential direction along the wall surface of the flow guide (10) outside thereof. A nozzle ring (12) is provided. The nozzle ring (12) is provided with the same number of nozzle channels (13) and nozzle walls (14) as the openings (11). The directions of the nozzle channels (13) are inclined with respect to the plane including the rotation axis of the impeller (22). Since the inside of the nozzle wall (14) is in contact with the flow guide (10), the nozzle ring (12) is rotated to move the nozzle channel (13) to the flow guide as shown in FIG. 2 (b). When it is superposed on the opening (11), the flow (15) from the inside of the scroll (16) to the inlet (17) of the impeller (22) is generated. Then, since the direction of the nozzle flow path (13) is inclined with respect to the plane including the rotation axis, a swirl flow can be given to the flow at the inlet (17) of the impeller (22). When the nozzle wall (14) is overlapped with the opening (11) of the flow guide as shown in FIG. 2 (a), the opening is closed. Further, since the nozzle flow path (13) has an inclination in the axial direction as shown in FIG. 1, it is possible to generate a flow toward the impeller (22) while turning.

【0007】 従来のインレットガイドベーン(21)に代わる予旋回発生装置として、送風 機や圧縮機の吐出圧または別の圧力源からの空気またはガスをフローガイドの円 周方向に噴出し羽根車入口の流れに予旋回を生じさせるアイデアは、従来より考 案されていたが、本実施例は、遠心送風機または遠心圧縮機のスクロールとフロ ーガイドの差圧を利用して、フローガイド内側の吸込流れに予旋回を与える構造 としたものである。As a pre-swirling generator that replaces the conventional inlet guide vane (21), air or gas from the discharge pressure of a blower or compressor or another pressure source is jetted in the circumferential direction of the flow guide to impeller inlet. The idea of causing a pre-swirl in the flow of air has been conventionally considered, but in this embodiment, the suction flow inside the flow guide is used by utilizing the differential pressure between the scroll of the centrifugal blower or the centrifugal compressor and the flow guide. It has a structure that gives a pre-turning to the.

【0008】[0008]

【考案の効果】[Effect of device]

本考案によれば、インレットガイドベーンを用いることなく、遠心送風機,遠 心圧縮機の吸込流れに予旋回を与えることができる。そして、開孔面積の調整に よりその予旋回流の強さを調整できる。 According to the present invention, a pre-swirl can be given to the suction flow of a centrifugal blower or a centrifugal compressor without using an inlet guide vane. The strength of the pre-swirl flow can be adjusted by adjusting the area of the opening.

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

【図1】図1は本考案の一実施例を示す縦断面図であ
る。
FIG. 1 is a longitudinal sectional view showing an embodiment of the present invention.

【図2】図2は図1のII−II断面図である。FIG. 2 is a sectional view taken along line II-II of FIG.

【図3】図3は従来の遠心送風機の一例を示す縦断面図
である。
FIG. 3 is a vertical cross-sectional view showing an example of a conventional centrifugal blower.

【符号の説明】[Explanation of symbols]

(10) フローガイド (11) 開孔 (12) ノズルリング (13) ノズル流路 (14) ノズル壁 (16) スクロール (22) 羽根車 (10) Flow guide (11) Open hole (12) Nozzle ring (13) Nozzle flow path (14) Nozzle wall (16) Scroll (22) Impeller

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 【請求項1】 羽根車,スクロールおよびフローガイド
を具えた遠心式の送風機または圧縮機において、上記フ
ローガイドには円周方向に沿って等間隔に複数の開孔が
明けられ、同開孔の外側に上記フローガイドの壁面に沿
って円周方向に回動できるノズルリングが設けられると
ともに、同ノズルリングには上記開孔と同数のノズル流
路が円周方向に沿って等間隔に明けられ、かつ同ノズル
流路の方向は上記羽根車の回転軸線を含む平面に対して
傾斜していることを特徴とする送風機または圧縮機。
1. A centrifugal blower or compressor provided with an impeller, a scroll and a flow guide, wherein the flow guide is provided with a plurality of holes at equal intervals along the circumferential direction. A nozzle ring that can be rotated in the circumferential direction along the wall surface of the flow guide is provided on the outside, and the same number of nozzle channels as the openings are opened in the nozzle ring at equal intervals along the circumferential direction. The blower or compressor is characterized in that the direction of the nozzle flow path is inclined with respect to a plane including the rotation axis of the impeller.
JP6985192U 1992-10-07 1992-10-07 Blower or compressor Expired - Fee Related JP2534592Y2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6985192U JP2534592Y2 (en) 1992-10-07 1992-10-07 Blower or compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6985192U JP2534592Y2 (en) 1992-10-07 1992-10-07 Blower or compressor

Publications (2)

Publication Number Publication Date
JPH0634198U true JPH0634198U (en) 1994-05-06
JP2534592Y2 JP2534592Y2 (en) 1997-04-30

Family

ID=13414734

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6985192U Expired - Fee Related JP2534592Y2 (en) 1992-10-07 1992-10-07 Blower or compressor

Country Status (1)

Country Link
JP (1) JP2534592Y2 (en)

Also Published As

Publication number Publication date
JP2534592Y2 (en) 1997-04-30

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Legal Events

Date Code Title Description
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 19961126

LAPS Cancellation because of no payment of annual fees