JPS6018243A - Production of hollow vane - Google Patents
Production of hollow vaneInfo
- Publication number
- JPS6018243A JPS6018243A JP12743783A JP12743783A JPS6018243A JP S6018243 A JPS6018243 A JP S6018243A JP 12743783 A JP12743783 A JP 12743783A JP 12743783 A JP12743783 A JP 12743783A JP S6018243 A JPS6018243 A JP S6018243A
- Authority
- JP
- Japan
- Prior art keywords
- hollow
- vane
- plate
- wing
- reinforcing ribs
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/78—Making other particular articles propeller blades; turbine blades
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
【発明の詳細な説明】
(産業上の利用分野〉
本発明は、遠心式送風機のロータ羽根に使用される中空
翼の製造方法に関Jるものである。DETAILED DESCRIPTION OF THE INVENTION (Industrial Field of Application) The present invention relates to a method of manufacturing a hollow blade used for a rotor blade of a centrifugal blower.
〈従来技術)
従来、遠心式送風機にJノいては、軽量化を図る見地よ
りそのロータ羽根として、例えば第1図に示づように、
所定形状の翼面を形成Jる中空翼膜(a )と、該中空
翼膜(a)に内挿入固着された補強部材(1))とから
なる中空翼(c)が使用されている(特公昭b 2−4
7567 @公報等参照)しかるに、従来、このにうな
中空R(C)を金属製で製造する場合、中空翼膜<a
>を所定の中空形状に成形した後、該中空翼膜(a )
に対して補強部材(b)を挿入し溶接により固着力ると
いう方法で形成することが行われていた。そのため、特
に中空翼(C)の翼厚が博い(10mm程1′a)場合
には、補強部材(b)の溶接作業が困ツ「となり、作業
性に欠けるという問題があった。<Prior Art> Conventionally, in order to reduce the weight of a centrifugal blower, the rotor blades were used as shown in Fig. 1, for example.
A hollow wing (c) is used, which consists of a hollow wing membrane (a) forming a wing surface of a predetermined shape, and a reinforcing member (1) inserted and fixed into the hollow wing membrane (a). Special public show b 2-4
7567 @Refer to publications, etc.) However, conventionally, when manufacturing this hollow R (C) from metal, the hollow blade membrane < a
> is formed into a predetermined hollow shape, the hollow blade membrane (a)
The conventional method was to insert a reinforcing member (b) into the reinforcing member and fix it by welding. Therefore, especially when the thickness of the hollow blade (C) is large (approximately 10 mm 1'a), welding of the reinforcing member (b) becomes difficult, resulting in a problem of poor workability.
尚、前記記載の公報には、中空翼膜(a)lI3よび補
強部材(b)の外周部を合成樹脂で構成覆ることにより
、その合成樹脂の特性(未硬化合成樹脂の粘着性)を利
用して補強部材(b)を、溶接を要することなく中空翼
膜(a )内に固るし1[するようにした方法が開示さ
れている。しかし、中空m殻(a )等を合成樹脂で構
成した中空翼(c )は、金属で構成したものに比べ中
空閃殻(a )の表面が必然的に粗くなるため、空気抵
抗が大きくなるという不具合があり、また強度的にも難
点があっC1実用性に欠()る嫌いがある。In addition, the above-mentioned publication states that by covering the outer periphery of the hollow wing membrane (a) lI3 and the reinforcing member (b) with a synthetic resin, the characteristics of the synthetic resin (the tackiness of the uncured synthetic resin) are utilized. A method is disclosed in which the reinforcing member (b) is consolidated into the hollow blade membrane (a) without the need for welding. However, in hollow blades (c) whose hollow m-shells (a) etc. are made of synthetic resin, the surface of the hollow m-shells (a) is inevitably rougher than those made of metal, resulting in greater air resistance. There are problems such as this, and there are also drawbacks in terms of strength, making C1 impractical.
(ざt明の目的)
本発明の目的は、前)!lSの如き中空翼の製造におい
て、中空製膜に対Jる補強部材の付設を、中空製膜を所
定の中空形状に形成した後ではなくその前に行うことに
より、作業性の向上を図るものである。(Objective of the present invention) The object of the present invention is the previous)! In the manufacture of hollow blades such as IS, work efficiency is improved by attaching reinforcing members to the hollow membrane before forming the hollow membrane into a predetermined hollow shape, instead of after forming the hollow membrane into a predetermined hollow shape. It is.
(発明の構成)
前記目的を達成するlcめ、本発明の構成は、プレス加
工により中空翼の翼面を展間した形状に形成された翼面
展開板を用意し、該翼面展間板に補強リブを形成した後
、該補強リブ形成側を内側にし−C翼面展間板を所定形
状の翼面を形成するように2つに折り曲げ、該翼面展開
板の折り曲げ自由端同士を溶接により互いに接合して中
空翼を形成するものである。このことにより、前記翼面
展間板の折り曲げ成形後つまり中空翼殻形成後に該中空
製膜に対して補強リブの溶接固着作業を要することなく
、中空翼殻内に補強リブを予め設は得るようにしたもの
である。(Structure of the Invention) To achieve the above-mentioned object, the structure of the present invention is to prepare a wing surface expansion plate formed in a shape in which the wing surface of a hollow wing is expanded by press working, and to After forming the reinforcing ribs on the side, bend the -C wing surface expansion plate in two so as to form a wing surface of a predetermined shape, with the reinforcing rib forming side facing inside, and fold the bent free ends of the wing surface expansion plates together. They are joined together by welding to form a hollow blade. As a result, reinforcing ribs can be provided in the hollow wing shell in advance without requiring welding and fixing of the reinforcing ribs to the hollow film after the bending and forming of the wing surface plate, that is, after the formation of the hollow wing shell. This is how it was done.
(発明の効果)
したがって、本発明にJ:れば、中空翼殻形成後に該中
空製膜に対づる補強リブの溶接固着作業を要することな
く、中空翼殻内に補強リブを予め設けることができるの
で、補強リブにより中空シフ酸を有効に補強して中空翼
の強度を増大さUながら、作業の容易化により作業性の
向上を図ることがでさるものである。(Effects of the Invention) Therefore, according to the present invention, reinforcing ribs can be provided in advance in the hollow wing shell without requiring welding and fixing of the reinforcing ribs to the hollow membrane after the formation of the hollow wing shell. Therefore, the reinforcing ribs can effectively reinforce the hollow Schiff acid to increase the strength of the hollow blade, and at the same time, it is possible to improve the workability by making the work easier.
〈実施例)
以下、本発明の技術的手段の具体例としの実施例を図面
により説明する。<Example> Hereinafter, an example as a specific example of the technical means of the present invention will be described with reference to the drawings.
第2図および第3図は遠心式送風機のロータ(A>を示
し、このロータ(A)は、駆動モータの駆動軸(図示「
ず)に取付部材(1)を介して装着される円形状のプレ
ート(2)と、該プレート(2)の−側面に円周方向に
等ピッチでもって立設されたロータ羽根としての多数の
中空翼(3)、<3)、・・・とを備え、エアをプレー
ト(2)の前プ)より吸入して外局方向に加速噴出Jる
ものである。Figures 2 and 3 show the rotor (A) of a centrifugal blower, and this rotor (A) is connected to the drive shaft of the drive motor (
A circular plate (2) is attached to the plate (2) via a mounting member (1), and a large number of rotor blades are installed on the side surface of the plate (2) at equal pitches in the circumferential direction. It is equipped with hollow blades (3), <3), .
前記各中空翼(3)は、第4図に詳示するように翼面を
形成するアルミニウム合金等の金属からなる中空製膜(
4)内に該中空製膜(4)を補強するための補強リブ(
5)、(5)を有している。Each of the hollow blades (3) is made of a hollow film (made of metal such as aluminum alloy) that forms the blade surface, as shown in detail in FIG.
4) Reinforcing ribs (4) for reinforcing the hollow membrane (4)
5) and (5).
また、各中空翼(3)の取付基端部および先端部は、そ
れぞれプレー1〜(2)およびリング(7)に設()た
嵌合孔(6)、(6’ )に嵌合され外面全周溶接(×
)により固着されている。In addition, the mounting base end and tip end of each hollow wing (3) are fitted into the fitting holes (6) and (6') provided in the plays 1 to (2) and the ring (7), respectively. Welded all around the outer surface (×
) is fixed.
次に、本発明の第1実施例としての前記中空翼(3)の
製造方法を第5図により説明する。Next, a method of manufacturing the hollow blade (3) as a first embodiment of the present invention will be explained with reference to FIG.
づなわち、中空翼(3)を製造する場合には、先ず、第
5図(a)に示づ如く上型(d+)ど下型(d2)とを
備えたプレスMfiff(D>により金属板(8)をプ
レスして翼面展間板(9)を形成づる。この翼面展間板
(9)は、中空間膜(4)の後縁を切り離して展開した
形状であって、その路中央部に中空製膜(4)の110
縁に相応づる段部(9a)を有し、また該段部(9a)
の両側方の所定位置に断面逆U字状に湾曲した突出部(
9b)、(9G)を有している。That is, when manufacturing the hollow blade (3), first, as shown in FIG. The plate (8) is pressed to form a wing plate (9).The wing plate (9) has a shape in which the trailing edge of the hollow space membrane (4) is separated and expanded, 110 of the hollow membrane (4) in the center of the path
The edge has a corresponding step (9a), and the step (9a)
A protrusion (with an inverted U-shaped cross section) is placed at a predetermined position on both sides of the
9b) and (9G).
続いて、前記翼面展間板(9)の各突出部(9b)、(
9c)を、上記プレス装置(I〕)とは別のプレス装@
(図示せず)によりそれぞれ両側壁を挾むようにプレス
し、該両側壁を溶接にJ、り固着することにより、四面
展開板く9)上に補強リブ(5)、(5)を突出した状
態に形成する(第5図(b)参照)。Subsequently, each protrusion (9b), (
9c) in a press equipment different from the above-mentioned press equipment (I)
(not shown), and by welding and fixing the both side walls, the reinforcing ribs (5), (5) are projected on the four-sided expansion plate 9). (see FIG. 5(b)).
しかる後、前記補強リブ(5)、(5)形成側を内側に
し、また段部(9a)を折曲げ中心部として四面展開板
(9)を中空製膜(4)を形成刃るように2つに折り曲
げ、該翼面展間板(9)の折曲げ自由端(中空製膜(4
)の後縁)同士を溶接により互いに接合する(第5図(
C)参照)。After that, the reinforcing ribs (5), (5) are formed on the inner side, and the four-sided expansion plate (9) is bent to form the hollow film (4) with the stepped portion (9a) as the center. Bend it in two, and open the bent free end (hollow film-forming (4) of the wing surface spreading plate (9)
) are joined to each other by welding (see Figure 5 (
See C).
以上によって、中空製膜(4)内に補強リブ(5)、(
5)を有してなる中空翼(3)が形成される。As a result of the above, the reinforcing ribs (5), (
5) is formed.
尚、前記補強リブ(5)、(5)は、中空製膜(4〉内
において中空翼(3)の長さ方向にメフレットされ、ま
た先端が中空IM殻(4)内面に所定の間隙を隔てて対
向JるJ、うに設定されていて、中空翼(3)が熱膨張
したときでも該補強リブ(5)、(5)によって中空内
殻(4)が変形するのを防止Jるようにしている。The reinforcing ribs (5), (5) are meshed in the length direction of the hollow blade (3) within the hollow membrane (4), and the tips are formed with a predetermined gap on the inner surface of the hollow IM shell (4). The reinforcing ribs (5), (5) prevent the hollow inner shell (4) from deforming even when the hollow blade (3) thermally expands. I have to.
したがって、このような中空翼(3)の製造方法によれ
ば、翼面展間板(9)を折り曲げて中空内殻(4)を成
形Jる前に該内面展開板(9)に補強リブ(5)、(5
)を予め形成しておくだけで、中空内殻(4)の成形後
には該中空翼M(4)内に補強リブ(5)、(5)を有
する中空翼く3)を形成づることができ、従来の如く中
空内殻(4)の成形後に該中空内殻(4〉内に補強部材
を挿入し溶接により固着する必要がないので、中空翼〈
3)の翼厚が薄い場合でも中空翼(3)の製造作業を簡
単に行うことができる。Therefore, according to the manufacturing method of the hollow wing (3), before the wing surface spreading plate (9) is bent to form the hollow inner shell (4), reinforcing ribs are added to the inner surface spreading plate (9). (5), (5
) can be formed in advance, and after molding the hollow inner shell (4), it is possible to form the hollow wing 3) having the reinforcing ribs (5), (5) inside the hollow wing M(4). Since it is not necessary to insert a reinforcing member into the hollow inner shell (4) and fix it by welding after molding the hollow inner shell (4) as in the conventional case, the hollow wing
Even when the thickness of the blade (3) is thin, the manufacturing operation of the hollow blade (3) can be easily performed.
しかも、前記中空n殻(4)の成形前における補強リブ
(5)、(5)の成形は、翼面展間板(9)を形成する
際のプレス加工によって同時に形成した各突出部(9b
) 、(9c )をその両側壁を挾/υでプレスし、
溶接により固着するという簡単なものであるので、作業
性の向−りを一層図ることができる。Moreover, the reinforcing ribs (5), (5) are formed before forming the hollow N-shell (4), while the respective protrusions (9b
), (9c) is pressed on both sides with a scissor /υ,
Since it is simply fixed by welding, workability can be further improved.
その上、前記中空翼(3)は、中空内殻〈4)がその内
側の補強リブ(5)、(5)によって有効に補強されて
強度が増大され−Cいるので、強度性a5よび耐久性等
の向上を図ることができる。Moreover, since the hollow inner shell (4) is effectively reinforced by the reinforcing ribs (5), (5) inside the hollow wing (3), the strength is increased. It is possible to improve sexual performance, etc.
第6図および第7図はそれぞれ本発明の第2および第3
実施例としての中空翼(3)の製造方法を示づもので、
これらの製造方法は、プレス加工により中空内殻(4)
を展開した形状に形成された同面展間板(9′ )上に
断面り字状の補強リブ(5’ )、(5’ )を溶接に
より固着した後、該翼面展間板(9′)を折り曲げて中
空内殻(4′ )内に補強リブ(5’ )、(5’ )
を有してなる中空R(3’)を形成覆るようにしたもの
である。6 and 7 are the second and third embodiments of the present invention, respectively.
This shows a method for manufacturing a hollow blade (3) as an example,
These manufacturing methods involve forming a hollow inner shell (4) by press working.
After welding reinforcing ribs (5'), (5') having a cross-sectional shape on the same plane plate (9') formed in the expanded shape of the wing plate (9'), ′) is bent and reinforcing ribs (5′) and (5′) are placed inside the hollow inner shell (4′).
A hollow R (3') is formed and covered.
ここで、前記中空内殻(4′ 〉内の補強リフ(5’)
、(5’)は、第2実施例では互いに内側を向は合うよ
うに設定され(第6図(C−)参照)、第3実施例では
互いに外側を向【プ合うつまり背中合わせになるように
設定されている〈第7図(C)参照)。また、これらの
製造方法による場合にも、前記第1実施例と同様の作用
効果を奏Jることができるのは勿論である。Here, the reinforcing rift (5') inside the hollow inner shell (4')
, (5') are set so that they face each other inwardly in the second embodiment (see FIG. 6 (C-)), and in the third embodiment, they are set so that they face each other outwardly, that is, back to back. (See Figure 7(C)). Furthermore, it goes without saying that the same effects as in the first embodiment can also be achieved using these manufacturing methods.
第1図は従来例としての中空翼の断面図であり、第2図
ないし第7図は本発明の実施例を示すもので、第2図は
遠心式送Igi機のロータを示す平面図、第3図は同断
面図、m4図は中空内の断面図であり、第5図ないし第
7図はそれぞれ第1ないし第3実施例としての中空翼の
WA造方法を示J−製造工程図である。
(3)・・・中空翼、(5)、(5’ )・・・補強リ
ブ、(9)、<9’ )・・・翼面展間板。
始1図
O
第2図
拍4図
第3図Fig. 1 is a sectional view of a hollow blade as a conventional example, Figs. 2 to 7 show embodiments of the present invention, and Fig. 2 is a plan view showing a rotor of a centrifugal Igi machine. Figure 3 is a cross-sectional view of the same, Figure m4 is a cross-sectional view of the inside of the hollow, and Figures 5 to 7 show the WA manufacturing method of hollow blades as the first to third embodiments, respectively.J-Manufacturing process diagram It is. (3)...Hollow wing, (5), (5')...Reinforcement rib, (9), <9')...Wing surface extension plate. Start Figure 1 O Figure 2 Beat 4 Figure 3
Claims (1)
た形状に形成された翼面展間板(9)を用意し、該翼面
展開板(9)に補強リブ(5)。 ・・・を形成した後、該補強リブ(5)、・・・形成側
を内側にして翼面展間4f;t(9)を所定形状の翼面
を形成Jるように2つに折り曲げ、該翼面展間板(9)
の折曲げ自由端同士を溶接にJ、り互いに接合して中空
翼(3)を形成することを特徴とJる中空翼の製造方法
。(1) Pressing] A wing surface expansion plate (9) formed in a shape in which the wing surface of the hollow wing (3) is expanded is prepared, and reinforcing ribs (5) are attached to the wing surface expansion plate (9). . . . . After forming the reinforcing rib (5), . . . the wing surface extension space 4f; t (9) is folded into two with the forming side inward so as to form a wing surface of a predetermined shape. , the wing surface plate (9)
A method for manufacturing a hollow wing, characterized by joining the bent free ends of the two to each other by welding to form a hollow wing (3).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP12743783A JPS6018243A (en) | 1983-07-12 | 1983-07-12 | Production of hollow vane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP12743783A JPS6018243A (en) | 1983-07-12 | 1983-07-12 | Production of hollow vane |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS6018243A true JPS6018243A (en) | 1985-01-30 |
Family
ID=14959923
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP12743783A Pending JPS6018243A (en) | 1983-07-12 | 1983-07-12 | Production of hollow vane |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6018243A (en) |
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS62137110A (en) * | 1985-12-09 | 1987-06-20 | Nippon Steel Corp | Cold rolling method for steel strip |
JPS6384702A (en) * | 1985-04-16 | 1988-04-15 | エスエムエス シユレ−マン・ジ−マグ アクチエンゲゼルシヤフト | Roll stand with roll movable in axial direction |
JPH02102821A (en) * | 1988-10-11 | 1990-04-16 | Yamakawa Ind Co Ltd | Metallic plate reinforcing rib structure and its pressing method |
JPH05305376A (en) * | 1992-04-30 | 1993-11-19 | Asahi M & Ii:Kk | Method for forming blade for oblique flow fan |
WO1998016746A1 (en) * | 1996-10-14 | 1998-04-23 | Daikin Industries, Ltd. | Method of manufacturing hollow blade, and hollow blade manufactured by same |
JP2001349297A (en) * | 2000-06-06 | 2001-12-21 | Fuji Industrial Co Ltd | Turbofan for range hood, and range hood containing the turbofan |
WO2005052377A1 (en) * | 2003-11-27 | 2005-06-09 | Daikin Industries, Ltd. | Blade wheel for centrifugal blower and centerifugal blower with the same |
JP2009281421A (en) * | 2008-05-20 | 2009-12-03 | Teikoku Piston Ring Co Ltd | Piston ring |
CN107401525A (en) * | 2016-04-20 | 2017-11-28 | 庞克有限公司 | Formed blades and blast fan |
JP2020037900A (en) * | 2018-09-04 | 2020-03-12 | 株式会社日立製作所 | Centrifugal impeller and centrifugal fluid machine |
-
1983
- 1983-07-12 JP JP12743783A patent/JPS6018243A/en active Pending
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6384702A (en) * | 1985-04-16 | 1988-04-15 | エスエムエス シユレ−マン・ジ−マグ アクチエンゲゼルシヤフト | Roll stand with roll movable in axial direction |
JPH0755323B2 (en) * | 1985-04-16 | 1995-06-14 | エスエムエス シユレ−マン・ジ−マグ アクチエンゲゼルシヤフト | Roll stand with axially movable roll |
JPS62137110A (en) * | 1985-12-09 | 1987-06-20 | Nippon Steel Corp | Cold rolling method for steel strip |
JPH02102821A (en) * | 1988-10-11 | 1990-04-16 | Yamakawa Ind Co Ltd | Metallic plate reinforcing rib structure and its pressing method |
JPH05305376A (en) * | 1992-04-30 | 1993-11-19 | Asahi M & Ii:Kk | Method for forming blade for oblique flow fan |
US6132826A (en) * | 1996-10-14 | 2000-10-17 | Daikin Industries, Ltd. | Method of manufacturing hollow blade and hollow blade manufactured by same |
WO1998016746A1 (en) * | 1996-10-14 | 1998-04-23 | Daikin Industries, Ltd. | Method of manufacturing hollow blade, and hollow blade manufactured by same |
CN1093230C (en) * | 1996-10-14 | 2002-10-23 | 大金工业株式会社 | Hallow tab making method and made hollow tab |
JP2001349297A (en) * | 2000-06-06 | 2001-12-21 | Fuji Industrial Co Ltd | Turbofan for range hood, and range hood containing the turbofan |
WO2005052377A1 (en) * | 2003-11-27 | 2005-06-09 | Daikin Industries, Ltd. | Blade wheel for centrifugal blower and centerifugal blower with the same |
US8007240B2 (en) | 2003-11-27 | 2011-08-30 | Daikin Industries, Ltd. | Impeller of centrifugal fan and centrifugal fan disposed with the impeller |
JP2009281421A (en) * | 2008-05-20 | 2009-12-03 | Teikoku Piston Ring Co Ltd | Piston ring |
CN107401525A (en) * | 2016-04-20 | 2017-11-28 | 庞克有限公司 | Formed blades and blast fan |
JP2020037900A (en) * | 2018-09-04 | 2020-03-12 | 株式会社日立製作所 | Centrifugal impeller and centrifugal fluid machine |
WO2020049810A1 (en) * | 2018-09-04 | 2020-03-12 | 株式会社日立インダストリアルプロダクツ | Centrifugal impeller and centrifugal fluid machine |
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