JPS6214397Y2 - - Google Patents

Info

Publication number
JPS6214397Y2
JPS6214397Y2 JP1982077301U JP7730182U JPS6214397Y2 JP S6214397 Y2 JPS6214397 Y2 JP S6214397Y2 JP 1982077301 U JP1982077301 U JP 1982077301U JP 7730182 U JP7730182 U JP 7730182U JP S6214397 Y2 JPS6214397 Y2 JP S6214397Y2
Authority
JP
Japan
Prior art keywords
main body
impeller
blade material
extrusion molding
screw
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.)
Expired
Application number
JP1982077301U
Other languages
Japanese (ja)
Other versions
JPS58178499U (en
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 filed Critical
Priority to JP7730182U priority Critical patent/JPS58178499U/en
Publication of JPS58178499U publication Critical patent/JPS58178499U/en
Application granted granted Critical
Publication of JPS6214397Y2 publication Critical patent/JPS6214397Y2/ja
Granted legal-status Critical Current

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Description

【考案の詳細な説明】 本考案は遠心送風機用羽根車に用いられるエア
フオイル形の羽根材に関するものである。
[Detailed Description of the Invention] The present invention relates to an airfoil type impeller used in an impeller for a centrifugal blower.

遠心送風機の羽根車において、エアフオイル形
の断面形状となつた羽根が用いられることは周知
であるが、従来の羽根は平板をエアフオイル形に
曲げ加工したものが一般的であり、羽根車のバツ
クプレートやエンドリングへの取付けは溶接によ
つて行なわれるのが普通である。このため、羽根
の製作の羽根車の組立てに手数がかかつてコスト
高となり、また溶接部の歪やはずれなども生じや
すいという問題点があつた。
It is well known that impellers for centrifugal blowers use blades with an airfoil-shaped cross-sectional shape, but conventional blades are generally made by bending a flat plate into an airfoil shape, and the back plate of the impeller Attachment to the end ring or end ring is usually done by welding. For this reason, there have been problems in that the assembly of the impeller for producing the blades is time consuming and costly, and the welded parts are likely to be distorted or dislodged.

本考案はこの点に着目し、製作が容易で羽根車
の組立てにも手数のかからない羽根材を提供する
ことを目的としてなされたものであり、外形の断
面形状がエアフオイル形となつた中空薄肉の本体
と、本体内部に本体と連結された状態で設けられ
る複数個のビス止め部とを押出成形により一体に
形成し、各ビス止め部の中心にビス止め用の雌ね
じ穴を形成するための中子支持部によつて押出成
形時に必然的に生ずることになる開口部をすべて
本体の後方尾端寄りに向けて開口したことを特徴
としている。すなわち、本考案の羽根材は、大量
生産に適した押出成形によつて製造されるので製
作は容易でコストは安く、また軽量であり、組立
てはビス止めによつて行なうため組立ては簡単で
あるとともに、溶接の場合のような歪などの問題
が生ずることはない。更に押出成形の場合には、
金型の中子の関係でビス止め部には必ず開口部が
形成され、開口部のない円筒形のものよりもビス
止め強度が低下する傾向があるが、本考案では羽
根車が回転した場合の遠心力と空気抵抗力が加わ
らない後方尾端寄りに向けて開口部が設けられて
いるので、開口部はビス止め強度に実用上影響が
なく、強固な組立てを行なうことができるのであ
る。
The present invention was developed with the aim of providing a blade material that is easy to manufacture and requires no effort to assemble an impeller. The main body and a plurality of screw fastening parts provided inside the main body while being connected to the main body are integrally formed by extrusion molding, and an internal thread for forming a female threaded hole for screw fastening is formed in the center of each screw fastening part. It is characterized in that all openings that are inevitably created by the child support portion during extrusion molding are opened toward the rear tail end of the main body. That is, the blade material of the present invention is manufactured by extrusion molding, which is suitable for mass production, so it is easy to manufacture, low cost, and lightweight, and it is easy to assemble because it is fastened with screws. At the same time, problems such as distortion that occur in the case of welding do not occur. Furthermore, in the case of extrusion molding,
Due to the core of the mold, an opening is always formed in the screw fixing part, and the strength of the screw fixation tends to be lower than that of a cylindrical type without an opening. However, in this invention, when the impeller rotates, Since the opening is provided toward the rear tail end where the centrifugal force and air resistance force are not applied, the opening has no practical effect on the strength of screwing, allowing for a strong assembly.

次に本考案の実施例を図面により説明する。第
1図及び第2図は羽根材の断面図を示すもので、
第1図はビス止め部を2個設けたもの、第2図は
3個のビス止め部を設けたやや大形のものの例で
ある。
Next, an embodiment of the present invention will be described with reference to the drawings. Figures 1 and 2 show cross-sectional views of the blade material.
FIG. 1 shows an example of a device provided with two screw fastening portions, while FIG. 2 shows an example of a somewhat larger device provided with three screw fastening portions.

図において、1は外形の断面形状がエアフオイ
ル形となつた中空薄肉の本体、2,3は本体1の
内部に一体に設けられたビス止め部である。この
ビス止め部2は幅の広い部分ではリブ4によつて
本体1と連結される断面略C字形のもの、ビス止
め部3は本体1の後端の幅の狭くなつた部分に本
体1と連続的に形成されたものであり、各ビス止
め部2,3の中心には、ビス止め時にビスがねじ
込まれる雌ねじ穴2a,3aが形成されている。
5は各ビス止め部2,3の開口部であり、いずれ
も本体1後方の尾端1aに向けて開口するように
設けられている。本実施例の羽根材6は以上のよ
うな断面形状であり、押出成形により図面に直角
な方向に伸びた連続体として製造され、材料とし
ては例えばアルミニウムが用いられる。
In the figure, reference numeral 1 denotes a hollow, thin-walled main body with an airfoil-shaped external cross-sectional shape, and reference numerals 2 and 3 denote screw fixing parts integrally provided inside the main body 1. The screw fixing part 2 has a substantially C-shaped cross section connected to the main body 1 by a rib 4 at the wide part, and the screw fixing part 3 is connected to the main body 1 at the narrow part at the rear end of the main body 1. They are formed continuously, and female threaded holes 2a, 3a into which screws are screwed are formed in the center of each screw fastening part 2, 3.
Reference numeral 5 denotes an opening of each screw fixing part 2, 3, and both are provided so as to open toward the tail end 1a at the rear of the main body 1. The blade material 6 of this embodiment has the above-described cross-sectional shape, and is manufactured by extrusion molding as a continuous body extending in a direction perpendicular to the drawing, and is made of aluminum, for example.

第3図及び第4図は、上記の羽根材6を用いて
組立てられた遠心送風機用羽根車を示すものであ
り、11は羽根材6を所定長さに切断して得られ
た羽根、12はボス、13はボス12にリベツト
14により固定されたバツクプレート、16はエ
ンドリング、16は取付けビス、17は羽根車で
ある。羽根11のバツクプレート13への取付け
は、所定位置に設けられたビス穴(図示せず)に
取付けビス16を挿通し、ビス止め部2,3の雌
ねじ穴2a,3aにねじ込むことによつて行なわ
れ、エンドリング15の取付けも同じ要領で行な
われる。羽根11は例えば30度のピツチで配置さ
れ、且つ細くなつた尾端を外側にして直径方向に
対して一定の傾斜をもつて取付けられており、バ
ツクプレート13の両面に、第3図に実線と破線
で示すように半ピツチずつずれて交互に取付けら
れる。
3 and 4 show an impeller for a centrifugal blower assembled using the above-mentioned blade material 6, 11 is a blade obtained by cutting the blade material 6 into a predetermined length, 12 13 is a back plate fixed to the boss 12 with rivets 14, 16 is an end ring, 16 is a mounting screw, and 17 is an impeller. The blade 11 is attached to the back plate 13 by inserting the mounting screw 16 into a screw hole (not shown) provided at a predetermined position and screwing it into the female threaded hole 2a, 3a of the screw stopper part 2, 3. The end ring 15 is attached in the same manner. The blades 11 are arranged at a pitch of, for example, 30 degrees, and are attached at a constant inclination in the diametrical direction with the tapered tail ends outward. They are installed alternately, shifted by a half pitch, as shown by the broken lines.

羽根車17は反時計方向に回転して空気を中心
部から周縁部方向へ押出すが、この時、羽根11
には第3図に示すように放射状方向の遠心力F1
と、空気の流れによる空気抵抗力F2とが加わ
る。この空気抵抗力F2は空気によつて羽根11
を外方向へ押出す力と、エアフオイル形状によつ
て生ずる浮力などの合成されたものであり、その
方向は、回転速度などによつて若干変動するとし
ても常に遠心力F1と同じく外方向、すなわち、
羽根11の尾端方向に向いたものとなつて内方向
に向くことは決してない。従つて、開口部5を後
方尾端1a寄りに開口してある各ビス止め部2,
3はこれらの外力に対して丁度止まり勝手の形状
となり、開口部5の部分に力がかかることはな
く、取付けビス16がゆるんだり、開口部5が破
損したりするようなことは全く生じないのであ
る。なお、第1図及び第2図では、羽根材6の前
端から尾端までを貫く円弧状の基準線の方向に一
致させて尾端向きに開口部5を設けた例を示して
いるが、開口部5は基準線に対して若干傾斜した
角度で設けることもでき、またビス止め部2,3
の形状が個数も必要に応じて適宜選定できること
はもちろんである。
The impeller 17 rotates counterclockwise to push air from the center toward the periphery, but at this time, the impeller 11
As shown in Figure 3, there is a centrifugal force F 1 in the radial direction.
and the air resistance force F 2 due to the air flow. This air resistance force F 2 is caused by the air on the blade 11
It is a combination of the force pushing outward the buoyant force generated by the shape of the airfoil, and even if its direction varies slightly depending on the rotational speed, it is always outward like the centrifugal force F1 . That is,
It points toward the tail end of the blade 11 and never inward. Therefore, each screw fastening part 2, which has an opening 5 opened closer to the rear tail end 1a,
3 has a shape that can be stopped against these external forces, and no force is applied to the opening 5, and there is no possibility that the mounting screw 16 will loosen or the opening 5 will be damaged. It is. Note that although FIGS. 1 and 2 show an example in which the opening 5 is provided toward the tail end so as to match the direction of the arc-shaped reference line passing through the blade material 6 from the front end to the tail end, The opening 5 can be provided at a slightly inclined angle with respect to the reference line, and the screw fixing parts 2 and 3 can also be provided at an angle slightly inclined to the reference line.
It goes without saying that the shape and number of the parts can be appropriately selected as necessary.

上述にように、本考案の羽根材は、エアフオイ
ル形の中空薄肉の本体と本体内部のビス止め部と
を押出成形によつて一体に形成し、ビス止め部の
開口部を本体の後方尾端寄りに向けて開口したも
のであり、安いコストで容易に製作することがで
き、羽根車の組立てはビスによつて簡単に行なう
ことができるとともに歪が生ずることもなくな
り、また押出成形に避けられないビス止め部の開
口部があつても取付け強度が低下せず、強固な取
付けを行なうことができる等の利点のあるもので
ある。
As mentioned above, the blade material of the present invention has an airfoil-shaped hollow thin-walled main body and a screw fastening part inside the main body integrally formed by extrusion molding, and the opening of the screw fastening part is connected to the rear tail end of the main body. It is open toward the side, and can be manufactured easily at low cost.The impeller can be easily assembled using screws, and distortion does not occur, and it can be avoided by extrusion molding. This has the advantage that even if there is an opening in the screw fixing part, the installation strength does not decrease and a strong installation can be achieved.

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

第1図及び第2図はそれぞれ本考案の実施例の
断面図、第3図は本考案の羽根材を用いた羽根車
の一部破断面図、第4図は同上の一部破断正面図
である。 1は本体、1aは尾端、2,3はビス止め部、
2a,3aは雌ねじ穴、5は開口部、6は羽根
材、11は羽根である。
Figures 1 and 2 are respectively sectional views of embodiments of the present invention, Figure 3 is a partially cutaway cross-sectional view of an impeller using the blade material of the present invention, and Figure 4 is a partially cutaway front view of the same. It is. 1 is the main body, 1a is the tail end, 2 and 3 are screw fixing parts,
2a and 3a are female screw holes, 5 is an opening, 6 is a blade material, and 11 is a blade.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 押出成形によつて、外形の断面形状がエアフオ
イル形となつた中空薄肉の本体内部に、ビス止め
用の雌ねじ穴となる部分を中心に備えた複数個の
ビス止め部が本体に連結された状態で一体に形成
された遠心送風機用羽根車の羽根材であつて押出
成形時における雌ねじ穴形成用の中子支持部のた
めに生ずる各ビス止め部の開口部をすべて本体の
後方尾端寄りに向けて開口させてなる遠心送風機
用羽根車の羽根材。
Inside the hollow, thin-walled main body whose external cross-sectional shape has an airfoil shape through extrusion molding, multiple screw fastening parts are connected to the main body, each having a female threaded hole for screw fastening in the center. The blade material of the impeller for a centrifugal blower is formed integrally with the core support part for forming the female screw hole during extrusion molding. A blade material for an impeller for a centrifugal blower that opens toward the direction of the air.
JP7730182U 1982-05-25 1982-05-25 Blade material for impellers for centrifugal blowers Granted JPS58178499U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7730182U JPS58178499U (en) 1982-05-25 1982-05-25 Blade material for impellers for centrifugal blowers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7730182U JPS58178499U (en) 1982-05-25 1982-05-25 Blade material for impellers for centrifugal blowers

Publications (2)

Publication Number Publication Date
JPS58178499U JPS58178499U (en) 1983-11-29
JPS6214397Y2 true JPS6214397Y2 (en) 1987-04-13

Family

ID=30086569

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7730182U Granted JPS58178499U (en) 1982-05-25 1982-05-25 Blade material for impellers for centrifugal blowers

Country Status (1)

Country Link
JP (1) JPS58178499U (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4821084B2 (en) * 2003-10-22 2011-11-24 パナソニック株式会社 Turbofan and turbofan manufacturing method

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56126698A (en) * 1980-02-06 1981-10-03 Kofuimuko Esu Ei Esu Radial flow fan with large sucking force having twist-less blade

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS56126698A (en) * 1980-02-06 1981-10-03 Kofuimuko Esu Ei Esu Radial flow fan with large sucking force having twist-less blade

Also Published As

Publication number Publication date
JPS58178499U (en) 1983-11-29

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