JPS6233999Y2 - - Google Patents

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Publication number
JPS6233999Y2
JPS6233999Y2 JP1982199937U JP19993782U JPS6233999Y2 JP S6233999 Y2 JPS6233999 Y2 JP S6233999Y2 JP 1982199937 U JP1982199937 U JP 1982199937U JP 19993782 U JP19993782 U JP 19993782U JP S6233999 Y2 JPS6233999 Y2 JP S6233999Y2
Authority
JP
Japan
Prior art keywords
engagement
base frame
impeller
engagement protrusion
piece
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
JP1982199937U
Other languages
Japanese (ja)
Other versions
JPS59105099U (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 JP19993782U priority Critical patent/JPS59105099U/en
Publication of JPS59105099U publication Critical patent/JPS59105099U/en
Application granted granted Critical
Publication of JPS6233999Y2 publication Critical patent/JPS6233999Y2/ja
Granted legal-status Critical Current

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Description

【考案の詳細な説明】 本考案は、斜流送風機の羽根車の構造に関する
ものである。
[Detailed Description of the Invention] The present invention relates to the structure of an impeller for a mixed flow blower.

斜流送風機の羽根車については、種々研究され
ており、本出願人も、実願昭57−78004号として
出願している。先願にかかる斜流送風機の羽根車
は、第5図図示の如く、截頭円錐状の基枠aの円
錐部bに、翼片cと該翼片cの基端部dに一体形
成され且つ前記基枠円錐部bを所望の翼枚数と同
数に円周方向に等分割した形状を有する間隔片e
とからなる翼ユニツトfを複数個全周に亘つて被
着して構成されているが、この場合基枠aの大径
端部となる環状体gの嵌合面が平面状に形成され
ているため、翼ユニツトfの基枠aへの組付作業
が容易に行なえないという問題があつた。
Various studies have been conducted on impellers for mixed flow blowers, and the present applicant has also filed an application as Utility Model Application No. 1978-78004. As shown in FIG. 5, the impeller of the mixed flow blower according to the prior application is integrally formed with a conical portion b of a truncated conical base frame a, a blade c and a base end d of the blade c. and a spacing piece e having a shape in which the base frame conical part b is equally divided in the circumferential direction into the same number as the desired number of blades.
In this case, the fitting surface of the annular body g, which is the large diameter end of the base frame a, is formed into a flat shape. Therefore, there was a problem in that it was not easy to assemble the wing unit f to the base frame a.

本考案は、上記問題を解消して、組立て作業を
著しく容易ならしめることを目的とするものであ
り、かかる目的達成のため、截頭円錐状の基枠の
円錐部に翼片と該翼片の基端部に一体形成され且
つ前記基枠円錐部を所望の翼枚数と同数に円周方
向に等分割した形状を有する間隔片とからなる翼
ユニツトを複数個全周に亘つて被着するようにし
た斜流送風機の羽根車であつて、前記基枠におい
て、小径端部となる截頭部に環状の係合部を、大
径端部となる環状体に断面円弧状の凸周面を有す
る係合突起をそれぞれ形成する一方、前記各間隔
片内面に、前記係合部および係合突起と係合する
一対の係合片を、これら係合片の係合面が相対向
する如くして求心方向に突設するとともに、前記
係合突起と係合する側の係合片の係合面を、前記
翼ユニツトが前記係合突起を軸として回動され得
るように、該係合突起の凸周面に対して摺接可能
な凹溝形状となした構成を特徴とする。
The purpose of the present invention is to solve the above-mentioned problems and make the assembly work considerably easier.In order to achieve this purpose, the wing pieces and the wing pieces are attached to the conical part of the truncated conical base frame. A plurality of blade units are attached over the entire circumference of the blade unit, each consisting of a spacer piece integrally formed on the base end portion of the base frame and having a shape in which the base frame conical portion is equally divided in the circumferential direction into the same number of blades as the desired number. In the impeller of the mixed flow blower, in the base frame, the truncated portion serving as the small diameter end portion has an annular engagement portion, and the annular body serving as the large diameter end portion has a convex circumferential surface having an arcuate cross section. and a pair of engaging pieces that engage with the engaging portion and the engaging protrusion are formed on the inner surface of each of the spacer pieces so that the engaging surfaces of these engaging pieces face each other. and protrudes in the centripetal direction, and the engagement surface of the engagement piece on the side that engages with the engagement protrusion is arranged such that the wing unit can be rotated around the engagement protrusion. It is characterized by a concave groove shape that can slide into contact with the convex peripheral surface of the protrusion.

以下添付の図面を参照して本考案の実施例にか
かる斜流送風機の羽根車を説明する。
DESCRIPTION OF THE PREFERRED EMBODIMENTS An impeller for a mixed flow fan according to an embodiment of the present invention will be described below with reference to the accompanying drawings.

この羽根車は、截頭円錐状の基枠1と該基枠1
の円錐部1aに被着される翼ユニツト2と、前記
基枠1の前後面に被着される端板3,4とによつ
て構成されている。
This impeller includes a truncated conical base frame 1 and the base frame 1.
The wing unit 2 is attached to the conical portion 1a of the base frame 1, and the end plates 3 and 4 are attached to the front and rear surfaces of the base frame 1.

前記基枠1の小径端部となる截頭部1bには、
外周縁の環状鍔5と中心部のモータ軸取付用のボ
ス部6とを3個の連結部7,7,7で連結して構
成されており、環状鍔5とボス部6との間には、
連結部7,7,7によつて隔てられた3個の扇形
の通風穴8,8,8が形成されている。
The truncated head 1b, which is the small diameter end of the base frame 1, has a
It is constructed by connecting an annular flange 5 on the outer periphery and a boss part 6 for attaching the motor shaft in the center with three connecting parts 7, 7, 7, and between the annular flange 5 and the boss part 6 teeth,
Three sector-shaped ventilation holes 8, 8, 8 are formed separated by the connecting portions 7, 7, 7.

前記環状鍔5には、後述する翼ユニツト2前端
側の係合片21を係止すべき係合部となる環状溝
9が形成されている。
An annular groove 9 is formed in the annular collar 5 and serves as an engaging portion for engaging an engaging piece 21 on the front end side of the wing unit 2, which will be described later.

前記ボス部6には、モータの駆動軸を軸着すべ
き軸穴10が形成されている。
The boss portion 6 is formed with a shaft hole 10 into which a drive shaft of a motor is to be mounted.

前記連結部7には、前部の端板3を固定するた
めのビス11を螺着すべきビス孔12が形成され
ている。
The connecting portion 7 is formed with a screw hole 12 into which a screw 11 for fixing the front end plate 3 is screwed.

前記各通風穴8には、前記基枠1内方から通風
穴8を通つて外方へ向う空気流を誘起する冷却用
羽根13,13が設けられている。
Each of the ventilation holes 8 is provided with cooling vanes 13, 13 that induce an air flow from inside the base frame 1 to the outside through the ventilation holes 8.

一方、基枠1の円錐部1aは、その大径端部を
構成する環状体14を截頭部1bの連結部7,
7,7の延長上に位置する連結枠15,15,1
5で連結して構成されており、該連結枠15,1
5,15相互間には開口部16,16,16が形
成されている。
On the other hand, the conical part 1a of the base frame 1 connects the annular body 14 constituting its large diameter end to the connecting part 7 of the truncated head 1b.
Connecting frame 15, 15, 1 located on the extension of 7, 7
5 are connected to each other, and the connecting frames 15, 1
Openings 16, 16, 16 are formed between 5, 15.

前記環状体14の外端には、断面円弧状の凸周
面を有する環状の係合突起17が形成されてい
る。
An annular engagement protrusion 17 having a convex circumferential surface with an arcuate cross section is formed at the outer end of the annular body 14 .

又、各連結枠15の後端部には、後部の端板4
を固定するためのビス18を螺着すべきビス孔3
4が形成されている。
Also, at the rear end of each connection frame 15, a rear end plate 4 is provided.
Screw hole 3 into which screw 18 should be screwed to fix the
4 is formed.

前記翼ユニツト2は、翼片19と該翼片19の
基端部19aに一体突設された間隔片20とによ
つて構成されている。
The wing unit 2 is composed of a wing 19 and a spacing piece 20 integrally projecting from the base end 19a of the wing 19.

該間隔片20は、基枠1の円錐部1aを所望の
翼枚数(本実施例では12枚)と同数に円周方向に
等分割した形状を有している。即ち、間隔片20
は、隣り合う翼片19,19の基端部19a,1
9aの間の間隔を決定する作用を有しており、こ
れら12個の間隔片20,20……で羽根車の円錐
面が構成されている。該間隔片20の周方向端面
20aは、翼片基端部19aと同一の形状とされ
ている。
The spacing pieces 20 have a shape in which the conical portion 1a of the base frame 1 is equally divided in the circumferential direction into the same number of blades as the desired number (12 in this embodiment). That is, the spacing piece 20
are the proximal ends 19a, 1 of the adjacent wing pieces 19, 19.
These 12 spacing pieces 20, 20, . . . constitute a conical surface of the impeller. The circumferential end surface 20a of the spacing piece 20 has the same shape as the blade base end 19a.

前記間隔片20内面における軸方向の前端縁と
中間部位とには、前記環状溝9および係合突起1
7と係合する一対の係合片21,22が、これら
係合片21,22の係合面を相対向させて求心方
向にそれぞれ一体に突設されている。
The annular groove 9 and the engagement protrusion 1 are provided at the axial front edge and the intermediate portion of the inner surface of the spacer piece 20.
A pair of engagement pieces 21 and 22 that engage with the engagement piece 7 are integrally provided in a centripetal direction with the engagement surfaces of these engagement pieces 21 and 22 facing each other.

該前側の係合片21の前後面には、前部端板3
に形成した円形凹部23に嵌合して翼ユニツト2
の回り止めを行なう円形突起24および基枠截頭
部1bの環状鍔5に形成した環状溝9に係合すべ
き突起25がそれぞれ形成されている。
A front end plate 3 is provided on the front and rear surfaces of the front engagement piece 21.
The wing unit 2 is fitted into the circular recess 23 formed in the
A circular protrusion 24 for preventing rotation of the base frame and a protrusion 25 for engaging with an annular groove 9 formed in the annular collar 5 of the base frame truncated head 1b are formed, respectively.

又、前記後側の係合片22の前後面には、基枠
円錐部1aの係合突起17を嵌合すべき円弧状内
周面を有する嵌合溝26および後部端板4に形成
した凹部27に係合すべき突起28がそれぞれ形
成されている。
Further, on the front and rear surfaces of the rear engaging piece 22, a fitting groove 26 having an arcuate inner circumferential surface into which the engaging protrusion 17 of the base frame conical portion 1a is fitted, and a rear end plate 4 are formed. Protrusions 28 to be engaged with the recesses 27 are respectively formed.

更に、前記間隔片20には、係合片21,22
間において空気吸込側に適宜大きさの通風穴29
が形成されている。
Further, the spacing piece 20 includes engagement pieces 21 and 22.
A ventilation hole 29 of an appropriate size is provided on the air suction side between
is formed.

なお図面中、符号30および31は前後の端板
3および4に形成したビス11および18用のビ
ス孔、32および33は前後の端板3および4を
仮止めするための爪片である。
In the drawings, numerals 30 and 31 are screw holes for the screws 11 and 18 formed in the front and rear end plates 3 and 4, and 32 and 33 are claw pieces for temporarily fixing the front and rear end plates 3 and 4.

次いで、この羽根車の組立順序を説明すると、
第3図図示の如く、翼ユニツト2の後側の係合片
22に設けた嵌合溝26に基枠円錐部1aの係合
突起17を嵌合せしめた後、該係合突起17と嵌
合溝26との接合面を支点として翼ユニツト2を
矢印B方向に弧回動させて、翼ユニツト2の前側
の係合片21に設けた突起25を基枠截頭部1b
の環状溝9に係合せしめる。このようにして基枠
円錐部1a全周に亘つて翼ユニツト2,2……を
被着した後、前後から端板3および4をビス1
1,18でそれぞれ固着するのである。
Next, the assembly order of this impeller will be explained as follows.
As shown in FIG. 3, after the engagement protrusion 17 of the base frame conical portion 1a is fitted into the engagement groove 26 provided in the engagement piece 22 on the rear side of the wing unit 2, the engagement protrusion 17 is fitted into the engagement protrusion 17. The blade unit 2 is rotated arcuately in the direction of arrow B using the joint surface with the mating groove 26 as a fulcrum, and the protrusion 25 provided on the front engaging piece 21 of the blade unit 2 is connected to the base frame truncated head 1b.
into the annular groove 9 of. After the wing units 2, 2, etc. are attached to the entire circumference of the base frame conical portion 1a in this way, the end plates 3 and 4 are screwed in from the front and back.
1 and 18, respectively.

上記の如くすると、羽根車の組立作業が著しく
簡易化されることとなり、生産性の向上が著し
い。
By doing so as described above, the assembly work of the impeller is significantly simplified, and the productivity is significantly improved.

続いて、本考案の斜流送風機の羽根車の効果を
述べる。
Next, the effects of the impeller of the mixed flow blower of the present invention will be described.

本考案によれば、基枠1の大径端部となる環状
体14に断面円弧状の凸周面を有する係合突起1
7を形成し、該係合突起17と翼ユニツト2の間
隔片20内面に突設した後部係合片22の凹溝形
状の係合面との接合面を支点として、翼ユニツト
2を弧回動させることによつて、基枠円錐部1a
に翼ユニツト2を被着するようにしたので、第5
図図示の先願のものに比べて翼ユニツト2の組付
け作業を著しく簡易化でき、生産性の向上に寄与
すること大であるという実用的な効果がある。
According to the present invention, the engagement protrusion 1 has a convex circumferential surface having an arcuate cross section on the annular body 14 which is the large diameter end of the base frame 1.
7, and the blade unit 2 is rotated in an arc using the joint surface between the engaging protrusion 17 and the groove-shaped engaging surface of the rear engaging piece 22 protruding from the inner surface of the spacer piece 20 of the blade unit 2 as a fulcrum. By moving the base frame conical part 1a
Since the wing unit 2 is attached to the
This embodiment has the practical effect of significantly simplifying the assembly work of the wing unit 2 compared to the prior application shown in the figure, and greatly contributing to improved productivity.

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

第1図は本考案の実施例にかかる斜流送風機の
羽根車の1部を断面とした側面図、第2図は第1
図の斜流送風機の羽根車の正面図、第3図は第2
図の羽根車の分解縦断面図、第4図は第2図の羽
根車における翼ユニツトの斜視図、第5図は先願
にかかる斜流送風機の羽根車の縦断面図である。 1……基枠、1a……基枠の円錐部、1b……
基枠の截頭部、2……翼ユニツト、9……係合
部、14……環状体、17……係合突起、19…
…翼片、20……間隔片、21,22……係合
片。
FIG. 1 is a side view of a part of the impeller of the mixed flow blower according to the embodiment of the present invention, and FIG.
Figure 3 is a front view of the impeller of the mixed flow blower.
4 is a perspective view of the blade unit in the impeller of FIG. 2, and FIG. 5 is a longitudinal sectional view of the impeller of the mixed flow blower according to the prior application. 1...Base frame, 1a...Conical part of base frame, 1b...
Truncated portion of base frame, 2... Wing unit, 9... Engaging portion, 14... Annular body, 17... Engaging protrusion, 19...
...wing piece, 20... spacing piece, 21, 22... engagement piece.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 截頭円錐状の基枠1の円錐部1aに翼片19と
該翼片19の基端部19aに一体形成され且つ前
記基枠円錐部1aを所望の翼枚数と同数に円周方
向に等分割した形状を有する間隔片20とからな
る翼ユニツト2を複数個全周に亘つて被着するよ
うにした斜流送風機の羽根車であつて、前記基枠
1において、小径端部となる截頭部1bに環状の
係合部9を、大径端部となる環状体14に断面円
弧状の凸周面を有する係合突起17をそれぞれ形
成する一方、前記各間隔片20内面に、前記係合
部9および係合突起17と係合する一対の係合片
21,22を、これら係合片21,22の係合面
が相対向する如くして求心方向に突設するととも
に、前記係合突起17と係合する側の係合片22
の係合面を、前記翼ユニツト2が前記係合突起1
7を軸として回動され得るように、該係合突起1
7の凸周面に対して摺接可能な凹溝形状となした
ことを特徴とする斜流送風機の羽根車。
A wing piece 19 is integrally formed on the conical part 1a of the truncated conical base frame 1 and a base end 19a of the wing piece 19, and the base frame conical part 1a is arranged in the same number as the desired number of blades in the circumferential direction. This is an impeller for a mixed flow blower in which a plurality of blade units 2 each consisting of a spacer piece 20 having a divided shape are attached over the entire circumference, and in the base frame 1, a cut portion serving as a small diameter end portion is provided. An annular engagement portion 9 is formed on the head 1b, and an engagement protrusion 17 having a convex peripheral surface with an arcuate cross section is formed on the annular body 14 serving as the large diameter end. A pair of engagement pieces 21 and 22 that engage with the engagement portion 9 and the engagement protrusion 17 are provided so as to protrude in the centripetal direction so that the engagement surfaces of these engagement pieces 21 and 22 face each other. Engagement piece 22 on the side that engages with engagement protrusion 17
The blade unit 2 connects the engagement surface of the engagement protrusion 1 with the engagement surface of the engagement protrusion 1.
The engagement protrusion 1 can be rotated about the axis 7.
An impeller for a mixed flow blower, characterized in that the impeller has a concave groove shape that can slide against the convex peripheral surface of No. 7.
JP19993782U 1982-12-30 1982-12-30 mixed flow blower impeller Granted JPS59105099U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19993782U JPS59105099U (en) 1982-12-30 1982-12-30 mixed flow blower impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19993782U JPS59105099U (en) 1982-12-30 1982-12-30 mixed flow blower impeller

Publications (2)

Publication Number Publication Date
JPS59105099U JPS59105099U (en) 1984-07-14
JPS6233999Y2 true JPS6233999Y2 (en) 1987-08-31

Family

ID=30425466

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19993782U Granted JPS59105099U (en) 1982-12-30 1982-12-30 mixed flow blower impeller

Country Status (1)

Country Link
JP (1) JPS59105099U (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5252201A (en) * 1975-10-24 1977-04-26 Kawasaki Heavy Ind Ltd Split type radial impeller
JPS5746097A (en) * 1980-09-04 1982-03-16 Toshiba Corp Propeller fan

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5252201A (en) * 1975-10-24 1977-04-26 Kawasaki Heavy Ind Ltd Split type radial impeller
JPS5746097A (en) * 1980-09-04 1982-03-16 Toshiba Corp Propeller fan

Also Published As

Publication number Publication date
JPS59105099U (en) 1984-07-14

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