JPS6237999Y2 - - Google Patents

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Publication number
JPS6237999Y2
JPS6237999Y2 JP1982107527U JP10752782U JPS6237999Y2 JP S6237999 Y2 JPS6237999 Y2 JP S6237999Y2 JP 1982107527 U JP1982107527 U JP 1982107527U JP 10752782 U JP10752782 U JP 10752782U JP S6237999 Y2 JPS6237999 Y2 JP S6237999Y2
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JP
Japan
Prior art keywords
boss
piece
pieces
wing
overlapping
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
JP1982107527U
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Japanese (ja)
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JPS5911197U (en
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Filing date
Publication date
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Priority to JP10752782U priority Critical patent/JPS5911197U/en
Publication of JPS5911197U publication Critical patent/JPS5911197U/en
Application granted granted Critical
Publication of JPS6237999Y2 publication Critical patent/JPS6237999Y2/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.

本出願人は、既に第1図図示の斜流送風機の羽
根車について実用新案登録出願している(昭和57
年5月25日出願)即ち、この羽根車は截頭円錐状
のボス1′の円錐面1a′に、翼片3′と該翼片3′
の基端部3a′に一体形成され且つ前記ボス円錐面
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4′とからなる翼ユニツト
2′を複数個全周に亘つて被着して構成されてい
る。ところが、この場合、所望の翼枚数に応じて
翼ユニツト2′の間隔片4′の形状が決定されると
ころから、送風性能上の都合等によつて翼枚数を
変更しようとするときには、翼ユニツト2′を製
作するための金型を全面的に変更しなければなら
なくなる。従つて、金型コスト等の面から、同一
のボス1′において翼枚数を任意に変更すること
が不可能であつた。
The applicant has already filed a utility model registration application for the impeller of the mixed flow blower shown in Figure 1 (1982).
(filed on May 25, 2013) That is, this impeller has a conical surface 1a' of a truncated conical boss 1', a blade 3' and a blade 3'.
A plurality of blade units 2' are integrally formed on the base end portion 3a' of the blade unit 2' and spacer pieces 4' each having a shape in which the boss conical surface 1a' is equally divided in the circumferential direction into the same number of blades as the desired number. It is constructed by being coated over the circumference. However, in this case, since the shape of the spacing piece 4' of the blade unit 2' is determined according to the desired number of blades, when changing the number of blades for reasons such as ventilation performance, the blade unit The mold for manufacturing 2' would have to be completely changed. Therefore, from the viewpoint of mold cost, etc., it has been impossible to arbitrarily change the number of blades in the same boss 1'.

本考案は、上記の点に鑑み、同一のボスにおい
て翼枚数を任意に変更できるようにすることを目
的とするものであり、かかる目的達成のため、截
頭円錐状のボスと、翼片の基端部に前記ボスの円
錐面に沿う形状の間隔片を一体形成し且つ該間隔
片の周方向端部に前記ボスの円錐面に沿う形状の
重合片を一体に延設してなる所定数の翼ユニツト
とからなり、前記各間隔片の前縁部と重合片の中
間部位とに、前記ボスの軸方向前後端面間と略同
間隔となる係合片を求心方向に突設し且つ該係合
片間に、前記ボスの軸方向前後端面を挟み込むよ
うにし、しかも隣り合う翼ユニツトの間隔片と重
合片とが所望の翼枚数に応じた重合割合で重合し
合う如くして前記ボスの円錐面に前記翼ユニツト
を配設するとともに、前記間隔片の前縁部に形成
された係合片外面に、位置決め用の突起を突設す
る一方、前記ボスの截頭面に固定される端板に、
前記係合片の突起が選択的に嵌挿される複数の通
孔を形成した。
In view of the above points, the purpose of the present invention is to make it possible to arbitrarily change the number of blades in the same boss. A predetermined number of spacing pieces having a shape along the conical surface of the boss are integrally formed at the base end, and overlapping pieces having a shape along the conical surface of the boss are integrally extended at the circumferential ends of the spacing pieces. a blade unit, and engaging pieces protruding in the centripetal direction at the front edge of each of the spacing pieces and the intermediate portion of the overlapping piece at substantially the same distance as between the front and rear end surfaces in the axial direction of the boss; The front and rear end surfaces of the boss in the axial direction are sandwiched between the engagement pieces, and the spacing pieces and overlapping pieces of adjacent blade units overlap each other at a ratio corresponding to the desired number of blades, so that the boss is The wing unit is disposed on a conical surface, and a protrusion for positioning is provided protrudingly on the outer surface of the engagement piece formed on the front edge of the spacing piece, while the end is fixed to the truncated surface of the boss. on the board,
A plurality of through holes were formed into which the protrusions of the engagement piece were selectively inserted.

以下第2図ないし第7図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 of a mixed flow blower according to an embodiment of the present invention will be described below with reference to FIGS. 2 to 7.

この羽根車は、截頭円錐状のボス1と該ボス1
の円錐面1aに被着される翼ユニツト2とによつ
て構成されている。前記ボス1及び翼ユニツト2
はそれぞれ合成樹脂製のものである。
This impeller includes a truncated conical boss 1 and a truncated conical boss 1.
A wing unit 2 is attached to the conical surface 1a of the wing. The boss 1 and the wing unit 2
are made of synthetic resin.

前記ボス1の截頭面1bには、第3図に示すよ
うに、外周縁の環状鍔3と該環状鍔3を十字状に
連結する連結板4とを残して4個の風穴5,5,
5,5が形成されている。
As shown in FIG. 3, the truncated surface 1b of the boss 1 has four air holes 5, 5, except for the annular collar 3 on the outer periphery and the connecting plate 4 connecting the annular collar 3 in a cross shape. ,
5,5 are formed.

この連結板4は、後に詳述するように、翼ユニ
ツト2を被着した時、環状鍔3に係合される翼ユ
ニツト2前端側の係合片15の表面と同一高さと
なるように隆起せしめられている。
As will be described in detail later, this connecting plate 4 is raised so that it is flush with the surface of the engagement piece 15 on the front end side of the wing unit 2 that is engaged with the annular collar 3 when the wing unit 2 is attached. I'm being forced to do it.

又、連結部4の四本の支脚部4a,4a…の端
部には、前記環状鍔3内周面に連続する係合溝
6,6…と該係合溝6,6…のそれぞれ内側にビ
ス孔7,7…とがそれぞれ形成されている。
Further, at the ends of the four supporting legs 4a, 4a... of the connecting part 4, there are engagement grooves 6, 6... that are continuous with the inner circumferential surface of the annular collar 3, and grooves 6, 6... on the inner sides of the engagement grooves 6, 6..., respectively. Screw holes 7, 7, . . . are formed therein, respectively.

前記環状鍔3には、翼ユニツト2の位置決め用
となる突起8が形成されている。
A protrusion 8 for positioning the wing unit 2 is formed on the annular collar 3.

一方、ボス1の円錐面1aの大径側端部には、
円錐面1aを部分的にえぐつて環状鍔9が一体に
形成され、該環状鍔9には、12個のビス孔10,
10…が等間隔に形成されている。
On the other hand, at the large diameter end of the conical surface 1a of the boss 1,
An annular collar 9 is integrally formed by partially gouging out the conical surface 1a, and the annular collar 9 has 12 screw holes 10,
10... are formed at equal intervals.

前記翼ユニツト2は、第4図に示すように翼片
11と該翼片11の基端部11aに一体突設され
た間隔片12と該間隔片12に延設された重合片
13とによつて構成されている。
As shown in FIG. 4, the wing unit 2 includes a wing 11, a spacing piece 12 integrally projecting from the base end 11a of the wing 11, and an overlapping piece 13 extending from the spacing piece 12. It is structured accordingly.

該間隔片12は、ボス1の円錐面1aを最大翼
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12
は、最大翼枚数取付時において隣り合う翼片1
1,11の基端部11a,11aの間の間隔を決
定する作用を有しており、そのため間隔片12と
重合片13との境界には、翼片11の基端部11
aと同一形状の段差面14が形成されている。
The spacing pieces 12 have a shape in which the conical surface 1a of the boss 1 is equally divided in the circumferential direction into the same number as the maximum number of blades (12 in this embodiment). That is, the spacing piece 12
is the number of adjacent blades 1 when the maximum number of blades is installed.
It has the function of determining the distance between the base end portions 11a, 11a of the blades 1, 11, and therefore, at the boundary between the spacing piece 12 and the overlapping piece 13, the base end portion 11 of the blade 11
A stepped surface 14 having the same shape as a is formed.

前記重合片13は、前記間隔片12と同一形状
とされており、翼ユニツト2,2…をボス円錐面
1aに被着する際に隣りの翼ユニツト2の間隔片
12と重合せしめられる。従つて、重合片13の
周方向端面13aは、翼片11の基端部11aと
同一の形状とされている。
The overlapping piece 13 has the same shape as the spacing piece 12, and is overlapped with the spacing piece 12 of the adjacent blade unit 2 when attaching the blade units 2, 2, . . . to the boss conical surface 1a. Therefore, the circumferential end surface 13a of the overlapping piece 13 has the same shape as the base end 11a of the wing piece 11.

前記間隔片12における軸方向前端縁と重合片
13における軸方向中間部位とには、求心方向に
向かつて係合片15,16がそれぞれ一体に突設
されている。
Engagement pieces 15 and 16 are integrally provided on the axial front end edge of the spacing piece 12 and the axial intermediate portion of the overlapping piece 13, respectively, so as to face in the centripetal direction.

これら係合片15,16先端には、相対向する
如く爪部15a,16aがそれぞれ設けられてい
る。
At the tips of these engaging pieces 15 and 16, claw portions 15a and 16a are provided, respectively, so as to face each other.

前側の係合片15には、中央部に前向きの突起
17と両側端に半円状の切欠穴18,18とが形
成されている。この突起17は、後述する端板1
9を仮止めするためのものであり、又切欠穴18
は、ボス截頭面1b側の突起8と係合して翼ユニ
ツト2の最初の取付位置を決定する作用をなす。
The front engagement piece 15 has a forward-facing protrusion 17 in the center and semicircular cut holes 18 at both ends. This protrusion 17 corresponds to the end plate 1 which will be described later.
9 for temporary fixing, and the cutout hole 18
engages with the protrusion 8 on the boss truncated surface 1b side to determine the initial mounting position of the wing unit 2.

後側の係合片16には、後向きの突起20とビ
ス孔21とが併設されている。この突起20は、
後述する端板22を仮止めするものであり、ビス
孔21には、端板22を固着するためのビス29
が挿着される。
The rear engagement piece 16 is provided with a rearward protrusion 20 and a screw hole 21. This protrusion 20 is
The end plate 22 to be described later is temporarily fixed, and the screw hole 21 has screws 29 for fixing the end plate 22.
is inserted.

尚、係合片15と16との間の間隔は、ボス1
の環状鍔3と9との表面間の間隔より若干狭くさ
れており、係合片15,16が環状鍔3,9に対
して無理嵌めされるようになつている。
Note that the distance between the engagement pieces 15 and 16 is the same as that of the boss 1.
The distance between the surfaces of the annular flanges 3 and 9 is slightly narrower than that of the annular flanges 3 and 9, so that the engaging pieces 15 and 16 are force-fitted into the annular flanges 3 and 9.

前側の端板19は、鋼板製の環状部19aと該
環状部19aを連結する十字状の連結部19bと
からなり、且つ取付状態においてボス截頭面1b
の風穴5,5…と一致する穴23,23…を有し
ている。
The front end plate 19 is composed of an annular portion 19a made of a steel plate and a cross-shaped connecting portion 19b that connects the annular portion 19a, and has a boss truncated surface 1b in the attached state.
It has holes 23, 23... which coincide with the air holes 5, 5....

端板環状部19aには、翼ユニツト2の係合片
15に形成した突起17を嵌挿すべき通孔24
a,24a…及び24b,24b…が形成され
る。通孔24a…は12個であり、12枚の翼ユニツ
ト用のものである。又通孔24b…は8個であり
8枚用のものである。端板連結部19bには、ボ
ス截頭面1b側のビス孔7,7…と一致するビス
孔25,25…が形成されている。
The end plate annular portion 19a has a through hole 24 into which the projection 17 formed on the engagement piece 15 of the wing unit 2 is inserted.
a, 24a... and 24b, 24b... are formed. There are 12 through holes 24a, and they are for 12 blade units. Also, there are eight through holes 24b for eight sheets. Screw holes 25, 25, . . ., which coincide with the screw holes 7, 7, .

一方、後側の端板22は、鋼板製でドーナツ状
を呈しており、ボス1の後部環状鍔9に形成した
ビス孔10,10…と一致する通孔26…及び各
翼ユニツト2,2…の後部係合片16,16…に
形成した突起20,20…を嵌挿すべき通孔26
…が15゜間隔で交互に形成されている。この通孔
26…は全部で24個設けられており、後記する如
く翼ユニツト2が12枚のときは全部使用され、翼
ユニツト2が8枚のときは、16個を使用し、残り
の8個は不使用となるものである。
On the other hand, the rear end plate 22 is made of a steel plate and has a donut shape, and has through holes 26 that match the screw holes 10, 10, formed in the rear annular collar 9 of the boss 1, and each wing unit 2, 2. A through hole 26 into which the protrusions 20, 20, formed on the rear engaging pieces 16, 16, are to be inserted.
...are formed alternately at 15° intervals. A total of 24 through holes 26 are provided, and as described later, when there are 12 blade units 2, all of them are used, and when there are 8 blade units 2, 16 are used, and the remaining 8 holes are used. This item will not be used.

次いて、本実施例にかかる斜流送風機の羽根車
の組立順序を説明すると、ボス1前後の環状鍔
3,9に対して順次翼ユニツト2の前後の係合片
15,16を軸に直角な方向から無理嵌めする。
この時、係合片15及び16のそれぞれの爪部1
5a及び16aは、それぞれ環状鍔3及び9の内
周面に係止され、これによつて遠心方向への離脱
が防止される。
Next, to explain the assembly order of the impeller of the mixed flow blower according to this embodiment, the annular flanges 3 and 9 at the front and rear of the boss 1 are sequentially assembled at right angles about the front and rear engagement pieces 15 and 16 of the blade unit 2. Forcibly fit from the correct direction.
At this time, each claw portion 1 of the engaging pieces 15 and 16
5a and 16a are locked to the inner peripheral surfaces of the annular flanges 3 and 9, respectively, thereby preventing them from coming off in the centrifugal direction.

しかして、最初の翼ユニツト2は、環状鍔3の
突起8への係合片15の切欠穴18の係合によつ
て取付位置が決定される。2個目の翼ユニツト2
からは、既に取付けられた翼ユニツト2の重合片
13上に、取付けようとする翼ユニツト2の間隔
片12を重合させた状態で被着される。従つて、
間隔片12と重合片13との重合の割合を適宜変
更することによつて、隣り合う翼片11,11の
間隔dを任意に決定できる。(第7図参照)。即
ち、ボス円錐面1aへの取付翼枚数の変更も可能
である。例えば、第5図図示の如く、先に取付け
た翼ユニツト2における間隔片12と重合片13
との境界の段差面14に次に取付けようとする翼
ユニツト2における翼片11の基端部11aを当
接する時は、最大取付翼枚数(本実施例では12
枚)となり、第6図図示の如く、先に取付けた翼
ユニツト2における重合片13の中間位置に、次
に取付けようとする翼ユニツト2における翼片基
端部11aを位置せしめる時は、取付翼枚数を減
少できる(本実施例では8枚)。
Thus, the mounting position of the first wing unit 2 is determined by the engagement of the cutout hole 18 of the engagement piece 15 with the projection 8 of the annular collar 3. 2nd wing unit 2
From there, the spacing piece 12 of the wing unit 2 to be attached is applied in a superposed state onto the overlapped piece 13 of the wing unit 2 that has already been attached. Therefore,
By appropriately changing the ratio of overlapping between the spacing pieces 12 and the overlapping pieces 13, the distance d between adjacent wing pieces 11, 11 can be arbitrarily determined. (See Figure 7). That is, it is also possible to change the number of blades attached to the boss conical surface 1a. For example, as shown in FIG.
When contacting the base end portion 11a of the wing piece 11 in the wing unit 2 to be attached next to the step surface 14 at the boundary between the
As shown in FIG. The number of blades can be reduced (eight in this embodiment).

上記のようにして、ボス円錐面1a全周に亘つ
て翼ユニツト2,2…を被着した後、各翼ユニツ
ト2,2…における係合片15,15…及び1
6,16…の突起17,17…及び20,20…
にそれぞれ端板19及び22の通孔24a,24
a…あるいは24b,24b……及び26…を嵌
合して、端板19及び22を仮止めし、ビス28
及び29で固着する。
After the blade units 2, 2... are attached over the entire circumference of the boss conical surface 1a as described above, the engaging pieces 15, 15... and 1 of each blade unit 2, 2... are attached.
6, 16... protrusions 17, 17... and 20, 20...
through holes 24a and 24 in end plates 19 and 22, respectively.
a... or 24b, 24b... and 26..., temporarily fasten the end plates 19 and 22, and screw 28
and fixed at 29.

又、翼枚数は、以上の説明においては、12枚と
8枚とに変更するものであつたが、これは、例え
ば12枚と9枚等任意に決定することができる。た
だしこの場合には、前側及び後側の端板の通孔の
数を適宜選択決定する必要がある。
Further, in the above explanation, the number of blades was changed to 12 and 8, but this can be arbitrarily determined, for example, 12 and 9. However, in this case, it is necessary to appropriately select and determine the number of through holes in the front and rear end plates.

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、截頭円錐状のボス1と、翼片
11の基端部11aに前記ボス1の円錐面1aに
沿う形状の間隔片12を一体形成し且つ該間隔片
12の周方向端部に前記ボス1の円錐面1aに沿
う形状の重合片13を一体に延設してなる所定数
の翼ユニツト2,2…とからなり、前記各間隔片
12の前縁部と重合片13の中間部位とに、前記
ボス1の軸方向前後端面間と略同間隔となる係合
片15,16を求心方向に突設し且つ該係合片1
5,16間に、前記ボス1の軸方向前後端面を挟
み込むようにし、しかも隣り合う翼ユニツト2,
2…の間隔片12,12…と重合片13,13…
とが所望の翼枚数に応じた重合割合で重合し合う
如くして前記ボス1の円錐面1aに前記翼ユニツ
ト2,2…を配設するようにしたので、ボス1に
対する翼ユニツト2,2……の組付が、係合片1
5,16によるボス1の軸方向前後端面間への挟
み込みという簡易な手段で行なわれるとともに、
同一のボス1に対して同一の翼ユニツト2,2…
を被着するに際して間隔片12と重合片13との
重合割合を変更するだけで、任意の翼枚数の羽根
車を製作することができるため、翼ユニツト用の
金型を多種類容易する必要がなくなり、生産性向
上および製作コストの大巾低減を図り得るという
実用的な効果がある。
According to the present invention, a truncated conical boss 1 and a spacing piece 12 having a shape along the conical surface 1a of the boss 1 are integrally formed on the base end 11a of the wing piece 11, and the spacing piece 12 has a circumferential direction. It consists of a predetermined number of wing units 2, 2... each having an overlapping piece 13 extending along the conical surface 1a of the boss 1 at its end, and the front edge of each spacing piece 12 and the overlapping piece. Engagement pieces 15 and 16 are provided at an intermediate portion of the boss 1 in a centripetal direction with substantially the same spacing as between the front and rear end surfaces of the boss 1, and the engagement pieces 1
The front and rear end surfaces of the boss 1 in the axial direction are sandwiched between the blade units 5 and 16, and the adjacent blade units 2,
2... spacer pieces 12, 12... and overlapping pieces 13, 13...
The blade units 2, 2, etc. are arranged on the conical surface 1a of the boss 1 in such a way that the blade units 2, 2, etc. are superimposed on each other at a polymerization ratio corresponding to the desired number of blades. The assembly of ... is the engagement piece 1.
5 and 16 between the front and rear end surfaces of the boss 1 in the axial direction, and
The same wing unit 2, 2... for the same boss 1.
It is possible to manufacture an impeller with any number of blades by simply changing the polymerization ratio of the spacing piece 12 and the polymerization piece 13 when applying the impeller, so there is no need to easily create a wide variety of molds for the blade unit. This has the practical effect of improving productivity and significantly reducing manufacturing costs.

また、前記間隔片12の前縁部に形成された係
合片15外面に、位置決め用の突起17を突設す
る一方、前記ボス1の截頭面1bに固定される端
板19に、前記係合片15の突起17が選択的に
嵌挿される複数の通孔24,24…を形成したの
で、翼ユニツト2,2…の配設枚数に応じて間隔
片12と重合片13との重合割合を変更する際に
おける翼ユニツト2,2…の位置決めを、前記突
起17の通孔24,24…に対する選択的嵌挿に
よつて行うことができることとなり、翼ユニツト
2,2…のボス1への組付けが極めて容易となる
という効果もある。
Further, a positioning protrusion 17 is provided on the outer surface of the engagement piece 15 formed on the front edge of the spacer piece 12, while an end plate 19 fixed to the truncated surface 1b of the boss 1 is provided with the Since a plurality of through holes 24, 24... are formed into which the protrusions 17 of the engaging pieces 15 are selectively inserted, the spacing pieces 12 and the overlapping pieces 13 can overlap depending on the number of blade units 2, 2... arranged. When changing the ratio, the blade units 2, 2... can be positioned by selectively fitting the projections 17 into the through holes 24, 24... Another advantage is that the assembly becomes extremely easy.

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

第1図は、先出願の斜流送風機の羽根車の正面
図、第2図は、本考案の実施例にかかる斜流送風
機の羽根車の縦断面図、第3図は、第2図の羽根
車におけるボス部の分解斜視図、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
及び第6図は、本考案の実施例にかかる羽根車に
おいて翼枚数を変更した時(12枚から8枚)の組
立途中の正面図、第7図は第6図の−断面図
である。 1……ボス、1a……円錐面、1b……截頭
面、2……翼ユニツト、11……翼片、11a…
…翼片の基端部、12……間隔片、13……重合
片、15,16……係合片、17……突起、19
……端板。
Fig. 1 is a front view of the impeller of the mixed flow blower of the earlier application, Fig. 2 is a longitudinal sectional view of the impeller of the mixed flow blower according to the embodiment of the present invention, and Fig. 3 is the same as that of Fig. 2. Figure 4 is an exploded perspective view of the boss portion of the impeller.
FIGS. 5 and 6 are a perspective view of the blade unit in the impeller shown in FIG. FIG. 7 is a cross-sectional view taken from FIG. DESCRIPTION OF SYMBOLS 1... Boss, 1a... Conical surface, 1b... Trunked surface, 2... Wing unit, 11... Wing piece, 11a...
...Base end of wing piece, 12... Spacing piece, 13... Overlapping piece, 15, 16... Engagement piece, 17... Protrusion, 19
...end plate.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 截頭円錐状のボス1と、翼片11の基端部11
aに前記ボス1の円錐面1aに沿う形状の間隔片
12を一体形成し且つ該間隔片12の周方向端部
に前記ボス1の円錐面1aに沿う形状の重合片1
3を一体に延設してなる所定数の翼ユニツト2,
2…とからなり、前記各間隔片12の前縁部と重
合片13の中間部位とには、前記ボス1の軸方向
前後端面間と略同間隔となる係合片15,16を
求心方向に突設し且つ該係合片15,16間に、
前記ボス1の軸方向前後端面を挟み込むように
し、しかも隣り合う翼ユニツト2,2…の間隔片
12,12…と重合片13,13…とが所望の翼
枚数に応じた重合割合で重合し合う如くして前記
ボス1の円錐面1aに前記翼ユニツト2,2…を
配設するとともに、前記間隔片12の前縁部に形
成された係合片15外面には、位置決め用の突起
17を突設する一方、前記ボス1の截頭面1bに
固定される端板19には、前記係合片15の突起
17が選択的に嵌挿される複数の通孔24,24
…を形成したことを特徴とする斜流送風機の羽根
車。
A frustoconical boss 1 and a base end 11 of a wing piece 11
a spacer piece 12 having a shape that follows the conical surface 1a of the boss 1 is integrally formed thereon, and an overlapping piece 1 that has a shape that follows the conical surface 1a of the boss 1 at the circumferential end of the spacer piece 12;
A predetermined number of wing units 2,
2... At the front edge of each spacing piece 12 and the intermediate portion of the overlapping piece 13, engaging pieces 15 and 16 are provided in the centripetal direction at approximately the same distance as between the front and rear end surfaces of the boss 1 in the axial direction. and between the engaging pieces 15 and 16,
The front and rear end surfaces of the boss 1 in the axial direction are sandwiched, and the spacing pieces 12, 12... of the adjacent blade units 2, 2... and the overlapping pieces 13, 13... overlap at a polymerization ratio corresponding to the desired number of blades. The blade units 2, 2, . The end plate 19 fixed to the truncated surface 1b of the boss 1 has a plurality of through holes 24, 24 into which the projections 17 of the engagement piece 15 are selectively inserted.
An impeller for a mixed flow blower characterized by forming...
JP10752782U 1982-07-13 1982-07-13 mixed flow blower impeller Granted JPS5911197U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP10752782U JPS5911197U (en) 1982-07-13 1982-07-13 mixed flow blower impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP10752782U JPS5911197U (en) 1982-07-13 1982-07-13 mixed flow blower impeller

Publications (2)

Publication Number Publication Date
JPS5911197U JPS5911197U (en) 1984-01-24
JPS6237999Y2 true JPS6237999Y2 (en) 1987-09-28

Family

ID=30251214

Family Applications (1)

Application Number Title Priority Date Filing Date
JP10752782U Granted JPS5911197U (en) 1982-07-13 1982-07-13 mixed flow blower impeller

Country Status (1)

Country Link
JP (1) JPS5911197U (en)

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4815603B1 (en) * 1969-12-29 1973-05-16
JPS5037525U (en) * 1973-07-27 1975-04-18

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5042403Y2 (en) * 1971-06-30 1975-12-02

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS4815603B1 (en) * 1969-12-29 1973-05-16
JPS5037525U (en) * 1973-07-27 1975-04-18

Also Published As

Publication number Publication date
JPS5911197U (en) 1984-01-24

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