JP4695687B2 - Impeller, fan device, and impeller manufacturing method - Google Patents

Impeller, fan device, and impeller manufacturing method Download PDF

Info

Publication number
JP4695687B2
JP4695687B2 JP2008329214A JP2008329214A JP4695687B2 JP 4695687 B2 JP4695687 B2 JP 4695687B2 JP 2008329214 A JP2008329214 A JP 2008329214A JP 2008329214 A JP2008329214 A JP 2008329214A JP 4695687 B2 JP4695687 B2 JP 4695687B2
Authority
JP
Japan
Prior art keywords
impeller
connecting member
central axis
mold
widened portion
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.)
Active
Application number
JP2008329214A
Other languages
Japanese (ja)
Other versions
JP2010151009A (en
Inventor
旭 比護
充 伊藤
哲也 日沖
太郎 旦野
治 関口
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.)
Nidec Advanced Motor Corp
Original Assignee
Nidec Servo Corp
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 Nidec Servo Corp filed Critical Nidec Servo Corp
Priority to JP2008329214A priority Critical patent/JP4695687B2/en
Priority to CN2009101757287A priority patent/CN101713417B/en
Priority to US12/570,330 priority patent/US8317478B2/en
Priority to DE102009048382A priority patent/DE102009048382A1/en
Publication of JP2010151009A publication Critical patent/JP2010151009A/en
Application granted granted Critical
Publication of JP4695687B2 publication Critical patent/JP4695687B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Landscapes

  • Structures Of Non-Positive Displacement Pumps (AREA)

Description

本発明は、複数の翼同士を連結する略環状の連結部材を有するインペラ、ファン装置及びインペラの製造方法に関する。   The present invention relates to an impeller having a substantially annular connecting member that connects a plurality of blades, a fan device, and a method for manufacturing the impeller.

インペラは回転することによって、翼自体に遠心力が働く。遠心力は、翼の支持部との付け根から見て半径方向と略平行に発生する。高速で回転するインペラは、遠心力によって翼の付け根に発生する応力を考慮した強度設計を施す必要がある。また、遠心力の影響によって、翼が変形し、翼の径方向外端が径方向外方に変位することも懸念される。翼の径方向外端が径方向外方に変位すると、翼の径方向外端がインペラを外囲する外枠体の内側面に接触するおそれもある。この遠心力の影響に対する有効な対策として、例えば、特許文献1〜7等において、翼同士を連結する略環状の連結部材が開示されている。   As the impeller rotates, centrifugal force acts on the blade itself. Centrifugal force is generated substantially parallel to the radial direction when viewed from the root of the blade support. An impeller that rotates at high speed needs to be designed with strength in consideration of the stress generated at the base of the wing by centrifugal force. Further, there is a concern that the blade is deformed by the influence of centrifugal force and the radially outer end of the blade is displaced radially outward. If the radially outer end of the blade is displaced radially outward, the radially outer end of the blade may come into contact with the inner surface of the outer frame that surrounds the impeller. As an effective measure against the influence of this centrifugal force, for example, Patent Documents 1 to 7 disclose a substantially annular connecting member that connects blades.

また、インペラは、製造コスト及び量産性等の観点より射出成形により製造される場合が多い。射出成形用の金型には、インペラの中心軸方向に離型する1組の金型が用いられる。その1組の金型は、例えば固定側の金型と可動側の金型とから構成されている。   Further, the impeller is often manufactured by injection molding from the viewpoint of manufacturing cost and mass productivity. As a mold for injection molding, a set of molds that are released in the central axis direction of the impeller is used. The one set of molds is composed of, for example, a fixed mold and a movable mold.

このような1組の金型の少なくもいずれか一方側の金型には、中心軸方向に進退可能に設けられ、インペラを金型から押し出す可動部(イジェクターピンと呼ばれる場合がある)が設けられており、その可動部によって成形後のインペラが金型から離反される。金型に対する可動部の配置は、インペラの形状、及び、インペラと金型が密着している密着部分の分布等を考慮して決定される。   At least one of these sets of molds is provided with a movable part (sometimes called an ejector pin) that is provided so as to be able to advance and retreat in the direction of the central axis and push the impeller out of the mold. The impeller after molding is separated from the mold by the movable part. The arrangement of the movable part with respect to the mold is determined in consideration of the shape of the impeller, the distribution of the close contact portion where the impeller and the mold are in close contact, and the like.

また、可動部による金型からのインペラの押し出しは、射出成形された樹脂材料が完全に硬化する前の状態で行われるため、可動部により押圧されたインペラの部分に変形(圧痕も含む。以下同様)が生じる場合がある。このため、可動部の受けとなるインペラの部分として、翼等のように、変形の生じやすい部分又は変形による流体特性の悪化が問題となり易い部分を避け、インペラの中央の支持部等に避けられる場合が多い。   Further, since the impeller is pushed out of the mold by the movable portion, it is performed in a state before the injection-molded resin material is completely cured, so that the impeller portion pressed by the movable portion is deformed (including an indentation). The same may occur. For this reason, as a part of the impeller that receives the movable part, a part that is likely to be deformed or a part that is liable to be deteriorated in fluid characteristics due to the deformation, such as a wing, is avoided, and a support part in the center of the impeller can be avoided. There are many cases.

上述のような複数の翼同士を連結する連結部材を有するインペラの場合では、翼の径方向外方に略環状の連結部材が設けられているため、インペラの径方向外方におけるインペラと金型との密着部分が増大している。このため、射出成形後の離型を容易にするためには、金型の可動部の受けを連結部材の部分にも追加で設けるか、あるいは可動部の受けを支持部の代わりに連結部材の部分に設ける必要がある。その結果、連結部材には可動部による押圧に耐え得るだけの強度が求められる。   In the case of an impeller having a connecting member for connecting a plurality of blades as described above, a substantially annular connecting member is provided on the radially outer side of the blade, so that the impeller and the mold on the radially outer side of the impeller There is an increase in the close contact area. For this reason, in order to facilitate mold release after injection molding, a receiving part for the movable part of the mold is additionally provided in the part of the connecting member, or a receiving part for the moving part is used instead of the supporting part. It is necessary to provide in the part. As a result, the connecting member is required to have enough strength to withstand the pressing by the movable part.

連結部材に設けられる可動部の受けは、連結部材におけるインペラの中心軸方向の両側を向いた2つの面のうちの少なくもいずれか一方に設けられる。このため、連結部材の可動部による押圧に対する強度を向上させるための構成としては、例えば、連結部材の径方向の厚みを周方向の全体で増大させた構成が考えられる。しかし、連結部材の全体で径方向の厚みを増大すると、翼によって発生される空気流と連結部材との干渉の度合いが増し、インペラの流体特性が悪化する。また、連結部材の厚みが増大すると、インペラの質量が増大し、インペラを回転させるために必要なトルクが増大し、効率低下が低下する。
米国意匠特許第D511824号公報 米国特許出願公開第2008/0056899号公報 米国特許第6554574号公報 米国特許第4684324号公報 米国特許第4569631号公報 米国特許第4569632号公報 米国特許第6241474号公報
The receiving part of the movable part provided in the connecting member is provided on at least one of the two surfaces facing both sides of the impeller in the central axis direction of the impeller. For this reason, as a structure for improving the intensity | strength with respect to the press by the movable part of a connection member, the structure which increased the thickness of the radial direction of the connection member in the whole circumferential direction can be considered, for example. However, when the radial thickness of the entire connecting member is increased, the degree of interference between the air flow generated by the blade and the connecting member increases, and the fluid characteristics of the impeller deteriorate. Further, when the thickness of the connecting member increases, the mass of the impeller increases, the torque required to rotate the impeller increases, and the efficiency reduction decreases.
US Design Patent No. D511824 US Patent Application Publication No. 2008/0056899 US Pat. No. 6,554,574 US Pat. No. 4,684,324 U.S. Pat. No. 4,569,631 U.S. Pat. No. 4,569,632 US Pat. No. 6,241,474

そこで、本発明の解決すべき課題は、複数の翼同士を連結する略環状の連結部材が設けられたインペラにおいて、射出成形用の金型に設けられた可動部による離型時の押圧によって連結部材の変形が生じるのを回避できるとともに、径方向の厚み増大による連結部材の流体特性の悪化及び質量の増大も抑制できるインペラ、ファン装置及びインペラの製造方法を提供することである。   Therefore, the problem to be solved by the present invention is that an impeller provided with a substantially annular connecting member for connecting a plurality of blades is connected by pressing at the time of mold release by a movable part provided in a mold for injection molding. An object of the present invention is to provide an impeller, a fan device, and a method of manufacturing an impeller that can prevent deformation of the member and can suppress deterioration in fluid characteristics and increase in mass due to an increase in radial thickness.

上記の課題を解決するため、本発明のインペラにあっては、中心軸を中心とした円筒状外側面を有する支持部と、前記支持部の前記円筒状外側面から径方向外方に向けて延伸して形成され、前記支持部と共に前記中心軸を中心に回転することで前記中心軸方向の空気流を発生する複数の翼と、前記中心軸を中心とした周方向に沿って形成され、前記中心軸方向の両側をそれぞれ向いた2つの面を有し、前記複数の翼同士を連結する略環状の連結部材とを備え、前記支持部、前記複数の翼及び前記連結部材は、連続した樹脂部材により一体に成形されており、前記連結部材の前記2つの面の少なくともいずれか一方に、該面の径方向の幅が部分的に拡大されてなる少なくとも1つの拡幅部が設けられている。   In order to solve the above problems, in the impeller of the present invention, a support portion having a cylindrical outer surface centered on a central axis, and radially outward from the cylindrical outer surface of the support portion. A plurality of blades that are formed by stretching and rotate around the central axis together with the support portion, and are formed along a circumferential direction centered on the central axis; The support unit, the plurality of blades, and the connecting member are continuous with each other, having two surfaces facing both sides in the central axis direction, and a substantially annular connecting member that connects the plurality of blades. The resin member is integrally formed, and at least one of the two surfaces of the connecting member is provided with at least one widened portion obtained by partially expanding the radial width of the surface. .

上記した本発明に係るインペラにおいて、前記拡幅部を、前記中心軸方向から見て、該拡幅部が設けられる前記連結部材の前記面における前記翼と重なる重複区間内のいずれかの位置に配置することができる。   In the above-described impeller according to the present invention, the widened portion is disposed at any position in the overlapping section overlapping the wing on the surface of the connecting member provided with the widened portion when viewed from the central axis direction. be able to.

この場合、前記拡幅部は、前記重複区間の前記周方向の両側の第1及び第2の端のうち、該端と前記翼との前記中心軸方向に沿った距離が大きい方の第1の端と、前記重複区間の前記周方向に対する中間位置との間におけるいずれかの位置に配置されているのがよい。   In this case, the widened portion is the first of the first and second ends on both sides in the circumferential direction of the overlapping section, which has a larger distance along the central axis direction between the end and the wing. It is good to arrange at any position between the end and an intermediate position in the circumferential direction of the overlapping section.

特に、前記拡幅部は、前記重複区間の前記第1の端と前記中間位置との間において、前記周方向に対して前記中間位置よりも前記第1の端に近い位置に配置されているのがなおよい。   In particular, the widened portion is disposed between the first end of the overlapping section and the intermediate position at a position closer to the first end than the intermediate position with respect to the circumferential direction. Is even better.

また、上記した本発明に係るインペラにおいて、前記拡幅部を、前記重複区間の前記周方向の両側の第1及び第2の端のうち、該端と前記翼との前記中心軸方向に沿った距離が大きい方の第1の端の近傍に配置するようにしてもよい。   Further, in the impeller according to the present invention described above, the widened portion is arranged along the central axis direction of the end and the blade among the first and second ends on both sides in the circumferential direction of the overlapping section. You may make it arrange | position in the vicinity of the 1st end with a larger distance.

また、本発明に係るインペラにおいて、前記拡幅部を、前記複数の翼にそれぞれ対応して得られる複数の前記重複区間内にそれぞれ配置するのが望ましい。   In the impeller according to the present invention, it is preferable that the widened portion is disposed in each of the plurality of overlapping sections obtained corresponding to the plurality of blades.

上記した本発明に係るインペラにおいて、前記拡幅部が、前記樹脂部材を成形する金型に進退可能に設けられ、前記樹脂部材を前記金型から押し出す可動部の受けを形成するものとすることができる。   In the above-described impeller according to the present invention, the widened portion is provided so as to be able to advance and retreat in a mold for molding the resin member, and forms a receiving portion of a movable portion that pushes the resin member from the mold. it can.

また、上記の課題を解決するため、発明のファン装置では、上述した発明に係る前記インペラと、前記インペラを駆動するモータと、前記インペラを外囲する外枠体と、前記外枠体の径方向内方に設けられ、前記モータを支持する支持体とを備えて構成される。   In order to solve the above problems, in the fan device of the invention, the impeller according to the invention described above, a motor that drives the impeller, an outer frame body that surrounds the impeller, and a diameter of the outer frame body And a support body that is provided inward in the direction and supports the motor.

また、上記の課題を解決するため、本発明のインペラの製造方法にあっては、中心軸を中心とした円筒状外側面を有する支持部と、前記支持部の前記円筒状外側面から径方向外方に向けて延伸して形成され、前記支持部と共に前記中心軸を中心に回転することで前記中心軸方向の空気流を発生する複数の翼と、前記中心軸を中心とした周方向に沿って形成され、前記中心軸方向の両側をそれぞれ向いた2つの面を有し、前記複数の翼同士を連結する略環状の連結部材とを備え、かつ、前記連結部材の前記2つの面の少なくともいずれか一方に、該面の径方向の幅が部分的に拡大されてなる少なくとも1つの拡幅部が設けられてなるインペラの製造方法であって、前記中心軸方向に離型する1組の金型によって形成された閉空間内に樹脂を射出することにより、前記インペラの前記支持部、前記複数の翼及び前記連結部材を連続した樹脂部材として一体に形成する工程と、前記金型を前記中心軸方向に離型するとともに、前記金型に前記中心軸方向に進退可能に設けられた可動部によって、前記樹脂部材における前記連結部材の前記拡幅部を前記金型から離反する方向に押し出す工程とを備える。   In order to solve the above problems, in the impeller manufacturing method of the present invention, a support portion having a cylindrical outer surface centered on a central axis, and a radial direction from the cylindrical outer surface of the support portion A plurality of blades that are formed to extend outward and rotate around the central axis together with the support portion, and in a circumferential direction centered on the central axis by generating airflow in the central axis direction. Two surfaces facing each other on both sides in the central axis direction, and a substantially annular connecting member for connecting the plurality of blades, and the two surfaces of the connecting member An impeller manufacturing method in which at least one of the at least one widened portion formed by partially expanding the radial width of the surface is provided on at least one of the surfaces, and a set of molds released in the central axis direction Resin is injected into the closed space formed by the mold. The step of integrally forming the support portion of the impeller, the plurality of blades and the connecting member as a continuous resin member, and releasing the mold in the central axis direction, And a step of pushing out the widened portion of the connecting member of the resin member in a direction away from the mold by a movable portion provided to be movable back and forth in the central axis direction.

本発明のインペラによれば、複数の翼同士を連結する略環状の連結部材におけるインペラの中心軸方向の両側の2つの面の少なくともいずれか一方に、該面の径方向の幅が部分的に拡大されてなる少なくとも1つの拡幅部が設けられている。それ故、インペラの支持部、複数の翼及び連結部材を、中心軸方向に離型する1組の金型を用いて射出成形により成形する場合に、連結部材の拡幅部を、成形品を金型から離反させるために金型に設けられた可動部の受けとすることができる。連結部材の拡幅部では、径方向の幅が部分的に拡大され、強度が向上されているため、可動部による離型時の押圧によって連結部材の変形が生じるのを回避できる。しかも、連結部材の前記2つの面の少なくともいずれか一方において、該面の径方向の幅を部分的に拡大して拡幅部を形成しているため、径方向の厚み増大による連結部材の流体特性の悪化及び質量の増大も抑制できる。   According to the impeller of the present invention, at least one of the two surfaces on both sides in the central axis direction of the impeller in the substantially annular connecting member that connects the plurality of blades partially has a radial width of the surface. At least one widened portion is provided which is enlarged. Therefore, when the impeller support section, the plurality of blades and the connecting member are molded by injection molding using a pair of molds that are released in the direction of the central axis, the widened portion of the connecting member is made of a molded product. It can be a receiving part of a movable part provided in the mold for separating from the mold. In the widened portion of the connecting member, since the radial width is partially enlarged and the strength is improved, it is possible to avoid the deformation of the connecting member due to the pressing at the time of releasing by the movable portion. Moreover, since at least one of the two surfaces of the connecting member partially enlarges the radial width of the surface to form a widened portion, the fluid characteristics of the connecting member due to an increase in radial thickness. It is also possible to suppress the deterioration and mass increase.

上記インペラにおいて、拡幅部を連結部材の面における翼と重なる位置に配置するようにすれば、射出成形後にインペラの支持部、複数の翼及び連結部材を構成する樹脂部材を、可動部によって金型から押し出して離反させるときに、翼及び連結部材の変形を生じることなく、容易に離反させることができる。すなわち、翼の部分は金型との密着面積が大きいため、連結部材を金型の可動部によって押圧して前記樹脂部材を金型から離反させるときに、樹脂部材と翼の結合部分に負荷がかかり易い。本発明では、拡幅部を、中心軸方向から見て、該拡幅部が設けられる連結部材の前記面における翼と重なる重複区間内のいずれかの位置に配置したため、金型の可動部によって連結部材における翼と結合されている部分を押圧して前記樹脂部材を金型から離反させることができる。その結果、前記樹脂部材を可動部によって金型から押し出して離反させるときに、翼及び連結部材の変形を生じることなく、前記樹脂部材を容易に離反させることができる。   In the impeller, if the widened portion is arranged at a position overlapping the blades on the surface of the connecting member, the resin member constituting the impeller support portion, the plurality of blades and the connecting member is molded by the movable portion after the injection molding. When being pushed away from each other, the blades and the connecting members can be easily separated without causing deformation. That is, since the wing portion has a large contact area with the mold, when the connecting member is pressed by the movable portion of the mold and the resin member is separated from the mold, a load is applied to the joint portion between the resin member and the wing. Easy to take. In the present invention, since the widened portion is disposed at any position in the overlapping section overlapping with the wings on the surface of the connecting member provided with the widened portion when viewed from the central axis direction, the connecting member is moved by the movable portion of the mold. The portion that is connected to the wings of the resin can be pressed to separate the resin member from the mold. As a result, when the resin member is pushed away from the mold by the movable part, the resin member can be easily separated without causing deformation of the wing and the connecting member.

ここで、インペラの翼は、翼の延伸方向と垂直な面で翼を切断したときの断面形状が中心軸方向と垂直な面に対して傾斜している。このため、連結部材の拡幅部が設けられる前記面の前記重複区間内における周方向の位置によって、前記面から翼までの中心軸方向に沿った距離が変化する。これに伴い、前記重複区間に対応する連結部材の径方向内側面又は外側面における部分と、前記可動部が設けられる金型との密着の度合いも、前記重複区間内における周方向の位置によって変化し、前記面から翼までの中心軸方向に沿った距離が大きい程、密着の度合いが大きくなる。   Here, the impeller blades are inclined with respect to a plane perpendicular to the central axis direction when the blade is cut along a plane perpendicular to the extending direction of the blades. For this reason, the distance along the center axis direction from the said surface to a wing | blade changes with the circumferential position in the said overlap area of the said surface in which the wide part of a connection member is provided. Accordingly, the degree of close contact between the portion on the radially inner side surface or the outer side surface of the connecting member corresponding to the overlapping section and the mold on which the movable portion is provided also varies depending on the circumferential position in the overlapping section. However, the greater the distance along the central axis direction from the surface to the wing, the greater the degree of adhesion.

本発明において、拡幅部を、前記重複区間の周方向の両側の第1及び第2の端のうち、該端と翼との中心軸方向に沿った距離が大きい方の第1の端と、前記重複区間の周方向に対する中間位置との間におけるいずれかの位置に配置すれば、連結部材の前記重複区間内において、前記重複区間に対応する連結部材の径方向内側面又は外側面の部分と、可動部が設けられる金型との密着の度合いが大きい部分に可動部の受けを設けることができる。その結果、前記樹脂部材を可動部によって金型から押し出して離反させるときに、翼及び連結部材の変形をより確実に防止しながら、前記樹脂部材を容易に離反させることができる。   In the present invention, the widened portion of the first and second ends on both sides in the circumferential direction of the overlapping section, the first end having a larger distance along the central axis direction between the end and the wing, If it is disposed at any position between the intermediate position with respect to the circumferential direction of the overlapping section, in the overlapping section of the connecting member, the radially inner side surface or the outer surface portion of the connecting member corresponding to the overlapping section; The receiving part of the movable part can be provided at a portion where the degree of close contact with the mold provided with the movable part is large. As a result, when the resin member is pushed away from the mold by the movable portion, the resin member can be easily separated while preventing the wing and the connecting member from being deformed more reliably.

特に、拡幅部が、前記重複区間の前記第1の端と前記中間位置との間において、周方向に対して前記中間位置よりも前記第1の端に近い位置に配置されているように構成すれば、インペラの連結部材における前記重複区間のうち、前記重複区間に対応する連結部材の径方向内側面又は外側面の部分と、可動部が設けられる金型との密着の度合いがより大きい部分に可動部の受けを設けることができる。その結果、前記樹脂部材を可動部によって金型から押し出して離反させるときに、翼及び連結部材の変形をさらに確実に防止しながら、前記樹脂部材を容易に離反させることができる。   In particular, the widened portion is configured to be disposed at a position closer to the first end than the intermediate position in the circumferential direction between the first end and the intermediate position of the overlapping section. Then, among the overlapping sections in the connecting member of the impeller, a portion having a higher degree of adhesion between the radially inner side surface or the outer side surface of the connecting member corresponding to the overlapping section and the mold on which the movable portion is provided A receiving part for the movable part can be provided. As a result, when the resin member is pushed away from the mold by the movable part, the resin member can be easily separated while further reliably preventing deformation of the wing and the connecting member.

また、本発明において、拡幅部を、前記重複区間の周方向の両側の第1及び第2の端のうち、該端と翼との中心軸方向に沿った距離が大きい方の第1の端の近傍に配置するようにすれば、インペラの連結部材における前記重複区間のうち、前記重複区間に対応する連結部材の径方向内側面又は外側面の部分と、可動部が設けられる金型との密着の度合いが最も大きい部分の近傍に可動部の受けを設けることができる。その結果、前記樹脂部材を可動部によって金型から押し出して離反させるときに、翼及び連結部材の変形をさらに確実に防止しながら、前記樹脂部材を容易に離反させることができる。   Further, in the present invention, the widened portion is a first end having a larger distance along the central axis direction between the end and the wing among the first and second ends on both sides in the circumferential direction of the overlapping section. In the overlapping section of the impeller connecting member, the radially inner side surface or the outer surface portion of the connecting member corresponding to the overlapping section and the mold provided with the movable portion A receiving part for the movable part can be provided in the vicinity of the part having the greatest degree of adhesion. As a result, when the resin member is pushed away from the mold by the movable part, the resin member can be easily separated while further reliably preventing deformation of the wing and the connecting member.

さらに、本発明において、拡幅部を、すべての翼にそれぞれ対応して得られる複数の前記重複区間内にそれぞれ配置すれば、前記樹脂部材を可動部によって金型から押し出して離反させるときに、すべての翼について、翼及び翼と連結部材の結合部分における変形をより確実に防止しながら、前記樹脂部材を容易に離反させることができる。   Further, in the present invention, when the widened portion is arranged in each of the plurality of overlapping sections obtained corresponding to all the blades, when the resin member is pushed away from the mold by the movable portion, all With respect to the wing, the resin member can be easily separated while more reliably preventing the wing and the joint between the wing and the connecting member from being deformed.

上述した本発明のインペラにおいて、拡幅部が成型金型の可動部の受けを形成する構成とすれば、複数の翼同士を連結する略環状の連結部材が設けられたインペラにおいて、射出成形用の金型に設けられた可動部による離型時の押圧によって連結部材の変形が生じるのを回避できるとともに、径方向の厚み増大による連結部材の流体特性の悪化及び質量の増大も抑制できる。   In the impeller of the present invention described above, if the widened portion forms a receiving part of the movable part of the molding die, the impeller provided with a substantially annular connecting member for connecting a plurality of blades is used for injection molding. It is possible to avoid the deformation of the connecting member due to the pressing at the time of releasing by the movable part provided in the mold, and it is possible to suppress the deterioration of the fluid characteristics and the increase of the mass of the connecting member due to the increase in the radial thickness.

本発明のファン装置によれば、上述したインペラが、射出成形後の金型の可動部による押し出しによってインペラの複数の翼を連結する略環状の連結部材に変形が生じるのが回避されているとともに、径方向の厚み増大による連結部材の流体特性の悪化及び質量の増大も抑制されているため、安定して効率よく空気流を発生させることができる。   According to the fan device of the present invention, the above-described impeller is prevented from being deformed in the substantially annular connecting member that connects the plurality of impeller blades due to extrusion by the movable portion of the mold after injection molding. Since the deterioration of the fluid characteristics and the increase in mass of the connecting member due to the increase in the radial thickness are suppressed, an air flow can be generated stably and efficiently.

さらに、本発明のインペラの製造方法によれば、複数の翼同士を連結する略環状の連結部材におけるインペラの中心軸方向の両側の2つの面の少なくともいずれか一方に、該面の径方向の幅が部分的に拡大されてなる少なくとも1つの拡幅部が設けられている。また、インペラの支持部、複数の翼及び連結部材を、中心軸方向に離型する1組の金型を用いて射出成形により成形する場合に、連結部材の拡幅部が、成形品を金型から離反させるために金型に設けられた可動部の受けとなっている。それ故、その連結部材の拡幅部では、径方向の幅が部分的に拡大され、強度が向上されているため、可動部による離型時の押圧によって連結部材の変形が生じるのを回避できる。しかも、連結部材の前記2つの面の少なくともいずれか一方において、該面の径方向の幅を部分的に拡大して拡幅部を形成しているため、径方向の厚みの増大による連結部材の流体特性の悪化及び質量の増大も抑制できる。   Furthermore, according to the impeller manufacturing method of the present invention, at least one of the two surfaces on both sides in the central axis direction of the impeller in the substantially annular connecting member that connects the plurality of blades is arranged in the radial direction of the surface. At least one widened portion having a partially enlarged width is provided. In addition, when the impeller support portion, the plurality of blades, and the connecting member are molded by injection molding using a set of molds that are released in the central axis direction, the widened portion of the connecting member is used to mold the molded product. It is a receiving part of the movable part provided in the mold in order to be separated from the mold. Therefore, in the widened portion of the connecting member, since the radial width is partially enlarged and the strength is improved, it is possible to avoid the deformation of the connecting member due to the pressing at the time of releasing by the movable portion. In addition, since at least one of the two surfaces of the connecting member partially enlarges the radial width of the surface to form a widened portion, the fluid of the connecting member due to an increase in the radial thickness. The deterioration of characteristics and the increase in mass can also be suppressed.

図1は本発明の一実施形態に係るインペラ1の中心軸17方向吸気側から見た斜視図であり、図2は図1のインペラ1の側面図であり、図3は図1のインペラ1の中心軸17方向排気側から見た底面図であり、図4は図3の一部を拡大して示す図であり、図5は図1のインペラ1における動翼22と連結部材23との結合部分を径方向内側から見た図であり、図6は図1のインペラ1が用いられたファン装置11の断面図である。   FIG. 1 is a perspective view of an impeller 1 according to an embodiment of the present invention as viewed from the intake side in the direction of the central axis 17, FIG. 2 is a side view of the impeller 1 of FIG. 1, and FIG. FIG. 4 is an enlarged view of a part of FIG. 3, and FIG. 5 is a view of the rotor blade 22 and the connecting member 23 in the impeller 1 of FIG. 1. FIG. 6 is a cross-sectional view of the fan device 11 in which the impeller 1 of FIG. 1 is used.

本実施形態に係るインペラ1が用いられたファン装置11は、図6に示すように、インペラ1と、複数の静翼12と、モータ13と、外枠体14と、支持体15とを備えている。静翼12、外枠体14及び支持体15は、このファン装置11のハウジング16を構成している。なお、本実施形態では、静翼12及び支持体15は、インペラ1の中心軸17方向排気側(図6における下方側)に設けられている。   As shown in FIG. 6, the fan device 11 using the impeller 1 according to the present embodiment includes the impeller 1, a plurality of stationary blades 12, a motor 13, an outer frame body 14, and a support body 15. ing. The stationary blade 12, the outer frame body 14, and the support body 15 constitute a housing 16 of the fan device 11. In the present embodiment, the stationary blade 12 and the support 15 are provided on the exhaust side of the impeller 1 in the direction of the central axis 17 (the lower side in FIG. 6).

外枠体14、支持体15及び静翼12は、射出成形により連続した樹脂部材として一体に形成されている。一般的に射出成形に用いられる金型は、ハウジング16に対して中心軸17方向に離型される可動側金型と固定側金型の主に2つの金型部材で構成される。これによって、ファン装置11を安価に量産することができる。   The outer frame body 14, the support body 15, and the stationary blade 12 are integrally formed as a continuous resin member by injection molding. A mold generally used for injection molding is mainly composed of two mold members, a movable mold and a fixed mold which are separated from the housing 16 in the direction of the central axis 17. As a result, the fan device 11 can be mass-produced at low cost.

外枠体14は、インペラ1を外囲するように設けられている。支持体15は、外枠体14の半径方向内方に設けられ、モータ13、及びモータ13を駆動するための駆動回路を構成する図示しない回路基板を支持している。   The outer frame body 14 is provided so as to surround the impeller 1. The support 15 is provided inward of the outer frame 14 in the radial direction, and supports the motor 13 and a circuit board (not shown) that constitutes a drive circuit for driving the motor 13.

静翼12は、外枠体14と支持体15とを連結し、支持体15から径方向外方に向けて放射状に伸延され、中心軸17方向に対して傾斜する受風面を有している。この静翼12の役割には、インペラ1が回転することによって発生された空気流を中心軸17側に集風すること、及び、発生された空気流を径方向内方又は径方向外方などの任意の方向に向けることが含まれる。このような静翼12は、インペラ1が発生させた空気の集風又は方向転換を効率よくできるようにインペラ1の中心軸17方向排気側に設けられている。変形例として、静翼12をインペラ1の中心軸17方向吸気側に設けてもよい。   The stationary blade 12 connects the outer frame body 14 and the support body 15, has a wind receiving surface that extends radially outward from the support body 15 and inclines with respect to the direction of the central axis 17. Yes. The role of the stationary blade 12 is to collect the air flow generated by the rotation of the impeller 1 toward the central shaft 17, and to generate the generated air flow radially inward or radially outward. Pointing in any direction. Such a stationary blade 12 is provided on the exhaust side of the impeller 1 in the direction of the central axis 17 so as to efficiently collect air or change the direction of the air generated by the impeller 1. As a modification, the stationary blade 12 may be provided on the intake side in the direction of the central axis 17 of the impeller 1.

モータ13は、インペラ1の後述する支持部21の内側面に取り付けられたロータマグネット18と、そのロータマグネット18との間でトルクを発生させる電機子19とを備えて構成されている。このようなモータ13は、インペラ1の支持部21内に収容される。   The motor 13 includes a rotor magnet 18 attached to an inner surface of a support portion 21 described later of the impeller 1, and an armature 19 that generates torque between the rotor magnet 18. Such a motor 13 is accommodated in the support portion 21 of the impeller 1.

インペラ1は、図1ないし図5に示すように、支持部21、複数(例えば、7枚)の動翼22、及び連結部材23を備えている。支持部21は、中心軸17を中心とした円筒状外側面21aを有する。本実施形態では、支持部21が中心軸17を中心とした略カップ状の形状を有しており、支持部21の内部にモータ13が収容される。   As shown in FIGS. 1 to 5, the impeller 1 includes a support portion 21, a plurality of (for example, seven) moving blades 22, and a connecting member 23. The support portion 21 has a cylindrical outer surface 21 a centering on the central axis 17. In the present embodiment, the support portion 21 has a substantially cup shape centered on the central shaft 17, and the motor 13 is accommodated inside the support portion 21.

複数の動翼22は、中心軸17を中心とした周方向に間隔を開けて、支持部21の円筒状外側面21aから径方向外方に向けて延伸して形成されている。複数の動翼22は、支持部21と共に中心軸17を中心として回転方向20に回転することで、中心軸17方向の空気流を発生させる。本実施形態では、図1及び図2の上側(中心軸17方向吸気側)から吸い込まれた空気流が、図1及び図2の下側(中心軸17方向排気側)に吐き出される。このため、動翼22は、動翼22の回転方向20前方側縁部22aが回転方向20後方側縁部22bよりも中心軸17方向吸気側に位置するように、動翼22の延伸方向と垂直な面で動翼を切断したときの断面形状が中心軸17と垂直な面に対して傾斜している。   The plurality of moving blades 22 are formed to extend radially outward from the cylindrical outer surface 21a of the support portion 21 with a space in the circumferential direction around the central axis 17. The plurality of moving blades 22 rotate in the rotation direction 20 around the central axis 17 together with the support portion 21 to generate an air flow in the direction of the central axis 17. In the present embodiment, the air flow sucked from the upper side in FIG. 1 and FIG. 2 (center axis 17 direction intake side) is discharged to the lower side (center axis 17 direction exhaust side) of FIG. 1 and FIG. For this reason, the moving blade 22 has the extending direction of the moving blade 22 so that the front edge 22a in the rotation direction 20 of the moving blade 22 is located closer to the intake side in the direction of the central axis 17 than the rear edge 22b in the rotation direction 20. The cross-sectional shape when the moving blade is cut on a vertical plane is inclined with respect to the plane perpendicular to the central axis 17.

また、本実施形態では、動翼22に前進動翼が採用されており、動翼22が、その径方向内方側の支持部21との付け根から径方向に離反するに従って回転方向20前方側に大きく湾曲している。このような前進動翼を採用することにより、動翼22によって発生される空気流を径方向外方に広がるのを抑えながら送り出すことができる。   Further, in the present embodiment, a forward moving blade is adopted as the moving blade 22, and the moving blade 22 moves forward in the rotational direction 20 as it moves away in the radial direction from the root of the support portion 21 on the radially inner side. Is greatly curved. By adopting such a forward moving blade, the air flow generated by the moving blade 22 can be sent out while being prevented from spreading radially outward.

連結部材23は、遠心力による影響に対して動翼22の補強用に設けられる略環状の部材であり、中心軸17を中心とした周方向に沿って形成され、複数の動翼22同士を連結する。より詳細には、連結部材23は、中心軸17に沿って延びる略円筒形状を有し、各動翼22の径方向内方側端部と径方向外方側端部との間における径方向外方側寄りの部分と結合されている。   The connecting member 23 is a substantially annular member provided to reinforce the moving blade 22 against the influence of centrifugal force. The connecting member 23 is formed along the circumferential direction around the central axis 17, and connects the moving blades 22 to each other. Link. More specifically, the connecting member 23 has a substantially cylindrical shape extending along the central axis 17, and the radial direction between the radially inner end and the radially outer end of each rotor blade 22. It is combined with the outer side part.

また、インペラ1は、射出成形によって連続した樹脂部材として一体に成形されている。インペラ1の射出成形には、図7(a)ないし図7(c)に示すように、中心軸17方向に離型する一組の金型31,32が用いられる。金型31,32のいずれか一方が所定の設置位置に固定された固定側金型となっており、他方がその固定側金型に対して中心軸17方向に近接、離反する可動側金型となっている。なお、金型31,32は、ベースとなる金型に複数の金型要素(入れ子)を組み込んで構成される場合が多い。   The impeller 1 is integrally formed as a continuous resin member by injection molding. For injection molding of the impeller 1, as shown in FIGS. 7A to 7C, a pair of molds 31 and 32 that are released in the direction of the central axis 17 are used. One of the molds 31 and 32 is a fixed mold that is fixed at a predetermined installation position, and the other is a movable mold that approaches and separates from the fixed mold in the direction of the central axis 17. It has become. The molds 31 and 32 are often configured by incorporating a plurality of mold elements (nesting) into a base mold.

また、金型31,32の少なくともいずれか一方には、金型31,32内面から中心軸17方向に進退可能に設けられ、射出成形後にインペラ1を金型31,32から押し出す可動部(イジェクターピンと呼ばれる場合がある)33が設けられている。この可動部33は、金型31,32のうちの可動側金型の中心軸17方向の動きと連動して駆動される。図7(a)ないし図7(c)の図示例では、可動部33が金型32に設けられている。以下では、この図示例に基づいて説明を行う。   Further, at least one of the molds 31 and 32 is provided so as to be able to advance and retreat in the direction of the central axis 17 from the inner surfaces of the molds 31 and 32, and a movable part (ejector) that pushes the impeller 1 from the molds 31 and 32 after injection molding. 33 (sometimes called pins). The movable portion 33 is driven in conjunction with the movement of the movable mold of the molds 31 and 32 in the direction of the central axis 17. In the illustrated example of FIGS. 7A to 7C, the movable portion 33 is provided in the mold 32. Below, it demonstrates based on this example of illustration.

図7(a)に示すように、金型31,32が互いに当接され、樹脂材料が射出される閉空間34が金型31,32によって形成されているときには、可動部33は、その先端面33aが閉空間34を形成する金型32の内面と整合する位置にセットされている。そして、その状態で、図7(b)に示すように、閉空間34内に樹脂材料が射出され、これによってインペラ1が成形される。続いて、図7(c)に示すように、金型31,32のうちの可動側金型が固定側金型から離反する方向に移動されるのに連動して、可動部33が金型32の内面から突出する方向に変位される。その結果、インペラ1が可動部33によって金型32から離反する方向に押し出され、インペラ1と金型32とが離型される。   As shown in FIG. 7A, when the molds 31 and 32 are brought into contact with each other and the closed space 34 into which the resin material is injected is formed by the molds 31 and 32, the movable portion 33 has the tip thereof. The surface 33 a is set at a position where it is aligned with the inner surface of the mold 32 that forms the closed space 34. In this state, as shown in FIG. 7B, the resin material is injected into the closed space 34, and the impeller 1 is thereby molded. Subsequently, as shown in FIG. 7C, the movable portion 33 is moved to the mold in conjunction with the movement of the movable mold of the molds 31 and 32 in the direction away from the fixed mold. It is displaced in a direction protruding from the inner surface of 32. As a result, the impeller 1 is pushed away from the mold 32 by the movable portion 33, and the impeller 1 and the mold 32 are released.

上述の如く、可動部33による金型32からのインペラ1の押し出しは、射出成形された樹脂材料が完全に硬化する前の状態で行われるため、可動部33により押圧されたインペラの部分に変形が生じる場合がある。このため、可動部33の受けとなるインペラ1の部分としては、可動部33の押圧により変形が生じやすく、また変形による流体特性の悪化が問題となり易い動翼22の部分を避ける必要がある。   As described above, the impeller 1 is pushed out from the mold 32 by the movable portion 33 before the injection-molded resin material is completely cured, so that it is deformed into the portion of the impeller pressed by the movable portion 33. May occur. For this reason, it is necessary to avoid the portion of the impeller 1 that receives the movable portion 33, and the portion of the rotor blade 22 that is likely to be deformed by the pressing of the movable portion 33 and that is liable to deteriorate the fluid characteristics due to the deformation.

また、本実施形態に係るインペラ1においても、連結部材23が設けられているため、インペラ1の径方向外方におけるインペラ1と金型31,32との密着部分が増大している。このため、射出成形後の離型を容易にするためには、金型32の可動部33の受けを連結部材23の部分に設けるか、あるいは支持部21の部分と連結部材23の部分の両方に設ける必要がある。   Moreover, also in the impeller 1 according to the present embodiment, since the connecting member 23 is provided, the contact portion between the impeller 1 and the dies 31 and 32 on the radially outer side of the impeller 1 is increased. For this reason, in order to facilitate mold release after injection molding, the receiving of the movable part 33 of the mold 32 is provided in the connecting member 23 part, or both the support part 21 part and the connecting member 23 part are provided. It is necessary to provide in.

そこで、本実施形態では、図3ないし図4に示すように、連結部材23の中心軸23方向の両側を向いた2つの面26,27のうちの少なくともいずれか一方に、少なくとも1つの拡幅部28を設け、この拡幅部28によって可動部33の受けを形成している。拡幅部28は、面26,27の径方向の幅を部分的に拡大することによって形成されている。本実施形態では、拡幅部28は連結部材23の2つの面26,27のうち、支持部21が開口する側を向く面27に設けられている。なお、変形例として、拡幅部28を面27に設ける代わりに面26に設けてもよいし、面26,27の両方に設けてもよい。   Therefore, in the present embodiment, as shown in FIGS. 3 to 4, at least one widened portion is provided on at least one of the two surfaces 26 and 27 facing both sides of the connecting member 23 in the direction of the central axis 23. 28 is provided, and the receiving portion of the movable portion 33 is formed by the widened portion 28. The widened portion 28 is formed by partially enlarging the radial width of the surfaces 26 and 27. In the present embodiment, the widened portion 28 is provided on the surface 27 of the two surfaces 26 and 27 of the connecting member 23 that faces the side where the support portion 21 opens. As a modification, the widened portion 28 may be provided on the surface 26 instead of being provided on the surface 27, or may be provided on both the surfaces 26 and 27.

連結部材23の面27における拡幅部28では、径方向の幅が部分的に拡大され、強度が向上されているため、可動部33による離型時の押圧によって連結部材23の変形が生じるのを回避できる。しかも、連結部材23の面27において、該面27の径方向の幅を部分的に拡大して拡幅部28を形成しているため、径方向の厚み増大による連結部材23の流体特性の悪化及び質量の増大も抑制できる。   In the widened portion 28 on the surface 27 of the connecting member 23, the radial width is partially enlarged and the strength is improved. Therefore, the connecting member 23 is deformed by the pressing at the time of releasing by the movable portion 33. Can be avoided. In addition, since the widened portion 28 is formed by partially expanding the radial width of the surface 27 on the surface 27 of the connecting member 23, the fluid characteristics of the connecting member 23 are deteriorated due to an increase in the radial thickness. An increase in mass can also be suppressed.

また、本実施形態では、面27における拡幅部28では、面27の径方向内方の辺の一部が径方向内方に略半円形に膨出されることにより、面27の径方向の幅が部分的に拡大されている。面27における拡幅部28以外の部分では径方向の幅は略一定に保たれている。なお、変形例として、面27の径方向内方の辺の代わりに径方向外方の辺の一部を径方向外方に膨出させて拡幅部28を形成してもよく、あるいは、面27の径方向の両側の辺の一部を互いに離反するように径方向の両側にそれぞれ膨出させて拡幅部28を形成してもよい。また、拡幅部28を形成するための面27の径方向の内外の辺の膨出形状についても、略半円形に限定するものではなく、略矩形状又は略三角形状等、種々の膨出形状を採用できる。   In the present embodiment, in the widened portion 28 of the surface 27, a part of the radially inner side of the surface 27 bulges in a substantially semi-circular shape radially inward, so that the radial width of the surface 27 is increased. Has been partially enlarged. In the portion other than the widened portion 28 on the surface 27, the width in the radial direction is kept substantially constant. As a modification, instead of the radially inner side of the surface 27, a part of the radially outer side may bulge radially outward to form the widened portion 28, or the surface The widened portion 28 may be formed by bulging a part of both sides in the radial direction of the 27 in the radial direction so as to be separated from each other. Further, the bulging shape of the inner and outer sides in the radial direction of the surface 27 for forming the widened portion 28 is not limited to a substantially semicircular shape, and various bulging shapes such as a substantially rectangular shape or a substantially triangular shape. Can be adopted.

また、動翼22の部分は金型31,32との密着面積が大きいため、連結部材23を金型32の可動部33によって押圧してインペラ1を金型32から離反させるときに、連結部材23と動翼22の結合部分に負荷がかかり易くなっている。   Further, since the portion of the moving blade 22 has a large contact area with the molds 31, 32, the connecting member 23 is pressed when the impeller 1 is separated from the mold 32 by pressing the connecting member 23 with the movable portion 33 of the mold 32. A load is easily applied to the connecting portion between the rotor 23 and the rotor blade 22.

そこで、本実施形態では、拡幅部28は、動翼22と同数設けられ、中心軸17方向から見て、拡幅部28が設けられる連結部材23の面27における各動翼22と重なる重複区間S内のいずれかの位置にそれぞれ配置されている。なお、変形例として、拡幅部28の数は動翼22の数よりも多くても、少なくてもよく、例えば1つでもよい。また、拡幅部28を面27における重複区間S以外の位置に配置してもよい。   Therefore, in the present embodiment, the same number of widened portions 28 as the moving blades 22 are provided, and when viewed from the direction of the central axis 17, the overlapping sections S overlap the moving blades 22 on the surface 27 of the connecting member 23 where the widened portions 28 are provided. Are arranged at any of the positions. As a modification, the number of widened portions 28 may be larger or smaller than the number of moving blades 22, for example, one. Further, the widened portion 28 may be disposed at a position other than the overlapping section S on the surface 27.

このように、拡幅部28を連結部材23の面27における重複区間S内のいずれかの位置に配置したため、金型32の可動部33によって連結部材23における動翼22と結合されている部分を押圧してインペラ1を金型から離反させることができる。その結果、インペラ1を可動部33によって金型32から押し出して離反させるときに、動翼22及び連結部材23の変形を生じることなく、インペラ1を容易に離反させることができる。   As described above, since the widened portion 28 is disposed at any position in the overlapping section S on the surface 27 of the connecting member 23, a portion of the connecting member 23 coupled to the moving blade 22 by the movable portion 33 of the mold 32 is used. The impeller 1 can be separated from the mold by pressing. As a result, when the impeller 1 is pushed away from the mold 32 by the movable portion 33 and separated, the impeller 1 can be easily separated without causing deformation of the moving blade 22 and the connecting member 23.

また、拡幅部28が、すべての動翼22にそれぞれ対応して得られる複数の重複区間S内にそれぞれ配置されているため、インペラ1を可動部33によって金型32から押し出して離反させるときに、すべての動翼22について、動翼22及び動翼22と連結部材23の結合部分における変形をより確実に防止しながら、インペラ1を容易に離反させることができる。   In addition, since the widened portion 28 is disposed in each of a plurality of overlapping sections S obtained corresponding to all the rotor blades 22, when the impeller 1 is pushed away from the mold 32 by the movable portion 33 and separated. The impeller 1 can be easily separated while more reliably preventing the deformation of the moving blades 22 and the connecting portions of the moving blades 22 and the connecting members 23 for all of the moving blades 22.

次に、拡幅部28の重複区間S内における配置位置について説明する。インペラ1の動翼22は、上述の如く、動翼22の延伸方向と垂直な面で動翼22を切断したときの断面形状が中心軸17方向と垂直な面に対して傾斜している。このため、連結部材23の拡幅部28が設けられる面27の重複区間S内における周方向の位置によって、面27から動翼22までの中心軸17方向に沿った距離L(図5参照)が変化する。これに伴い、重複区間Sに対応する連結部材23の径方向内側面29又は外側面30の部分と、可動部33が設けられる金型32との密着の度合いも、重複区間S内における周方向の位置によって変化し、面27から動翼までの距離Lが大きい程、密着の度合いが大きくなる。   Next, the arrangement position of the widened portion 28 in the overlapping section S will be described. As described above, the rotor blade 22 of the impeller 1 is inclined with respect to a plane perpendicular to the direction of the central axis 17 when the rotor blade 22 is cut along a plane perpendicular to the extending direction of the rotor blade 22. For this reason, the distance L (refer FIG. 5) along the center axis | shaft 17 direction from the surface 27 to the moving blade 22 with the circumferential position in the overlap area S of the surface 27 in which the wide part 28 of the connection member 23 is provided. Change. Accordingly, the degree of close contact between the radial inner side surface 29 or the outer side surface 30 of the connecting member 23 corresponding to the overlapping section S and the mold 32 provided with the movable portion 33 is also determined in the circumferential direction within the overlapping section S. The degree of adhesion increases as the distance L from the surface 27 to the moving blade increases.

そこで、本実施形態では、拡幅部28が、重複区間Sの周方向の両側の第1及び第2の端E1,E2のうち、該端E1,E2と動翼22との中心軸17方向に沿った距離Lが大きい方の第1の端E1と、重複区間Sの周方向に対する中間位置Mとの間(部分区間Sa内)におけるいずれかの位置Pに配置されている。なお、本実施形態では、重複区間S内において、第1の端E1は回転方向20前方側の端になっており、第2の端E2は回転方向20後方側の端になっている。それ故、連結部材23の重複区間S内において、重複区間Sに対応する連結部材23の径方向内側面29又は外側面30の部分と、可動部33が設けられる金型32との密着の度合いが大きい部分に可動部33の受けを設けることができる。その結果、インペラ1を可動部33によって金型32から押し出して離反させるときに、動翼22及び連結部材23の変形をより確実に防止しながら、インペラ1を容易に離反させることができる。   Therefore, in the present embodiment, the widened portion 28 is located in the direction of the central axis 17 between the ends E1 and E2 and the rotor blade 22 among the first and second ends E1 and E2 on both sides of the overlapping section S in the circumferential direction. It is arranged at any position P between the first end E1 having the longer distance L along the intermediate position M in the circumferential direction of the overlapping section S (within the partial section Sa). In the present embodiment, in the overlapping section S, the first end E1 is an end on the front side in the rotational direction 20, and the second end E2 is an end on the rear side in the rotational direction 20. Therefore, in the overlapping section S of the connecting member 23, the degree of close contact between the portion of the radially inner side surface 29 or the outer side surface 30 of the connecting member 23 corresponding to the overlapping section S and the mold 32 provided with the movable portion 33. The receiving part of the movable part 33 can be provided in a large part. As a result, when the impeller 1 is pushed away from the mold 32 by the movable portion 33 and separated, the impeller 1 can be easily separated while preventing the moving blade 22 and the connecting member 23 from being deformed more reliably.

より好ましくは、本実施形態では、拡幅部28が、重複区間Sの第1の端E1と中間位置Mとの間(部分区間Sa内)において、周方向に対して中間位置Mよりも第1の端E1に近い位置Pに配置されている。それ故、連結部材23の重複区間S内において、重複区間Sに対応する連結部材23の径方向内側面29又は外側面30の部分と、可動部33が設けられる金型32との密着の度合いがより大きい部分に可動部33の受けを設けることができる。その結果、インペラ1を可動部33によって金型32から押し出して離反させるときに、動翼22及び連結部材23の変形をさらに確実に防止しながら、インペラ1を容易に離反させることができる。   More preferably, in the present embodiment, the widened portion 28 is first than the intermediate position M in the circumferential direction between the first end E1 of the overlapping section S and the intermediate position M (in the partial section Sa). It is arrange | positioned in the position P close | similar to the edge E1. Therefore, in the overlapping section S of the connecting member 23, the degree of close contact between the portion of the radially inner side surface 29 or the outer side surface 30 of the connecting member 23 corresponding to the overlapping section S and the mold 32 provided with the movable portion 33. The receiving part of the movable part 33 can be provided in a larger part. As a result, when the impeller 1 is pushed away from the mold 32 by the movable portion 33 and separated, the impeller 1 can be easily separated while further reliably preventing the deformation of the rotor blade 22 and the connecting member 23.

さらに好ましくは、本実施形態では、拡幅部28が、重複区間Sの第1及び第2の端E1,E2のうち、該端E1,E2と動翼22との距離Lが大きい方である第1の端E1の近傍に配置されている。すなわち、本実施形態では、中心軸17方向から見て、重複区間S内における動翼22の回転方向20前方側縁部22aが連結部材23に結合される部分の近傍に、拡幅部28が配置されている。それ故、連結部材23の重複区間S内において、重複区間Sに対応する連結部材23の径方向内側面29又は外側面30の部分と、可動部33が設けられる金型32との密着の度合いが最も大きい部分の近傍に可動部33の受けを設けることができる。その結果、インペラ1を可動部33によって金型32から押し出して離反させるときに、動翼22及び連結部材23の変形をさらに確実に防止しながら、インペラ1を容易に離反させることができる。   More preferably, in the present embodiment, the widened portion 28 is the first of the first and second ends E1, E2 of the overlapping section S that has the larger distance L between the ends E1, E2 and the rotor blade 22. 1 near the end E1. That is, in the present embodiment, the widened portion 28 is disposed in the vicinity of the portion where the front edge 22a in the rotational direction 20 of the moving blade 22 is coupled to the connecting member 23 in the overlapping section S when viewed from the direction of the central axis 17. Has been. Therefore, in the overlapping section S of the connecting member 23, the degree of close contact between the portion of the radially inner side surface 29 or the outer side surface 30 of the connecting member 23 corresponding to the overlapping section S and the mold 32 provided with the movable portion 33. The receiving part of the movable part 33 can be provided in the vicinity of the largest part. As a result, when the impeller 1 is pushed away from the mold 32 by the movable portion 33 and separated, the impeller 1 can be easily separated while further reliably preventing the deformation of the rotor blade 22 and the connecting member 23.

また、本実施形態では、連結部材23の拡幅部28が設けられる部分の金型31,32(本実施形態の場合は金型32)による成形を容易にするため、拡幅部28の径方向内方側への張り出し形状が、面27から動翼22の表面まで中心軸17方向に沿って一定の形状で連続的に連なっている。すなわち、本実施形態では、連結部材23の内側面29には、拡幅部28に対応する位置に面17から動翼27の表面まで中心軸17方向に連続的に筋状に延びる突状部35が設けられている。   Further, in the present embodiment, in order to facilitate the molding by the molds 31 and 32 (the mold 32 in this embodiment) where the widened portion 28 of the connecting member 23 is provided, The projecting shape toward the side is continuously connected in a constant shape from the surface 27 to the surface of the rotor blade 22 along the direction of the central axis 17. In other words, in the present embodiment, on the inner side surface 29 of the connecting member 23, the protruding portion 35 that continuously extends in the direction of the central axis 17 from the surface 17 to the surface of the rotor blade 27 at a position corresponding to the widened portion 28. Is provided.

また、インペラ1の動翼22は、上述の如く、その回転方向20前方側縁部22aが回転方向20後方側縁部22bよりも中心軸17方向吸気側に位置するように、その断面形状が中心軸17と垂直な面に対して傾斜している。このため、インペラ1の連結部材23における動翼22の間に位置する内側面29及び外側面30の部分に形成されるパーティングライン36,37には、略中心軸17方向又は中心軸17方向に対して傾斜した方向に沿って延びる部分36a,37aが含まれることになる。本実施形態では、この部分36a,37aは、略中心軸17方向に沿って延びている。なお、パーティングラインとは、樹脂成型品の表面に金型同士の接合部に沿って形成される形状変化部のことをいう。   Further, as described above, the rotor blade 22 of the impeller 1 has a cross-sectional shape such that the front side edge portion 22a in the rotational direction 20 is located closer to the intake side in the central axis 17 direction than the rear side edge portion 22b in the rotational direction 20. It is inclined with respect to a plane perpendicular to the central axis 17. For this reason, the parting lines 36 and 37 formed on the inner side surface 29 and the outer side surface 30 located between the rotor blades 22 in the connecting member 23 of the impeller 1 have substantially the central axis 17 direction or the central axis 17 direction. In other words, portions 36a and 37a extending along the direction inclined with respect to the angle are included. In the present embodiment, the portions 36a and 37a extend substantially along the direction of the central axis 17. In addition, a parting line means the shape change part formed along the junction part of metal mold | dies on the surface of a resin molded product.

本実施形態に係る構成の特徴として、連結部材23の内側面29に形成されるパーティングライン36の部分36aと、外側面30に形成されるパーティングライン37の部分37aとが、周方向に対して互いにずれた位置に配置されている。   As a feature of the configuration according to the present embodiment, a part 36a of the parting line 36 formed on the inner side surface 29 of the connecting member 23 and a part 37a of the parting line 37 formed on the outer side surface 30 are arranged in the circumferential direction. In contrast, they are arranged at positions shifted from each other.

以上のように、本実施形態に係るインペラ1は、射出成形後の金型31,32の可動部33による押し出しによってインペラ1の連結部材23に変形が生じるのが回避されているとともに、径方向の厚み増大による連結部材23の流体特性の悪化及び質量の増大も抑制されている。それ故、安定して効率よく空気流を発生させることができるファン装置11を提供できる。   As described above, in the impeller 1 according to the present embodiment, deformation of the connecting member 23 of the impeller 1 due to extrusion by the movable portion 33 of the molds 31 and 32 after injection molding is avoided, and the radial direction The deterioration of the fluid characteristics and the increase in mass of the connecting member 23 due to the increase in the thickness of the connecting member 23 are also suppressed. Therefore, it is possible to provide the fan device 11 that can generate an air flow stably and efficiently.

また、本実施形態に係るインペラ1では、図1に示すように、射出成形時のゲートのゲート跡210が支持部21の中心軸17方向吸気側面上における各動翼22の付け根近傍に配置されている。それ故、射出成形の際に連結部材23には動翼22を介して樹脂材料が充填されるため、連結部材23における各動翼22間の略中央部付近が樹脂材料の最終充填位置となり、その付近でガス焼けが発生するおそれがある。ガス焼けは、成形品の外観悪化(例えば、ショートモールド又は焼けによる変色等)及び強度低下(例えば、樹脂充填密度の低下、ウェルドライン等)を招くため、対策が必要である。   Further, in the impeller 1 according to the present embodiment, as illustrated in FIG. 1, the gate trace 210 of the gate at the time of injection molding is disposed near the root of each rotor blade 22 on the intake side surface in the direction of the central axis 17 of the support portion 21. ing. Therefore, since the connecting member 23 is filled with the resin material via the moving blades 22 at the time of injection molding, the vicinity of the substantially central portion between the moving blades 22 in the connecting member 23 is the final filling position of the resin material. There is a risk of gas burning in the vicinity. Since gas burning causes deterioration of the appearance of the molded product (for example, discoloration due to short molding or burning) and strength reduction (for example, decrease in resin filling density, weld line, etc.), countermeasures are necessary.

そこで、その対策として、インペラ1の連結部材23の面26又は27(本実施形態では27)上の複数箇所にガス抜きピンを配置し、成形時に発生するガスをガス抜きピンを利用して金型外に排出するようにしてもよい。例えば、図4に示す例では、連結部材23の面27における各動翼22と重複する各重複区間Sについて、その重複区間Sの周方向の中央位置Mの周方向の両側(例えば、重複区間Sの略両端E1,E2)にガス抜きピンがそれぞれ設けられている。図4では、そのガス抜きピンのピン跡230a,230bが示されている。これに対応して、金型31,32におけるガス抜きピンの配置位置に対応する部分には、ガス抜きピンの設置スペースが確保されている。   Therefore, as a countermeasure, degassing pins are arranged at a plurality of locations on the surface 26 or 27 (27 in the present embodiment) of the connecting member 23 of the impeller 1, and the gas generated during molding is made gold using the degassing pins. You may make it discharge | emit out of a type | mold. For example, in the example shown in FIG. 4, with respect to each overlapping section S overlapping with each rotor blade 22 on the surface 27 of the connecting member 23, both sides in the circumferential direction of the central position M in the circumferential direction of the overlapping section S (for example, overlapping sections) Gas venting pins are provided at substantially both ends E1, E2) of S, respectively. In FIG. 4, pin marks 230a and 230b of the degassing pins are shown. Correspondingly, an installation space for the gas vent pin is secured in a portion corresponding to the position of the gas vent pin in the molds 31 and 32.

本発明の一実施形態に係るインペラの中心軸方向吸気側から見た斜視図である。It is the perspective view seen from the central-axis direction intake side of the impeller which concerns on one Embodiment of this invention. 図1のインペラの側面図である。It is a side view of the impeller of FIG. 図1のインペラの中心軸方向排気側から見た底面図である。It is the bottom view seen from the central axial direction exhaust side of the impeller of FIG. 図3の一部を拡大して示す図である。It is a figure which expands and shows a part of FIG. 図1のインペラにおける動翼と連結部材との結合部分を径方向内側から見た図である。It is the figure which looked at the coupling | bond part of the moving blade and connecting member in the impeller of FIG. 1 from the radial inside. 図1のインペラが用いられたファン装置の断面図である。It is sectional drawing of the fan apparatus with which the impeller of FIG. 1 was used. 図7(a)ないし図7(c)は、図1のインペラの製造工程を示す図である。FIG. 7A to FIG. 7C are diagrams showing manufacturing steps of the impeller of FIG.

符号の説明Explanation of symbols

1 インペラ、11 ファン装置、12 静翼、13 モータ、14 外枠体、15 支持体、16 ハウジング、17 中心軸、18 ロータマグネット、19 電機子、20 回転方向、21 支持部、21a 円筒状外側面、22 動翼、23 連結部材、26,27 面、28 拡幅部、31,32 金型、33 可動部、34 閉空間、36,37 パーティングライン、E1,E2 端、L 距離、M 中央位置、S 重複区間。   DESCRIPTION OF SYMBOLS 1 Impeller, 11 Fan apparatus, 12 Stator blade, 13 Motor, 14 Outer frame body, 15 Support body, 16 Housing, 17 Center axis, 18 Rotor magnet, 19 Armature, 20 Rotating direction, 21 Support part, 21a Cylindrical outside Side, 22 blades, 23 connecting members, 26, 27 faces, 28 widened part, 31, 32 mold, 33 movable part, 34 closed space, 36, 37 parting line, E1, E2 end, L distance, M center Position, S Overlapping section.

Claims (5)

インペラであって、
中心軸を中心とした円筒状外側面を有する支持部と、
前記支持部の前記円筒状外側面から径方向外方に向けて延伸して形成され、前記支持部と共に前記中心軸を中心に回転することで前記中心軸方向の空気流を発生する複数の翼と、
前記中心軸を中心とした周方向に沿って形成され、前記中心軸方向の両側をそれぞれ向いた2つの面を有し、前記複数の翼同士を連結する略環状の連結部材と、
を備え、
前記支持部、前記複数の翼及び前記連結部材は、連続した樹脂部材により一体に成形されており、
前記連結部材の前記2つの面の少なくともいずれか一方に、該面の径方向の幅が部分的に拡大されてなる少なくとも1つの拡幅部が設けられ
前記拡幅部は、前記中心軸方向から見て、該拡幅部が設けられる前記連結部材の前記面における前記翼と重なる重複区間内であって、前記重複区間の前記周方向の両側の第1及び第2の端のうち、該端と前記翼との前記中心軸方向に沿った距離が大きい方の第1の端と、前記重複区間の前記周方向に対する中間位置との間におけるいずれかの位置に配置されていることを特徴とするインペラ。
An impeller,
A support portion having a cylindrical outer surface around the central axis;
A plurality of blades that are formed to extend radially outward from the cylindrical outer surface of the support portion and generate an air flow in the central axis direction by rotating around the central axis together with the support portion. When,
A substantially annular connecting member that is formed along a circumferential direction about the central axis and has two surfaces facing both sides of the central axis direction, and that connects the plurality of blades;
With
The support portion, the plurality of wings, and the connecting member are integrally formed of a continuous resin member,
At least one of the two surfaces of the connecting member is provided with at least one widened portion obtained by partially expanding the radial width of the surface ,
The widened portion is in an overlapping section overlapping the wings on the surface of the connecting member provided with the widened portion when viewed from the central axis direction, and the first and the first on both sides in the circumferential direction of the overlapping section Among the second ends, any position between the first end having a larger distance along the central axis direction between the end and the wing and the intermediate position of the overlapping section with respect to the circumferential direction Impeller characterized by being arranged in .
請求項1に記載のインペラにおいて、
前記拡幅部は、前記重複区間の前記第1の端と前記中間位置との間において、前記周方向に対して前記中間位置よりも前記第1の端に近い位置に配置されていることを特徴とするインペラ。
The impeller according to claim 1,
The widened portion is disposed between the first end of the overlapping section and the intermediate position at a position closer to the first end than the intermediate position with respect to the circumferential direction. Impeller.
請求項1又は請求項2に記載のインペラにおいて、
前記拡幅部は、前記複数の翼にそれぞれ対応して得られる複数の前記重複区間内にそれぞれ配置されることを特徴とするインペラ。
The impeller according to claim 1 or 2 ,
The widened portion is disposed in each of the plurality of overlapping sections obtained corresponding to each of the plurality of blades.
請求項1ないし請求項3のいずれかに記載のインペラにおいて、
前記拡幅部は、
前記樹脂部材を成形する金型に進退可能に設けられ、前記樹脂部材を前記金型から押し出す可動部の受けを形成することを特徴とするインペラ。
The impeller according to any one of claims 1 to 3 ,
The widened portion is
An impeller provided to a mold for molding the resin member so as to be capable of moving forward and backward, and forming a receiving part of a movable part that pushes the resin member out of the mold .
ファン装置であって、A fan device,
請求項1ないし請求項4のいずれかに記載の前記インペラと、  The impeller according to any one of claims 1 to 4,
前記インペラを駆動するモータと、  A motor for driving the impeller;
前記インペラを外囲する外枠体と、  An outer frame surrounding the impeller;
前記外枠体の径方向内方に設けられ、前記モータを支持する支持体と、  A support that is provided radially inward of the outer frame and supports the motor;
を備えることを特徴とするファン装置。A fan device comprising:
JP2008329214A 2008-10-08 2008-12-25 Impeller, fan device, and impeller manufacturing method Active JP4695687B2 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
JP2008329214A JP4695687B2 (en) 2008-12-25 2008-12-25 Impeller, fan device, and impeller manufacturing method
CN2009101757287A CN101713417B (en) 2008-10-08 2009-09-29 Impeller, fan apparatus using the same, and method of manufacturing impeller
US12/570,330 US8317478B2 (en) 2008-10-08 2009-09-30 Impeller, fan apparatus using the same, and method of manufacturing impeller
DE102009048382A DE102009048382A1 (en) 2008-10-08 2009-10-06 Impeller, fan device using the same, and method of manufacturing the impeller

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2008329214A JP4695687B2 (en) 2008-12-25 2008-12-25 Impeller, fan device, and impeller manufacturing method

Publications (2)

Publication Number Publication Date
JP2010151009A JP2010151009A (en) 2010-07-08
JP4695687B2 true JP4695687B2 (en) 2011-06-08

Family

ID=42570371

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008329214A Active JP4695687B2 (en) 2008-10-08 2008-12-25 Impeller, fan device, and impeller manufacturing method

Country Status (1)

Country Link
JP (1) JP4695687B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5993602B2 (en) * 2012-04-23 2016-09-14 ミネベア株式会社 Blower

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0361195U (en) * 1989-10-17 1991-06-14
JP2003035296A (en) * 2001-07-24 2003-02-07 Daikin Ind Ltd Manufacturing method of propeller fan
JP2003094494A (en) * 2001-09-25 2003-04-03 Denso Corp Fan and its molding method

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0361195U (en) * 1989-10-17 1991-06-14
JP2003035296A (en) * 2001-07-24 2003-02-07 Daikin Ind Ltd Manufacturing method of propeller fan
JP2003094494A (en) * 2001-09-25 2003-04-03 Denso Corp Fan and its molding method

Also Published As

Publication number Publication date
JP2010151009A (en) 2010-07-08

Similar Documents

Publication Publication Date Title
CN103890408B (en) The manufacture method of impeller
JP6081142B2 (en) Centrifugal fan impeller and centrifugal fan
US8317478B2 (en) Impeller, fan apparatus using the same, and method of manufacturing impeller
KR100929984B1 (en) Wing tea of multi-blown blower and manufacturing method thereof
US20130071247A1 (en) Impeller and method for producing same
EP3034884B1 (en) Centrifugal fan assembly
JP2003065291A (en) Turbo fan and its die for manufacture
KR20170091953A (en) Fluid machine
JP2008128232A (en) Turbofan and method of manufacturing the same
JP2013032711A (en) Electric blower, and vacuum cleaner using the same
JP4762775B2 (en) Ring fan and manufacturing method thereof
JP6363789B2 (en) Impeller manufacturing method
CN103659163B (en) Method for manufacturing fan wheel
JP4695687B2 (en) Impeller, fan device, and impeller manufacturing method
JP4821084B2 (en) Turbofan and turbofan manufacturing method
JP2012154339A (en) Method of manufacturing impeller
JP5303120B2 (en) Impeller
CN102162466A (en) Centrifugal fan impeller and moulding method thereof
CN111183293B (en) Housing made of a working program
JP5833797B1 (en) Negative pressure pump and manufacturing method thereof
KR20190009574A (en) Fan and mold for injection molding the same
JP2013060874A (en) Electric air blower and electric vacuum cleaner using the same
JP2011074763A (en) Impeller and blower having the same
US20060222498A1 (en) Impeller for centrifugal blower
JP2012087713A (en) Blower impeller and blower with the same

Legal Events

Date Code Title Description
A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20101008

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20101018

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20101201

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20110207

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20110225

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20140304

Year of fee payment: 3

R150 Certificate of patent or registration of utility model

Free format text: JAPANESE INTERMEDIATE CODE: R150

Ref document number: 4695687

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250