WO2006082877A1 - 軸流送風機 - Google Patents

軸流送風機 Download PDF

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Publication number
WO2006082877A1
WO2006082877A1 PCT/JP2006/301738 JP2006301738W WO2006082877A1 WO 2006082877 A1 WO2006082877 A1 WO 2006082877A1 JP 2006301738 W JP2006301738 W JP 2006301738W WO 2006082877 A1 WO2006082877 A1 WO 2006082877A1
Authority
WO
WIPO (PCT)
Prior art keywords
stationary blade
wind tunnel
axial
guide wall
blades
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.)
Ceased
Application number
PCT/JP2006/301738
Other languages
English (en)
French (fr)
Japanese (ja)
Inventor
Katsumichi Ishihara
Honami Oosawa
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.)
Sanyo Electric Co Ltd
Sanyo Denki Co Ltd
Original Assignee
Sanyo Electric Co Ltd
Sanyo Denki Co Ltd
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 Sanyo Electric Co Ltd, Sanyo Denki Co Ltd filed Critical Sanyo Electric Co Ltd
Priority to CN2006800042667A priority Critical patent/CN101115927B/zh
Priority to HK08106947.3A priority patent/HK1112043B/xx
Priority to US11/815,616 priority patent/US7828519B2/en
Priority to EP06712881.9A priority patent/EP1847718B8/en
Publication of WO2006082877A1 publication Critical patent/WO2006082877A1/ja
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/52Casings; Connections of working fluid for axial pumps
    • F04D29/54Fluid-guiding means, e.g. diffusers
    • F04D29/541Specially adapted for elastic fluid pumps
    • F04D29/542Bladed diffusers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00Axial-flow pumps
    • F04D19/002Axial flow fans
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00Pumping installations or systems
    • F04D25/02Units comprising pumps and their driving means
    • F04D25/06Units comprising pumps and their driving means the pump being electrically driven
    • F04D25/0693Details or arrangements of the wiring

Definitions

  • the present invention relates to an axial blower used for cooling the inside of an electric device or the like.
  • Patent Document 1 discloses an axial blower equipped with a stationary blade (static blade) in order to meet this requirement. Yes.
  • Patent Document 1 Japanese Patent Laid-Open No. 2000-257597 (FIGS. 1 and 4)
  • An object of the present invention is to provide an axial blower that includes a stationary blade, can improve static pressure and air volume characteristics, and can reduce noise.
  • An axial blower of the present invention includes a housing, an impeller, a motor that rotates the impeller, and a plurality of stationary blades.
  • the winging includes a wind tunnel having a suction opening on one side in the axial direction of the rotating shaft and a discharge opening on the other side in the axial direction.
  • the impeller includes a plurality of rotating blades that rotate in the wind tunnel. The plurality of rotating blades are arranged at equal intervals in the circumferential direction of the rotating shaft.
  • the motor then rotates the impeller in one direction of rotation about the rotation axis. Multiple
  • Multiple The stationary blade is disposed in the vicinity of the discharge opening in the wind tunnel.
  • the nosing and the winging are provided with lead wire locking portions for locking a plurality of lead wires.
  • the lead wire locking portion is provided on a wall portion surrounding the discharge opening of the housing and is configured to lock a plurality of lead wires connected to the motor.
  • the presence of multiple lead wires causes noise generation that not only affects airflow and static pressure. Therefore, in the present invention, a guide wall portion is formed which accommodates a plurality of lead wires between one stationary blade adjacent to the lead wire engaging portion and forms a guide groove for guiding the lead wire to the lead wire engaging portion.
  • the presence of the multiple lead wires reduces the air volume and static pressure, and reduces noise generation. it can.
  • Each of the plurality of stationary blades has an outer end fixed to the inner wall portion of the wind tunnel, and an inner end located on the opposite side of the rotation shaft in the radial direction.
  • a stationary blade fixing member having a peripheral wall portion to which the inner end portions of the plurality of stationary blades are fixed is disposed at the central portion of the wind tunnel near the discharge opening.
  • the guide wall includes a first end located on the discharge opening side, a second end located on the suction opening side, a third end located on the inner wall side of the wind tunnel, and stationary blade fixing And a fourth end located on the member side.
  • the first end portion of the guide wall portion is connected to the suction opening side end portion of one stationary blade located on the suction opening side, and the inner wall force of the wind tunnel extends toward the stationary blade fixing member. Then, a guide groove is formed between the guide wall portion and one stationary blade. By rubbing in this way, it is possible to suppress the presence of the guide wall itself from affecting the relationship of the static pressure to the air volume and being a noise generation source.
  • the third end of the guide wall is preferably fixed to the inner wall of the wind tunnel. With such a structure, the mechanical strength of the guide wall can be increased.
  • the shape of the connecting portion between the first end of the guide wall and the suction of one stationary blade and the end of the suction opening side is determined so that the thickness decreases toward the suction opening. Is preferred. In this way, it is possible to suppress a large resistance against the wind flow generated by the rotation of the connecting portion force impeller.
  • the second end of the guide wall is flush with the opening surface of the discharge opening. That's right.
  • the guide wall is positioned so as to be substantially orthogonal to the opening surface of the discharge opening.
  • the end force of 1 extends to the second end as well.
  • the lead wire locking portion is formed in the housing adjacent to the outer end of one stationary blade, and is formed in the housing and a through hole that communicates the inside of the wind tunnel and the outside of the housing. And a slit that communicates with the through-hole and opens to the other side in the axial direction.
  • the size of the slit is determined so that a plurality of lead wires that are accommodated in the guide groove and go out to the outside through the through hole cap do not easily come out of the slit. If the lead wire engaging portion is configured in this way, the lead wire can be easily inserted into the guide groove and pulled out of the housing.
  • the third end portion of the guide wall portion is fixed to the inner wall portion of the wind tunnel.
  • the length of the guide wall extending along the stationary blade should be set to a length that prevents a part of the air flow generated by the rotation of the impeller from actively flowing out of the housing through the through hole. preferable. In this way, the wind that flows through the through hole is substantially eliminated, and noise generation can be reduced.
  • FIG. 1A is a perspective view of an axial blower as an example of an embodiment of the present invention viewed from the front right side oblique upward force
  • FIG. (C) is a perspective view of the axial blower of the embodiment excluding three lead wires as viewed from the diagonally upper front right side.
  • FIG. 2 (A) and (B) are a front view and a rear view of the embodiment shown in FIG. 1 with the motor-side seal removed.
  • FIG. 3 is a plan view of an axial blower with three lead wires and a seal removed.
  • FIG. 4 is a right side view of the axial blower shown in FIG. 2 (A).
  • FIG. 5 is a diagram used for explaining the relationship between a rotating blade and a stationary blade.
  • FIG. 6 is a diagram used for explaining the relationship between a rotating blade and a stationary blade.
  • FIG. 7 is a cross-sectional view taken along line AA, with the internal structure of the motor of FIG. 4 omitted.
  • FIG. 8 This is a cross-sectional view taken along line B-B in FIG.
  • FIG. 9 is a cross-sectional view taken along line CC with the internal structure of the motor of FIG. 4 omitted.
  • FIG. 10 is a cross-sectional view taken along the line D-D in FIG.
  • FIG. 11 is a cross-sectional view taken along line EE of FIG.
  • FIG. 12 is a cross-sectional view taken along line FF in FIG.
  • FIG. 13 is a cross-sectional view taken along line GG in FIG.
  • FIG. 14 is a diagram showing the results of measuring the static pressure-air volume characteristics with and without the guide wall.
  • FIG. 15 is a diagram showing the measurement results when the number of rotating blades (moving blades) is fixed to 7 and the number of stationary blades (stationary blades) is changed.
  • FIG. 16 is a diagram showing measurement results when the number of rotating blades (moving blades) is changed and the number of stationary blades (stationary blades) is fixed to eight.
  • FIG. 1 (A) is a perspective view of an axial blower 1 as an example of an embodiment of the present invention as seen from diagonally upward on the front right side
  • FIG. FIG. 1 (C) is a perspective view of the axial blower 1 of the embodiment excluding three lead wires 10 and also seeing the diagonally upward force on the front right side
  • FIGS. 2A and 2B are a front view and a rear view of the embodiment shown in FIG. 1 with the motor 2 side seal 2 removed.
  • FIG. 3 is a plan view of the axial blower 1 with the three lead wires 10 and the seal 2 removed.
  • FIG. 4 is a right side view of the axial blower 1 shown in FIG. 2 (A).
  • 5 and 6 are diagrams used to explain the relationship between the rotating blade 5 and the stationary blade 11 described later.
  • FIGS. 7, 8 and 9 are cross-sectional views taken along the lines AA, B-B and the internal structure of the motor, respectively, with the internal structure of the motor shown in FIG. 4 omitted. .
  • an axial blower 1 includes a housing 3, an impeller 7 including seven rotating blades 5 that are disposed in the housing 3 and rotate, and a rotating shaft 8 on which the impeller 7 is mounted. It has a motor 9 provided and eight stationary blades 11. As shown in FIGS. 1 and 2, the housing 3 has an annular suction on one side in the direction in which the axis of the rotary shaft 8 extends (axial direction)! , And an annular discharge-side flange 15 on the other side in the axial direction.
  • the housing 3 has a cylindrical portion 17 between both flanges 13 and 15. A wind tunnel 19 is formed by the internal spaces of the flange 13, the flange 15, and the cylindrical portion 17.
  • the suction side flange 13 has a substantially square outline shape, and has a substantially circular suction opening 14 inside. Further, the suction side flange 13 has flat surfaces 13a at four corners, and through holes 13b through which mounting screws pass are formed at the four corners, respectively.
  • the discharge-side flange 15 also has a substantially square outline shape, and has a substantially circular discharge opening 16 inside.
  • the discharge-side flange 15 has flat surfaces 15a at four corners, and through holes 15b through which mounting screws pass are formed at the four corners, respectively.
  • the impeller 7 includes a cup-shaped rotating blade fixing member 6 in which seven rotating blades 5 are fixed to a peripheral wall portion.
  • a plurality of permanent magnets constituting a part of the rotor of the motor 9 are fixed inside the peripheral wall portion of the rotary blade fixing member 6.
  • the eight stationary blades 11 include an outer end portion 11 A fixed to the inner wall portion of the wind tunnel 19 and the outer end portion 11 A. And an inner end portion 11B located on the opposite side of the rotary shaft 8 in the radial direction.
  • a cup-shaped stationary blade fixing member 21 having a peripheral wall portion having an outer diameter less than or equal to the outer diameter of the peripheral wall portion of the rotating blade fixing member 6 is disposed in the central portion of the wind tunnel 19 near the discharge opening 16.
  • the stationary blade fixing member 21 does not become a great resistance against the wind flow generated by the rotation of the impeller 7.
  • the inner end portions 11B of the eight stationary blades 11 are fixed to the peripheral wall portion of the stationary blade fixing member 21.
  • the stationary blade fixing member 21 is fixed to the housing 3 by the eight stationary blades 11.
  • the stationary blade fixing member 21 supports a stator 23 (not shown) of the motor 9 and a bearing 23 that rotatably supports the rotating shaft 8.
  • the seven rotary blades 5 have a cross-sectional shape when the rotary blade 5 is cut in a direction perpendicular to the axial direction of the rotary shaft 8. Clockwise direction as viewed in (A): counterclockwise direction as viewed in Fig. 2 (B)] It has a shape. Further, as shown in FIG. 6, the curved shape of the seven rotating blades 5 is a cross-sectional shape force when the rotating blade 5 is cut in the axial direction. The curved shape is convex in the direction opposite to the rotating direction of the impeller 7. It is. In addition, as shown in FIG.
  • the stationary blade 11 has a cross-sectional shape when the stationary blade 11 is cut in a direction orthogonal to the axial direction, and a curved shape in which a concave portion is opened by directing in a direction opposite to the rotation direction have.
  • the curved shape of the eight stationary blades 11 is a curved shape in which the cross-sectional shape when the stationary blade 11 is cut in the axial direction is convex in the rotational direction.
  • the length dimension L2 of the side of the outer end portion 11A of the stationary blade 11 extending along the inner wall portion of the wind tunnel 19 is along the peripheral wall portion of the stationary blade fixing member 21.
  • the shape of the eight stationary blades 11 is determined so as to be longer than the length dimension L1 of the side of the inner end portion 11B of the stationary blade 11 extending.
  • the length dimension L1 of the inner end 11B side of one stationary blade 11 adjacent to the lead wire locking portion 25 described later is the length dimension of the inner end 11B side of the other stationary blade 11. It is shorter than L1. This is to achieve the purpose of drawing the lead wire 10 from the motor 9 side.
  • a method for determining the shape of the stationary blade 11 will be described with reference to FIG.
  • a virtual plane PS 1 is assumed.
  • a second virtual plane PS2 extending in the radial direction through the end portion 12B closest to the discharge opening 16 on the side of the outer end 11A of the stationary blade 11 and the center line CL is assumed.
  • a third virtual plane PS3 extending in the radial direction through the end portion 12C and the center line CL closest to the suction opening 14 on the side of the outer end 11A of the stationary blade 11 is assumed.
  • the direction of the force force from the first virtual plane PS1 to the second virtual plane PS2 and the direction of the force direction from the second virtual plane PS2 to the third virtual plane PS3 are opposite to the rotation direction of the impeller 7, respectively.
  • the angle ⁇ 1 between the first virtual plane PS1 and the second virtual plane PS2 is set to the angle ⁇ 2 between the second virtual plane PS2 and the third virtual plane PS3. Is bigger than.
  • the angle ⁇ 1 is about 30 degrees.
  • the angle ⁇ 2 is 20 degrees.
  • a preferable range of the angle ⁇ 1 is 25 to 30 degrees, and a range of the angle ⁇ 2 is 15 to 20 degrees. With such dimensions, it becomes easy to design an axial fan with a large air volume and high static pressure.
  • the length dimension L2 of the outer edge 11 ⁇ side of the stationary blade is 40% to 50% of the length dimension L3 extending in the axial direction of the rotating blade 5. I prefer to do it. With such dimensions, it becomes easy to design an axial fan with a large air volume and high static pressure.
  • the nozzle 3 is provided with a lead wire locking portion 25 for locking the three lead wires 10.
  • the lead wire locking portion 25 is formed in the cylindrical portion 17 of the housing 3 adjacent to the outer end portion 11B of one adjacent stationary blade 11, and communicates the inside of the wind tunnel 19 with the outside of the housing 3.
  • the through-hole 27 and the slit 29 that is formed in the flange 15 of the housing 3 and communicates with the through-hole 27 and opens toward the other side in the axial direction are also configured. In this case, the width of the slit 29 is determined so that the three lead wires 10 that are accommodated in a guide groove 31 to be described later and go out through the through hole 27 do not easily come out of the slit 29.
  • the lead wire locking portion 25 When the lead wire locking portion 25 is configured in this manner, the lead wire 10 can be easily inserted into the guide groove 31 and the housing 3 can be pulled out to the outside.
  • the lead wire locking portion 26 for locking the lead wire 10 bent along the cylindrical portion 17 is also formed on the flange 13 of the housing 3.
  • FIG. 2 (A), FIG. 3, FIG. 11 and FIG. A guide wall portion 33 is provided between the stationary blade 11 and the guide wall portion 33 for accommodating the three lead wires 10 and forming a guide groove 31 for guiding the lead wire 10 to the lead wire engaging portion 25.
  • the guide wall 33 includes a first end 35 located on the suction opening 14 side, a second end 37 located on the discharge opening 16 side, and a wind tunnel. 19 includes a third end 39 located on the inner wall side and a fourth end 41 located on the stationary blade fixing member 21 side.
  • the first end 35 of the guide wall 33 extends from the inner wall of the wind tunnel 19 toward the stationary blade fixing member 21 and the suction blade side end 11C of the stationary blade 11 located on the suction opening 14 side. Are connected to form a connecting part. As a result, a guide groove 31 is formed between the guide wall 33 and the single stationary blade 11. Made.
  • the third end 39 of the guide wall 33 is fixed to the inner wall of the wind tunnel 19. Also, the shape of the connecting portion between the first end 35 of the guide wall 33 and the suction opening side end 11C of the single stationary blade 11 is directed to the suction opening 14 as shown in FIG.
  • the thickness is set to be thinner. As a result, it can be suppressed that this connecting portion becomes a large resistance to the wind flow generated by the rotation of the impeller 7.
  • the second end portion 37 of the guide wall portion 33 is flush with the opening surface of the discharge opening portion 16.
  • the guide wall portion 33 extends from the first end portion 35 to the second end portion 37 so as to be substantially orthogonal to the opening surface of the discharge opening portion 16, that is, to be parallel to the rotation axis 8. ing.
  • the length L4 (see FIGS. 8 and 12) extending along the stationary blade 11 of the guide wall 33 is the flow of air generated by the rotation of the impeller 7.
  • This length is set to a length that can prevent a part of the air from actively flowing out of the housing 3 through the through hole 27. As a result, the wind that flows through the through hole 27 is substantially eliminated, and the generation of noise is reduced.
  • Fig. 14 shows the measurement results of the static pressure-air volume characteristics. The measurement was performed with the motor rotating speed set at 13000 rpm. As shown in FIG. 14, when the guide wall 33 is provided and the lead wire is accommodated in the guide groove 31, the air volume can be increased and the static pressure can be increased. confirmed.
  • the sound pressure level when the sound pressure level when the lead wire is stored in the guide groove 31 is Lp [dB (A)], the sound pressure level when the guide wall 33 is removed is Lp + 3 [dB (A)] was confirmed to increase.
  • Figure 15 shows the measurement results when the number of rotating blades (represented as moving blades in the figure) is fixed to 7 and the number of stationary blades (represented as stationary blades in the figure) is changed.
  • shows the results of 7 and 8 rotating blades and stationary blades
  • shows the results of 7 and 7 rotating blades and 7 stationary blades.
  • the country shows the results of 7 and 6 rotating blades and stationary blades
  • X shows the results of 7 and 9 rotating blades and stationary blades.
  • FIGS. 15 and 16 show the measurement results when the number of rotating blades (represented as moving blades in the figure) was changed and the number of stationary blades (represented as stationary blades in the figure) was fixed to 8. .
  • shows the results for 7 and 8 rotating blades and stationary blades
  • shows the results for 8 and 8 rotating blades and stationary blades.
  • the country shows the results of 9 and 8 rotating blades and stationary blades
  • X shows the results of 6 and 8 rotating blades and stationary blades.
  • FIGS. 15 and 16 when the number of rotating blades 5 and stationary blades 11 is 7 and 8, both the air volume and static pressure increase.
  • Table 1 below shows that the number of rotating blades (moving blades) is fixed and the number of stationary blades (stationary blades) is changed. The result of measuring the sound pressure level when the number of (static blades) is fixed is shown.
  • the sound pressure level is the sound pressure level when the lead wire is stored in the guide groove 31.
  • Lp [dB (A)] the change in the sound pressure level when the guide wall 33 is removed is shown.
  • 1 ⁇ + 5 [(18 (eight)) has a sound pressure level of 5 [dB (A) when the sound pressure level when the lead wire is stored in the guide groove 31 is Lp [dB (A)].
  • the axial blower of the present invention by providing the guide wall portion and storing the plurality of lead wires in the guide groove, the presence of the plurality of lead wires has an adverse effect on the air volume and static pressure. Therefore, it is possible to increase the air volume of the blower, increase the static pressure, and reduce the generation of noise.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
PCT/JP2006/301738 2005-02-07 2006-02-02 軸流送風機 Ceased WO2006082877A1 (ja)

Priority Applications (4)

Application Number Priority Date Filing Date Title
CN2006800042667A CN101115927B (zh) 2005-02-07 2006-02-02 轴流式鼓风机
HK08106947.3A HK1112043B (en) 2005-02-07 2006-02-02 Axial flow blower
US11/815,616 US7828519B2 (en) 2005-02-07 2006-02-02 Axial flow fan
EP06712881.9A EP1847718B8 (en) 2005-02-07 2006-02-02 Axial flow fan

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
JP2005031098A JP4397832B2 (ja) 2005-02-07 2005-02-07 軸流送風機
JP2005-031098 2005-02-07

Publications (1)

Publication Number Publication Date
WO2006082877A1 true WO2006082877A1 (ja) 2006-08-10

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ID=36777260

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/JP2006/301738 Ceased WO2006082877A1 (ja) 2005-02-07 2006-02-02 軸流送風機

Country Status (6)

Country Link
US (1) US7828519B2 (https=)
EP (1) EP1847718B8 (https=)
JP (1) JP4397832B2 (https=)
CN (1) CN101115927B (https=)
TW (1) TW200636170A (https=)
WO (1) WO2006082877A1 (https=)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4033891B1 (ja) * 2007-04-18 2008-01-16 山洋電気株式会社 二重反転式軸流送風機
USD665894S1 (en) * 2010-04-20 2012-08-21 Sanyo Denki Co., Ltd. Housing for a fan motor
JP5718980B2 (ja) * 2013-06-04 2015-05-13 山洋電気株式会社 ファンモータ、直列型ファンモータおよびその組立方法
CN104235035A (zh) * 2013-06-18 2014-12-24 鸿富锦精密工业(深圳)有限公司 风扇模组
USD818103S1 (en) * 2014-12-02 2018-05-15 Ebm-Papst Mulfingen Gmbh & Co. Kg Ventilator
DE102019107706A1 (de) * 2019-03-26 2020-10-01 Ebm-Papst St. Georgen Gmbh & Co. Kg Lüftergehäuse mit integrierter Motorelektronik

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS634396U (https=) * 1986-06-25 1988-01-12
JP2000217303A (ja) * 1999-01-22 2000-08-04 Toshiba Home Technology Corp モ―タシャフトの取付構造
JP2000257597A (ja) * 1999-03-02 2000-09-19 Taida Electronic Ind Co Ltd ファンの増圧気流案内装置
JP2000303998A (ja) * 1999-04-23 2000-10-31 Nippon Densan Corp ファンモータ
JP2002005093A (ja) * 2000-06-21 2002-01-09 Minebea Co Ltd 送風機
JP3083969U (ja) * 2001-08-08 2002-02-22 建準電機工業股▲分▼有限公司 ファンの増圧構造
JP3098046U (ja) * 2003-05-26 2004-02-19 日本電産株式会社 リード線固定構造

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4548548A (en) * 1984-05-23 1985-10-22 Airflow Research And Manufacturing Corp. Fan and housing
JPS6141886U (ja) * 1984-08-21 1986-03-17 株式会社 日本計器製作所 フアン・モ−タ
JPS6218398A (ja) 1985-07-16 1987-01-27 三菱電機株式会社 人工衛星の制御装置
JPS6218398U (https=) * 1985-07-17 1987-02-03
JPS634396A (ja) 1986-06-25 1988-01-09 株式会社東芝 プラント機器障害監視装置
NZ224967A (en) 1988-06-09 1992-04-28 Albert Maurice Prowse Two-directional parallel rule; two pairs of wheels at right-angles selectively operable by tilting rule
JPH02103197U (https=) * 1989-02-06 1990-08-16
JPH02245500A (ja) * 1989-03-17 1990-10-01 Mitsubishi Electric Corp 送風機
JPH0392681U (https=) 1990-01-06 1991-09-20
JPH0399404U (https=) 1990-01-31 1991-10-17
JP3099404B2 (ja) 1991-04-24 2000-10-16 松下電器産業株式会社 水晶発振器
JP3092681B2 (ja) 1992-07-17 2000-09-25 ソニー株式会社 位相検出装置
DE19753373A1 (de) * 1996-12-10 1998-06-25 Papst Motoren Gmbh & Co Kg Axiallüfter-Gehäuse
JP3432380B2 (ja) 1996-12-27 2003-08-04 山洋電気株式会社 ブラシレスファンモータの製造方法
US6136250A (en) * 1998-01-30 2000-10-24 Comair Rotron, Inc. Apparatus and method of encapsulating motors
JP3572602B2 (ja) * 1998-04-17 2004-10-06 東芝ホームテクノ株式会社 冷却ファンモータ
JP3784178B2 (ja) 1998-10-07 2006-06-07 山洋電気株式会社 軸流送風機
TW523652B (en) * 2001-08-01 2003-03-11 Delta Electronics Inc Combination fan and applied fan frame structure
US6561762B1 (en) * 2001-11-14 2003-05-13 Sunonwealth Electric Machine Industry Co., Ltd. Housing structure of a fan
JP3092681U (ja) * 2002-09-10 2003-03-20 建準電機工業股▲分▼有限公司 放熱ファンのケーシングの改良構造
WO2004081387A1 (ja) * 2003-03-13 2004-09-23 Sanyo Denki Co.,Ltd. 二重反転式軸流送風機
CN2627259Y (zh) 2003-05-16 2004-07-21 奇鋐科技股份有限公司 散热风扇的壳座
TW569663B (en) * 2003-05-16 2004-01-01 Sunonwealth Electr Mach Ind Co Serial-connected heat dissipating fan module
JP3099404U (ja) * 2003-07-23 2004-04-08 チーホンコーチークーフェンユーシェンコンシー 冷却ファン装置及びそのハウジング

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS634396U (https=) * 1986-06-25 1988-01-12
JP2000217303A (ja) * 1999-01-22 2000-08-04 Toshiba Home Technology Corp モ―タシャフトの取付構造
JP2000257597A (ja) * 1999-03-02 2000-09-19 Taida Electronic Ind Co Ltd ファンの増圧気流案内装置
JP2000303998A (ja) * 1999-04-23 2000-10-31 Nippon Densan Corp ファンモータ
JP2002005093A (ja) * 2000-06-21 2002-01-09 Minebea Co Ltd 送風機
JP3083969U (ja) * 2001-08-08 2002-02-22 建準電機工業股▲分▼有限公司 ファンの増圧構造
JP3098046U (ja) * 2003-05-26 2004-02-19 日本電産株式会社 リード線固定構造

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP1847718A4 *

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JP4397832B2 (ja) 2010-01-13
US20080050232A1 (en) 2008-02-28
EP1847718B8 (en) 2017-03-15
EP1847718B1 (en) 2016-11-16
TW200636170A (en) 2006-10-16
JP2006214420A (ja) 2006-08-17
CN101115927B (zh) 2011-03-23
CN101115927A (zh) 2008-01-30
US7828519B2 (en) 2010-11-09
HK1112043A1 (en) 2008-08-22
TWI297748B (https=) 2008-06-11
EP1847718A4 (en) 2013-07-10
EP1847718A1 (en) 2007-10-24

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