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TW200628059A - Fan stator - Google Patents

Fan stator

Info

Publication number
TW200628059A
TW200628059A TW094137334A TW94137334A TW200628059A TW 200628059 A TW200628059 A TW 200628059A TW 094137334 A TW094137334 A TW 094137334A TW 94137334 A TW94137334 A TW 94137334A TW 200628059 A TW200628059 A TW 200628059A
Authority
TW
Taiwan
Prior art keywords
airfoils
fan stator
hub
housing
fixedly coupled
Prior art date
Application number
TW094137334A
Other languages
Chinese (zh)
Other versions
TWI312267B (en
Inventor
Gavin Stanley
Ketan Shah
Ben Broili
Original Assignee
Intel 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 Intel Corp filed Critical Intel Corp
Publication of TW200628059A publication Critical patent/TW200628059A/en
Application granted granted Critical
Publication of TWI312267B publication Critical patent/TWI312267B/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/541—Specially adapted for elastic fluid pumps
    • F04D29/542—Bladed diffusers
    • F04D29/544—Blade shapes

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

According to some embodiments, an apparatus includes a housing, a hub, and a plurality of airfoils, each of the plurality of airfoils having a leading edge, a trailing edge, a first end, and a second end, wherein the first end of each of the plurality of airfoils is fixedly coupled to the hub and wherein the second end of each of the plurality of airfoils is fixedly coupled to the housing.
TW094137334A 2004-10-29 2005-10-25 Cooling apparatus and system TWI312267B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/976,634 US20060093476A1 (en) 2004-10-29 2004-10-29 Fan stator

Publications (2)

Publication Number Publication Date
TW200628059A true TW200628059A (en) 2006-08-01
TWI312267B TWI312267B (en) 2009-07-11

Family

ID=35883470

Family Applications (1)

Application Number Title Priority Date Filing Date
TW094137334A TWI312267B (en) 2004-10-29 2005-10-25 Cooling apparatus and system

Country Status (5)

Country Link
US (1) US20060093476A1 (en)
CN (1) CN101044324B (en)
DE (1) DE112005002393T5 (en)
TW (1) TWI312267B (en)
WO (1) WO2006050285A1 (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140251238A1 (en) * 2014-05-19 2014-09-11 Perkins Engines Company Limited Heat exchanging system for internal combustion engine
TWI578670B (en) * 2015-05-20 2017-04-11 Visionary Dynamics Co Ltd A hub motor with a guide seat
US10989221B2 (en) * 2016-06-29 2021-04-27 Quanta Computer Inc. Cooling system for streamlined airflow
US11884128B2 (en) 2017-12-18 2024-01-30 Carrier Corporation Fan stator construction to minimize axial depth
US10451447B2 (en) 2018-01-04 2019-10-22 Mitsubishi Electric Research Laboratories, Inc. Polarization-dependent position encoder
DE102019110934A1 (en) * 2019-04-29 2020-10-29 Ebm-Papst Mulfingen Gmbh & Co. Kg Guide device for an axial fan

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2191341A (en) * 1937-02-26 1940-02-20 Jeffrey Mfg Co Ventilator
DE3605086A1 (en) * 1986-02-18 1987-08-27 Rhein Flugzeugbau Gmbh TRAINING OF COMPONENTS LOCATED INTO THE INFLOW TO AIR SCREWS, COVER SCREWS AND / OR FANS TO REDUCE THE ADDITIONAL NOISE YOU MAKE AND TO REDUCE THE ALTERNATE LOAD ON THE PROPELLER BLOWERS
EP0458880A4 (en) * 1989-02-14 1992-02-12 Airflow Research & Manufacturing Corp. Centrifugal fan with airfoil vanes in annular volute envelope
US6045327A (en) * 1998-05-04 2000-04-04 Carrier Corporation Axial flow fan assembly and one-piece housing for axial flow fan assembly
US6206635B1 (en) * 1998-12-07 2001-03-27 Valeo, Inc. Fan stator
US6199624B1 (en) * 1999-04-30 2001-03-13 Molex Incorporated Folded fin heat sink and a heat exchanger employing the heat sink
US20020094271A1 (en) * 2001-01-16 2002-07-18 Yeuan Jian J. Axial flow fan structure
TW568508U (en) * 2001-03-27 2003-12-21 Delta Electronics Inc Fan with good heat dissipation
GB2377321B (en) * 2001-07-05 2003-06-11 Enlight Corp CPU cooling structure with a ventilation hood
US6749043B2 (en) * 2001-10-22 2004-06-15 General Electric Company Locomotive brake resistor cooling apparatus

Also Published As

Publication number Publication date
WO2006050285A1 (en) 2006-05-11
DE112005002393T5 (en) 2007-09-20
US20060093476A1 (en) 2006-05-04
TWI312267B (en) 2009-07-11
CN101044324A (en) 2007-09-26
CN101044324B (en) 2012-06-13

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Legal Events

Date Code Title Description
MM4A Annulment or lapse of patent due to non-payment of fees