US20210207520A1 - Turbine for tangential fan intended for being provided in a motor vehicle, tangential fan, ventilation device and heat-exchange module for a motor vehicle - Google Patents

Turbine for tangential fan intended for being provided in a motor vehicle, tangential fan, ventilation device and heat-exchange module for a motor vehicle Download PDF

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Publication number
US20210207520A1
US20210207520A1 US17/059,779 US201917059779A US2021207520A1 US 20210207520 A1 US20210207520 A1 US 20210207520A1 US 201917059779 A US201917059779 A US 201917059779A US 2021207520 A1 US2021207520 A1 US 2021207520A1
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US
United States
Prior art keywords
blades
impeller
stage
heat
air
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.)
Abandoned
Application number
US17/059,779
Other languages
English (en)
Inventor
Kamel Azzouz
Michael Lissner
Amrid Mammeri
Ivan Dobrev
Sofiane Khelladi
Farid Bakir
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.)
Valeo Systemes Thermiques SAS
Original Assignee
Valeo Systemes Thermiques SAS
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 Valeo Systemes Thermiques SAS filed Critical Valeo Systemes Thermiques SAS
Assigned to VALEO SYSTEMES THERMIQUES reassignment VALEO SYSTEMES THERMIQUES ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: LISSNER, Michael, Azzouz, Kamel, BAKIR, FARID, DOBREV, Ivan, KHELLADI, Sofiane, MAMMERI, Amrid
Publication of US20210207520A1 publication Critical patent/US20210207520A1/en
Abandoned legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/02Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal
    • F04D17/04Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps having non-centrifugal stages, e.g. centripetal of transverse-flow type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01PCOOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
    • F01P5/00Pumping cooling-air or liquid coolants
    • F01P5/02Pumping cooling-air; Arrangements of cooling-air pumps, e.g. fans or blowers
    • 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
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/663Sound attenuation
    • F04D29/665Sound attenuation by means of resonance chambers or interference
    • 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
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/661Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
    • F04D29/666Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps by means of rotor construction or layout, e.g. unequal distribution of blades or vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/14Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being elastic fluid
    • F04F5/16Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow the inducing fluid being elastic fluid displacing elastic fluids
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/44Component parts, details, or accessories not provided for in, or of interest apart from, groups F04F5/02 - F04F5/42
    • F04F5/46Arrangements of nozzles
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/44Component parts, details, or accessories not provided for in, or of interest apart from, groups F04F5/02 - F04F5/42
    • F04F5/46Arrangements of nozzles
    • F04F5/466Arrangements of nozzles with a plurality of nozzles arranged in parallel
    • 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
    • F04D25/08Units comprising pumps and their driving means the working fluid being air, e.g. for ventilation
    • 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
    • F04D29/26Rotors specially for elastic fluids
    • F04D29/28Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
    • F04D29/281Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers
    • F04D29/282Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers the leading edge of each vane being substantially parallel to the rotation axis
    • F04D29/283Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for fans or blowers the leading edge of each vane being substantially parallel to the rotation axis rotors of the squirrel-cage type

Definitions

  • the first rectilinear part extends over a portion of the first profile corresponding to a length, measured in a direction perpendicular to the direction of alignment of the ducts and to a longitudinal direction of the ducts, that is greater than or equal to 30 mm, preferably greater than or equal to 40 mm, and/or less than or equal to 50 mm;
  • the distance between the second rectilinear part of the first profile and the rectilinear part of the second profile is greater than or equal to 2 mm and/or less than or equal to 10 mm, preferably less than or equal to 5 mm;
  • the ventilation device further comprises a third tube, such that the second profile of the second tube faces the second profile of the third tube, the distance between the center of the geometric section of the second tube and the center of the geometric section of the third tube preferably being less than the distance between the center of the geometric section of the first tube and the center of the geometric section of the tube; and
  • FIG. 7 schematically depicts a superposition of views in section on planes A-A and B-B of FIG. 6 ;
  • the row of ventilation tubes 8 may be arranged at a distance less than or equal to 150 mm from the row of heat-transfer tubes 4 , preferably less than or equal to 100 mm This distance is preferably greater than or equal to 5 mm, preferably greater than 40 mm This is because too short a distance between the ventilation tubes 8 and the heat-transfer tubes 4 carries the risk of not allowing uniform mixing of the flow of air ejected from the ventilation tubes 8 with the induced flow of air.
  • the impeller 102 comprises a plurality of blades 110 (or vanes) distributed in stages 112 along the longitudinal axis L 102 of the impeller 102 .
  • the longitudinal axis L 102 of the impeller corresponds to its axis of rotation when driven by the motor of the fan 100 .
  • the impeller 102 comprises thirteen stages 112 of blades 110 . Of course, this number of stages 112 is nonlimiting.
  • the openings 16 consist of slots made in the wall 17 of the ventilation tube 8 , these slots 16 extending in the direction of elongation of the ventilation tube 8 .
  • This slotted shape makes it possible to form an air passage of large dimensions, while at the same time maintaining satisfactory structural integrity of the ventilation tubes 8 .
  • the openings 16 extend over a large proportion of the length of the ventilation tube 8 , preferably over a total length corresponding to at least 90% of the length of the ventilation tube 8 .
  • the aerodynamic tube 8 illustrated in FIGS. 10 to 12 also comprises at least one opening 40 for ejecting a flow of air passing along the aerodynamic tube 8 , outside the aerodynamic tube 8 and outside the air inlet header 12 , notably substantially toward the heat exchanger 1 .
  • the opening or each opening 40 is, for example, a slot in an external wall 41 of the aerodynamic tube 8 , the slot or slots extending for example in the direction of elongation of the aerodynamic tube 8 in which they are made.
  • the total length of the opening 40 or of the openings may be greater than 90% of the length of the aerodynamic tube.
  • Each opening 40 is distinct from the ends of the aerodynamic tube 8 , via which ends the aerodynamic tube 8 opens into an air header 12 .
  • Each opening 40 is also outside of the air inlet header 12 .
  • the slotted shape makes it possible to form a large-sized air passage toward the heat exchanger 1 without excessively reducing the mechanical strength of the aerodynamic tubes 8 .
  • the distance f separating the second rectilinear part 38 a of the first profile 42 and the portion 38 b of the rectilinear part 48 of the second profile 44 that faces it may, however, be less than the distance separating the first longitudinal wall and the second longitudinal wall of the heat-transfer tube facing which the aerodynamic tube 8 is positioned.
  • the openings 40 are analogous to those of the example of FIG. 12 .
  • the distance e separating the internal 40 b and external 40 a lips of each opening 40 can be greater than or equal to 0.3 mm, preferably greater than or equal to 0.5 mm, more preferably greater than or equal to 0.7 mm, and/or less than or equal to 2 mm, preferably less than or equal to 1.5 mm, more preferably less than or equal to 0.9 mm, and even more preferably less than or equal to 0.7 mm.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
US17/059,779 2018-05-31 2019-05-29 Turbine for tangential fan intended for being provided in a motor vehicle, tangential fan, ventilation device and heat-exchange module for a motor vehicle Abandoned US20210207520A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1854746A FR3081942B1 (fr) 2018-05-31 2018-05-31 Turbine pour ventilateur tangentiel destine a equiper un vehicule automobile, ventilateur tangentiel, dispositif de ventilation et module d’echange de chaleur pour vehicule automobile
FR1854746 2018-05-31
PCT/FR2019/051264 WO2019229382A1 (fr) 2018-05-31 2019-05-29 Turbine pour ventilateur tangentiel destiné à équiper un véhicule automobile, ventilateur tangentiel, dispositif de ventilation et module d'échange de chaleur pour véhicule automobile

Publications (1)

Publication Number Publication Date
US20210207520A1 true US20210207520A1 (en) 2021-07-08

Family

ID=62875020

Family Applications (1)

Application Number Title Priority Date Filing Date
US17/059,779 Abandoned US20210207520A1 (en) 2018-05-31 2019-05-29 Turbine for tangential fan intended for being provided in a motor vehicle, tangential fan, ventilation device and heat-exchange module for a motor vehicle

Country Status (5)

Country Link
US (1) US20210207520A1 (fr)
EP (1) EP3781797A1 (fr)
CN (1) CN112534123A (fr)
FR (1) FR3081942B1 (fr)
WO (1) WO2019229382A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20230122270A1 (en) * 2020-03-04 2023-04-20 Lg Electronics Inc. Blower

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3082884B1 (fr) 2018-06-26 2021-01-15 Valeo Systemes Thermiques Dispositif de ventilation pour vehicule automobile

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2878989A (en) * 1957-01-31 1959-03-24 Vernco Corp Multiple length spiral bladed blower wheel
AT404057B (de) 1986-02-03 1998-08-25 Avl Verbrennungskraft Messtech Wärmetauschersystem mit einem querstromlüfter
JPH0742692A (ja) * 1993-07-28 1995-02-10 Hitachi Ltd 貫流ファンおよびこれを備えた空気調和機
JP2001214740A (ja) 2000-01-28 2001-08-10 Denso Corp クロスフローファン冷却装置
JP2005307929A (ja) * 2004-04-26 2005-11-04 Calsonic Kansei Corp 送風機
JP2006296775A (ja) * 2005-04-21 2006-11-02 Mitsubishi Electric Corp 電気掃除機の床用吸込具及びそれを備えた電気掃除機
KR20110001664A (ko) * 2009-06-30 2011-01-06 기아자동차주식회사 자동차
FR2989423B1 (fr) * 2012-04-16 2015-03-06 Valeo Systemes Thermiques Ventilateur pour automobile a encombrement axial reduit
FR2989999B1 (fr) * 2012-04-26 2016-01-01 Sdmo Ind Dispositif de refroidissement comprenant un ventilateur axial a redressement de flux centripete et groupe electrogene correspondant.
JP2014020245A (ja) * 2012-07-17 2014-02-03 Calsonic Kansei Corp 冷却ファン装置
CN107676299A (zh) * 2017-10-31 2018-02-09 华南理工大学 一种带叶片式空气分离器的双导流环形风扇

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20230122270A1 (en) * 2020-03-04 2023-04-20 Lg Electronics Inc. Blower
US11982293B2 (en) * 2020-03-04 2024-05-14 Lg Electronics Inc. Blower

Also Published As

Publication number Publication date
EP3781797A1 (fr) 2021-02-24
CN112534123A (zh) 2021-03-19
FR3081942A1 (fr) 2019-12-06
FR3081942B1 (fr) 2021-05-21
WO2019229382A1 (fr) 2019-12-05

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Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:AZZOUZ, KAMEL;LISSNER, MICHAEL;MAMMERI, AMRID;AND OTHERS;SIGNING DATES FROM 20210203 TO 20210204;REEL/FRAME:057143/0321

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Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION