• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    1467659 Axial-flow fans; cooling IC engines INTERNATIONAL HARVESTER CO 5 April 1974 [5 April 1973] 15162/74 Headings FIB and F1C The subject matter of this Specification is substantially the same as that of Specification 1466795, but the flared portion of the fan cowl is modified, e.g. by providing apertures 55, so as to divide the flow leaving the cowl into distinct axial and radial streams.
    公开号:SU735161A3
    申请号:SU742014725
    申请日:1974-04-04
    公开日:1980-05-15
    发明作者:Д.Бек Гарольд；Л.Ханна Томас
    申请人:Интернэшнл Харвестер Компани (Фирма)；
    IPC主号:
    专利说明:

    (54) VEHICLE
    one
    FIELD OF THE INVENTION The invention relates to a transport engineering, in particular to vehicles equipped with a power plant and its blowing system.
    Known vehicles with a power plant equipped with a blowing system usually use an internal combustion engine and contain a radiator with side openings for inlet and outlet of purge air, a fan driven by an engine and with blades having front and rear edges, a fan casing equipped with serially interconnected and with lateral holes for the release of conical, cylindrical and torus sections, the latter of which is formed by a quarter of a circle and equipped with a flange with output edge, protruding radially one-third of the axial width of the blade 1.
    In the known device, the flow of air expelled in the axial direction through the radiator to blow the engine and the engine compartment consumes a considerable part of the engine power due to hydraulic resistance and creates a noise effect when passing through the fan and breaking off the edges of the casing and fan blades.
    The aim of the invention is to reduce the noise level generated by the fan and the power consumption of the engine to drive it. 5This is achieved by the fact that the tori section
    the fan casing is cut out to create radial and non-radial air flow. The cutouts are formed by parallel planes located on diametrically opposite sides
    10 sections. The parallel planes are spaced apart from each other by an amount smaller than the diameter of the cylindrical section or equal to its diameter, and the plane passing through the back edges of the blades coincides with the plane formed by the output edge
     flange, within ± 12% of the blade width. FIG. 1 shows a vehicle, side view of an internal combustion engine; in fig. 2 shows a fan casing connected to a radiator; on
    权利要求:
    Claims (5)
    [1]
    20 of FIG. 3 is a front view of the fan casing with one embodiment of the cut-outs; in fig. 4 is a side view of the fan COOKER of FIG. 3; in fig. 5 is a front view of a fan casing with a different cutout embodiment; in fig. 6 is a side view of the fan casing of FIG. 5. Vehicle 1 contains, as a power plant, an internal combustion engine 2 installed in the sub-cage 3. With the help of drive 4 (Fig. 2), a fan is connected to the engine 5. The drive can be made in the form of any known device, for example belt drive with pulley. The fan 5 is enclosed in the casing 6 (Fig. 1), the front edge of which (from the free end of the engine shaft) is connected to the housing of the water radiator 7, and is made with axial-type blades 8 (Fig. 2) providing air injection through a radiator 7 for heat exchange therein and cooling the engine 2, as well as for ventilation of the engine compartment 3. The radiator has an inlet 9 (FIG. 1) and an outlet 10 coolant nozzle for a engine cooling jacket. The fan casing 6 consists of the sections -conic 11 (fig. 2) connected in series between one another and attached with one edge to the radiator body 7, cylindrical 12 and torus 13, equipped with a flange 14, from which air is sucked by the fan 5. The flange 14 is formed by a part of the torus, the latter being made a quarter of a circle of radius R and provided with an output edge 15 extending radially and projecting in the radial direction by an amount equal to 1/3 of the axial extension of the fan blades 8. On the torus section 13, two parallel planes 16 located on diametrically opposite sides of the section, cutouts 17 are made to create simultaneously two streams of different types on the .., .-.,., I, .. l.; ..: -x- :: -itfХ -.:.:: - - Board: radial and non-radial, flowing smoothly around engine 2, as a result of which flow resistance on the fan 5 is reduced. Planes 16 passing through the surface of section 13 can be separated from each other by the diameter value D cylindrical section 12 of the casing 6 (Fig. 5 and 6) or by an amount slightly larger, dia an ether D of the fan casing (Fig. 3 and 4). In both cases, the effect of creating air flows in two directions is preserved. The rear edges 18 (Figs. 4 and 6) of the blades 8 form a plane that may coincide with the plane formed by the output edge 15 of the flange 14, or stand out from it within ± 12% of the axial spacing of the blades 0, i.e. the edges of the 18 blades may go beyond the edge 15 of the flange or fail to reach it, however the effect of creating radial and non-radial flows will be ensured. When the engine 2 is operating, the rotating fan 5 draws air from the atmosphere into the engine compartment 3 through the radiator 7, in which it is conventional. Cooling between the air and the engine coolant. The outgoing air from the edges 18 of the blades 8 takes axial direction, since the fan is axial. By making the fan casing, in particular its torus section, with the cutouts, the flow of air leaving the casing also acquires a radial direction and, partially, summing with the axial at the cutouts, is non-radial. This phenomenon contributes to a decrease in air resistance, converging from the fan blades, and, consequently, reduces the cost of engine power to drive the fan. It has been found that the best results are obtained with the following ratios of casing elements: the ratio of height and edge 15 of blade 8 to axial width in blades is 1/3, radius R forming the torus surface of flange 14 is selected in / 3, and axial width with cylindrical section 12-28/3. Claim 1. Transport means comprising an engine, a radiator with side holes for inlet and outlet of purge air, a fan driven by an engine, the blades of which have front and rear edges, and a fan casing provided in series with each other. with a side opening for discharging the conical, cylindrical and torus sections, the latter of which is formed by a quarter of a circle and provided with a flange with an output edge projecting radially one third of the axial spacing of the blade, lichayuschees in that, with a view to reducing the level schuma fan and power costs for its drive, Tore section is formed with notches for providing radial and non-radial airflows.
    [2]
    2. A vehicle according to claim 1, characterized in that the notches are formed by two parallel planes located diametrically on opposite sides ...,,
    [3]
    3 .. Vehicle rio nos. 1 and 2, characterized in that the parallel planes are spaced apart from each other by an amount smaller than the diameter of the cylindrical section.
    [4]
    4. Vehicle on PP. 1 and 2, characterized in that the parallel planes are spaced apart from each other by an amount equal to the diameter of the cylindrical section |
    [5]
    5. Vehicle on PP. 1-4; characterized in that the plane passing through the back edges of the blades coincides with the plane formed by the exit edge of the flange, within ± 12% of the width of the blade. And the information clerks take into account in the examination 1. U.S. Patent No. 3144859, cl. 123-41.49, publ. 1964.
    (Rig.5
    类似技术:
    公开号 | 公开日 | 专利标题
    SU735161A3|1980-05-15|Vehicle
    US4173995A|1979-11-13|Recirculation barrier for a heat transfer system
    EP0026997B1|1983-11-02|Shroud arrangement for engine cooling fan
    US4685513A|1987-08-11|Engine cooling fan and fan shrouding arrangement
    ES2321041T3|2009-06-01|AXIAL FAN WITH MOTOR WITH SELF-COOLED.
    US8746186B2|2014-06-10|Rotating screen for centrifugal fan
    US4411598A|1983-10-25|Fluid propeller fan
    AU605042B2|1991-01-03|Shrouding for engine cooling fan
    US4505641A|1985-03-19|Cooling fan for internal combustion engine
    US4396351A|1983-08-02|Engine cooling fan
    US4448573A|1984-05-15|Single-stage, multiple outlet centrifugal blower
    KR900018634A|1990-12-22|Fan stator assembly for heat exchanger
    EP0735252A2|1996-10-02|Engine cooling system
    US4364712A|1982-12-21|Cross flow cooling fan
    GB1466795A|1977-03-09|Fan and cowl assembly in a vehicle
    JP2001289197A|2001-10-19|Method and device for increasing operating area of centrifugal compressor
    RU2004103479A|2005-07-10|TURBINE HIGH PRESSURE TURBINE ROTOR VENTILATION DEVICE
    US4210835A|1980-07-01|Fan with a cooled motor
    SE439037B|1985-05-28|COMBUSTION ENGINE COOLING DEVICE
    GB1489880A|1977-10-26|Cooling of internal combustion engines
    KR880012891A|1988-11-29|Centrifugal compressor
    US2037880A|1936-04-21|Fan
    GB1596749A|1981-08-26|Mixed flow fan
    US6123051A|2000-09-26|Shroud for an engine cooling fan
    US2896595A|1959-07-28|Method and apparatus for cooling of radiators of engines and the like
    同族专利:
    公开号 | 公开日
    DE2411268A1|1974-10-24|
    NL158256B|1978-10-16|
    GB1467659A|1977-03-16|
    AU6756674A|1975-10-09|
    BR7402686D0|1974-11-19|
    FR2224319B1|1978-03-10|
    IT1004095B|1976-07-10|
    US3858644A|1975-01-07|
    FR2224319A1|1974-10-31|
    NL7404586A|1974-10-08|
    CA989264A|1976-05-18|
    AU471445B2|1976-04-29|
    SE405390B|1978-12-04|
    JPS49129033A|1974-12-10|
    引用文献:
    公开号 | 申请日 | 公开日 | 申请人 | 专利标题
    US608377A|1898-08-02|Neil w |
    US1190777A|1915-06-15|1916-07-11|Motor Cooling Systems Company|Cooling system.|
    US1519812A|1923-06-04|1924-12-16|Schneider Heinrich|Locomotive driven by internal-combustion engine|
    US1691598A|1925-08-23|1928-11-13|Sulzer Ag|Internal-combustion-engine locomotive|
    US1671373A|1927-10-24|1928-05-29|Thomas B Martin|Double cooling fan for automobiles or the like|
    US1966787A|1931-03-27|1934-07-17|Sulzer Ag|Cooling fan for vehicles driven by internal combustion engines|
    US2142307A|1934-06-14|1939-01-03|Mey Rene De|Mounting of axial flow fans and the like|
    US2252256A|1939-01-11|1941-08-12|Harris Eliot Huntington|Sound attenuator for air impellers|
    US2225398A|1939-09-13|1940-12-17|Clyde M Hamblin|Construction of ventilating fans|
    US2415621A|1944-10-20|1947-02-11|Solar Aircraft Co|Fan|
    US2664961A|1947-10-24|1954-01-05|Joy Mfg Co|Adjustable blade fan|
    US2544490A|1949-07-07|1951-03-06|Jeffrey Mfg Co|Adjustable cowling for fans or the like|
    US2668523A|1952-12-11|1954-02-09|Chrysler Corp|Fan shroud|
    US3144859A|1962-02-15|1964-08-18|Young Radiator Co|Fan-shroud structure and mounting|
    GB1215136A|1967-02-20|1970-12-09|Kort Propulsion Co Ltd|Improvements in nozzles or shrouds for ships' propellers|
    GB1308310A|1969-05-19|1973-02-21|Lips Nv|Ships propeller shrouded by a nozzle|US3995603A|1974-04-08|1976-12-07|Hans List|Cooler-cum-blower assembly for internal combustion engines|
    AT335231B|1974-04-08|1977-02-25|List Hans|COOLER FAN UNIT FOR COMBUSTION MACHINERY|
    US3937192A|1974-09-03|1976-02-10|General Motors Corporation|Ejector fan shroud arrangement|
    US4173995A|1975-02-24|1979-11-13|International Harvester Company|Recirculation barrier for a heat transfer system|
    DE2540040C3|1975-09-09|1979-06-07|Motoren- Und Turbinen-Union Friedrichshafen Gmbh, 7990 Friedrichshafen|Ventilation arrangement for an engine room|
    US4018297A|1975-11-03|1977-04-19|Allis-Chalmers Corporation|Four-piece fan shroud|
    JPS6047453B2|1978-01-13|1985-10-22|Toyota Motor Co Ltd|
    US4329946A|1979-10-09|1982-05-18|General Motors Corporation|Shroud arrangement for engine cooling fan|
    US4394111A|1981-09-11|1983-07-19|Snyder General Corporation|Top cover, motor, fan and fan shroud assembly for an air conditioning unit|
    DE4137703C1|1991-11-15|1992-12-10|Mercedes-Benz Aktiengesellschaft, 7000 Stuttgart, De|
    US6874990B2|2003-01-29|2005-04-05|Siemens Vdo Automotive Inc.|Integral tip seal in a fan-shroud structure|
    US7008175B2|2003-06-03|2006-03-07|Saied Fathi|Radiator cooling fan replacement to increase engine efficiency|
    US20060272800A1|2005-06-02|2006-12-07|Paccar Inc|Radiator fan shroud with flow directing ports|
    US7478993B2|2006-03-27|2009-01-20|Valeo, Inc.|Cooling fan using Coanda effect to reduce recirculation|
    WO2009000462A1|2007-06-22|2008-12-31|Thermo King Container-Denmark A/S|Refrigerating container for ships|
    WO2009000461A2|2007-06-22|2008-12-31|Thermo King Deutschland Gmbh|Refrigerating container for land, road and rail vehicles|
    US8221074B2|2007-12-21|2012-07-17|Paccar Inc|Fan ring shroud assembly|
    DK177428B1|2009-01-14|2013-05-21|Novenco As|axial blower|
    US8649171B2|2010-02-26|2014-02-11|Hewlett-Packard Development Company, L.P.|Mixed-flow ducted fan|
    US8939724B2|2010-05-31|2015-01-27|Green Earth Power Company Limited|System and methods for wind energy recapture from a non natural wind source|
    USD736261S1|2012-11-29|2015-08-11|Cummins Inc.|Shroud|
    US9551356B2|2013-10-04|2017-01-24|Caterpillar Inc.|Double bell mouth shroud|
    DE102014111767A1|2014-08-18|2016-02-18|Ebm-Papst Mulfingen Gmbh & Co. Kg|Axial|
    USD921883S1|2018-07-25|2021-06-08|Vornado Air, Llc|Fan head|
    US10947991B2|2019-03-15|2021-03-16|Deere & Company|Fan shroud|
    法律状态:
    优先权:
    申请号 | 申请日 | 专利标题
    US348437A|US3858644A|1973-04-05|1973-04-05|Fan shroud exit structure|
    [返回顶部]