US3842902A - Labyrinthian fan - Google Patents

Labyrinthian fan Download PDF

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US3842902A
US3842902A US00376692A US37669273A US3842902A US 3842902 A US3842902 A US 3842902A US 00376692 A US00376692 A US 00376692A US 37669273 A US37669273 A US 37669273A US 3842902 A US3842902 A US 3842902A
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Prior art keywords
fan
shroud
labyrinth seal
flange
hoop
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Expired - Lifetime
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US00376692A
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W Poslusny
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Hayes-Albion Corp
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Hayes-Albion Corp
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Priority to US00376692A priority Critical patent/US3842902A/en
Priority to CA203,688A priority patent/CA1007618A/en
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Assigned to CONTINENTAL BANK reassignment CONTINENTAL BANK AMENDED AND REINSTATED SECURITY AGREEMENT Assignors: HARVARD INDUSTRIES, INC.
Assigned to CONTINENTAL BANK, N.A., AS AGENT reassignment CONTINENTAL BANK, N.A., AS AGENT CORRECTIVE ASSIGNMENT TO CORRECT THE ASSIGNOR + ASSIGNEE ON REEL 6282/0523 ON SECURITY INTEREST. Assignors: BIRMINGHAM BENDERS COMPANY, DECKERVILLE DIE-FORM CO., HARMAN AUTOMOTIVE, INC., HARMAN AUTOMOTIVE-PUERTO RICO, INC., HARVARD INDUSTRIES, INC., INDIVIDUALLY AND D/B/A ELASTIC STOP NUT (ESNA), AND ALSO D/B/A HARVARD INTERIORS, HARVARD TRANSPORTATION CORPORATION, HAYES-ALBION CORPORATION, KINGSTON-WARREN CORPORATION, THE, SNOVER STAMPING CO., TRIM TRENDS, INC.
Assigned to SNOVER STAMPING CO., HAYES-ALBION CORPORATION, HARVARD INDUSTRIES, INC. (HARVARD INTERIORS MANUFACTURING COMPANY DIVISION), HARMAN AUTOMOTIVE - PUERTO RICO, INC., TRIM TRENDS, INC., HARMAN AUTOMOTIVE, INC., HARVARD INDUSTRIES, INC. (ELASTIC STOP NUT DIVISION), BIRMINGHAM BENDERS COMPANY, DECKERVILLE DIE-FORM CO., HARVARD TRANSPORTATION CORPORATION, KINGSTON-WARREN CORPORATION, THE, HARVARD INDUSTRIES, INC. reassignment SNOVER STAMPING CO. RELEASE OF SECURITY INTEREST RECORDED AT THE PTO O Assignors: BANK OF AMERICA NATIONAL TRUST AND SAVINGS ASSOCIATION, AS SUCCESSOR IN INTEREST BY ACQUISITION OF CONTINENTAL BANK, N.A.
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    • 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
    • F04D29/08Sealings
    • F04D29/16Sealings between pressure and suction sides
    • F04D29/161Sealings between pressure and suction sides especially adapted for elastic fluid pumps
    • F04D29/164Sealings between pressure and suction sides especially adapted for elastic fluid pumps of an axial flow wheel
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • 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
    • F04D29/32Rotors specially for elastic fluids for axial flow pumps
    • F04D29/325Rotors specially for elastic fluids for axial flow pumps for axial flow fans
    • F04D29/326Rotors specially for elastic fluids for axial flow pumps for axial flow fans comprising a rotating shroud

Definitions

  • This invention relates to engine cooling systems and in particular to an improved fan system for use in the cooling systems.
  • the prior art fans are normally affixed to the engine which in turn is resiliently mounted to the vehicle frame. This resiliency isolates engine vibration from the vehicle and results in the engine moving as a reaction to its output torque.
  • a heat exchanger or radiator and a stationary shroud are solidly mounted to the vehicle frame. To accommodate the relative movement between the fan and stationary shroud, and to allow for variances in installation, it is normal to provide clearance between these two members of to 1 inch radially.
  • a rotating member is added to the fan at the periphery with a minimum clearance between the blade tips and this member, hereinafter referred to as a rotating LII shroud.
  • This rotating shroud coacts with the stationary shroud, a box-like enclosure attached to the radiator. These two shrouds form a labyrinth seal in the clearance space between them, hereinafter referred to as the shroud gap.
  • the entire system thereby minimizes and mechanically separates the undesired turbulent flows. This action significantly reduces blade shear through turbulent flow patterns and results in improved useful air delivery, reduced input horsepower requirements, and greatly reduced noise generation.
  • a labyrinthian fan is constructed by disposing a U-shaped rotating shroud around the circumference of the fan.
  • the fore and aft disc portions of the U-channel extend radially outwardly from the fan circumference.
  • the stationary shroud a box-like structure, includes a circular orifice of lesser dimension than the sides of the box. This orifree is disposed between the disc portions of the rotating shroud forming a labyrinth seal in the shroud gap.
  • FIG. I is a plan view of a fan and shroud constructed in accordance with the principles of this invention.
  • FIG. 2 is a cross-sectional view of the fan and shroud shown in FIG. 1.
  • FIG. 3 schematically depicts the problem in the prior art solved by this invention.
  • FIG. 4 schematically depicts the air flow associated with fans constructed in accordance with this inventron.
  • FIGS. 5-9 schematically illustrate exemplary alternate embodiments of the invention.
  • a labyrinthian fan constructed in accordance with the principles of this invention is denoted generally by the reference numeral 10 in FIGS. 1 and 2.
  • the fan includes a central hub 12 with mounting holes 14.
  • a plurality of blades 16 emanate radially from the hub 12.
  • the particular type of fan is immaterial to this invention and thus the fan 10 has been illustrated somewhat diagrammatically. However, this invention may be used with any type of fan such as flex-fans, temperature sensitive fans and the like.
  • a sealing member 18 is affixed to the tips of the fan blades 16.
  • the sealing member 18 is in the form of a U-shaped channel, however, as will be treated in detail hereinafter, other configurations could be used.
  • the U-shape is preferred because of its rigidity in resisting deformation and the resulting stresses when the fan is rotating.
  • the sealing member 18 may be attached to the fan blades in any conventional manner; i.e., bolts, rivets, welds and the like.
  • the fan 10 is positioned behind a radiator 20.
  • a box-like stationary shroud 22 surrounds the fan 10.
  • the shroud 22 includes a downwardly turned flange 24 which operates in conjunction with the sealing member 18 to form a labyrinth seal at the shroud gap 30.
  • FIG. 3 illustrates a conventional fan blade 26, which is rotatably mounted behind a heat exchanger or radiator to the engine 34 by conventional means (not shown) and a shroud 28. Because the engine to which the fan is mounted moves relative to the shroud 28, a shroud gap is provided to prevent contact between the fan 26 and the shroud 28. As stated earlier, the shroud gap 30 is generally from %to 1 inch radially. This relatively large shroud gap 30 permits undesirable turbulent airflows to occur about the fan blade tips. These flow conditions have been schematically depicted in FlG. 3.
  • the flow indicated as 32 is the desirable flow which provides useful heat exchanger cooling air.
  • Flow path 38 indicated as a torous pattern in the shroud gap 30, and flow 39, depicted as a localized flow at each blade tip, are undesirable. They produce no useful cooling air movement, cause fan noise, and create losses in fan efficiency.
  • FIG. 4 the preferred embodiment flow conditions are schematically illustrated. It is readily apparent that any recirculating flow 38 in the shroud gap 30 will have to follow a twisted or tortuous path because of the labyrinth seal formed by the flange 24 and the sealing member 18.
  • the tortured nature of the shroud gap greatly increases the paths resistance to fluid flow and consequently reduces the amount of recirculating air. By reducing the recirculating air 38, the amount of desirable flow 32 is increased and the noise caused by the recirculating air 38 is reduced. Additional benefits are achieved since the clearance between the fan blades and the rotating shroud is extremely small, thereby essentially eliminating flow 39. However, the rotating shroud 18 could be spaced somewhat from the blade 16.
  • FIGS. 7-9 schematically illustrate three possible configurations. Many more could be used. The embodiment discussed is preferred because of the strength requirements in vehicular systems with high rotational speeds. In low speed applications other constructions may be preferred. Many other designs can be utilized without departing from the scope and spirit of the invention as is set forth in the appended claims.
  • a fan rotatably mounted to said engine and having a plurality of blades and including sealing means for creating a labyrinth seal;
  • shroud mounted to said heat exchanger and encircling said fan, said shroud having means for coacting with said sealing means on said fan to form a labyrinth seal in the gap between said shroud and said fan;
  • said means on said fan and said shroud which form said labyrinth seal being disposed such that relative axial and radial movement therebetween does not interfere with the rotation of said fan.
  • sealing means is a U-shaped hoop circumferentially disposed about said fan blades and said coacting means is an inwardly turned flange on said shroud.
  • a fan rotatably mounted to said engine and having a pluarlity of blades and including a substantially U- shaped hoop disposed about the perimeter of said blades for creating a labyrinth seal;
  • a shroud mounted to said heat exchanger and encircling said fan, said shroud having an inwardly depending flange entering the bight of said hoop for coacting with said hoop to form a labyrinth seal in the gap between said shroud and said fan;
  • said hoop and said flange which form said labyrinth seal being disposed such that relative axial and radial movement therebetween does not interfere with the rotation of said fan.

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

Abstract

An improved fan including means to form a seal at the fan tips and means to form a labyrinthian seal in the shroud gap. The combination of seals increases the effective airflow of the fan, reduces the operational noise, and reduces the horsepower required to drive the fan.

Description

nited States Patent 1.
1111 3,842,902 Poslusny 1 Oct. 22, 1974 LABYRINTHIAN FAN 3,572,728 3/1971 Smuland 415/171 3,677,660 7/1972 Taniguchi et al. 415/172 [751 lnvemorwarm" mlusny Jackson, Mlch- 3,680,977 8/1972 Rabouyt et al. 415/172 3 Assignee: Hayes A|bi0n Corporation, Jackson, 3,701,536 10/1972 Matthews et a1. 415/172 Mlch' FOREiGN PATENTS OR APPLlCATlONS [22] Filed: July 5, 1973 933,618 8/1963 Great Britain 415/172 [21] Appl. No.: 376,692
Primary Examiner-Manuel A. Antonakas Assistant ExaminerS. .1. Richter [52} US. Cl 165/51, 123/4149, 165/122,
415/172 Attorney, Agent, or rrm John L. Cline [51] Int. Cl. F281 13/06 [58] Field of Search 165/134, 51, 122; [57] ABSTRACT 123/4149; 172; 277/53 57 An improved fan including means to form a seal at the 6 f d fan tips and means to form a labyrinthian seal in the [5 1 Re erences shroud gap. The combination of seals increases the ef- UNITED STATES PATENTS fective airflow of the fan, reduces the operational 176,755 5/1876 Murphy 416/189 noise, and reduces the horsepower required to drive 1,292,830 1/1919 McCain 416/191 the fan, 2,634,713 4/1953 Bartch et al. 123/4149 2,668,523 2/1954 Lamb 123/4149 5 Claims, 9 Drawing Figures Pmmmwww 3.842.902
(PRIOR ART) LABYRINTHIAN FAN BACKGROUND OF THE INVENTION This invention relates to engine cooling systems and in particular to an improved fan system for use in the cooling systems.
The automotive industry has been faced with ever increasing cooling demands in vehicles. Increases in engine size and the addition of both pollution control equipment and power operated accessories have contributed to the need for higher cooling capacity.
At the same time as the demands for higher cooling capacity have increased, the demand for quieter operation has likewise increased. Because, in general, the noise attributed to the fan increases as its capacity to cool increases, the industry has been faced with a dilemma.
Also, with the addition of more auxillary equipment it is desirable to reduce the horsepower demands of the fan. This has beendifficult because the horsepower needed to drive the fan, in general, increases as its capacity to cool increases.
There have been attempts to solve this problem. One of these is the flex-fan, which reduces pitch as engine speed increases and thereby reduces the noise and horsepower necessary to drive the fan at high speeds. Other fans have been developed which are temperature sensitive. They reduce pitch as the ambient and/or engine termperature is lowered and therefore reduce .noise and horsepower requirements when the cooling SUMMARY OF THE INVENTION This invention presents a fan and a combination of a fan and shroud which dramatically increases the useable air flow of a given fan, improves its efficiency, and at the same time reduces the noise. Typically, the air flow is increased with a net decrease in noise. That is, the additional noise produced by the increased air flow is less than that eliminated by use of the invention.
If it is desired to maintain a certain airflow, large reductions in noise are observed in systems constructed in accordance with this invention. The constant airflow may be achieved by lessening the pitch and/or diameter of the fan and also by reducing its operating rotational speed. Thus, systems constructed in accordance with this invention produce less noise, require less input horsepower, and produce greater airflow than prior art fans.
The prior art fans are normally affixed to the engine which in turn is resiliently mounted to the vehicle frame. This resiliency isolates engine vibration from the vehicle and results in the engine moving as a reaction to its output torque. A heat exchanger or radiator and a stationary shroud are solidly mounted to the vehicle frame. To accommodate the relative movement between the fan and stationary shroud, and to allow for variances in installation, it is normal to provide clearance between these two members of to 1 inch radially.
The invention accomplishes the remarkable improvements without reducing these required clearances. A rotating member is added to the fan at the periphery with a minimum clearance between the blade tips and this member, hereinafter referred to as a rotating LII shroud. This rotating shroud coacts with the stationary shroud, a box-like enclosure attached to the radiator. These two shrouds form a labyrinth seal in the clearance space between them, hereinafter referred to as the shroud gap.
Three separate phenomena exist at the outside diameter of prior art fans: l a localized flow of air from the pressure side of a blade to its suction side over the blade tip; (2) a toroidal circulation of air from the exhaust side of the fan to the inlet side of the fan; and (3) a continuous shearing action through these turbulent flow regimes caused by the fan blade rotation.
The addition of the rotating shroud to the fan circum' ference, with minimal clearances, effectively limits air flow from the pressure side of the fan blade to its suction side over the blade tip. The rotating shroud coacting with the stationary shroud in a labyrinth sealing relationship greatly reduces the recirculating toroidal flow from the high-pressure fan discharge to the lowpressure fan inlet zone in the shroud gap. The entire system thereby minimizes and mechanically separates the undesired turbulent flows. This action significantly reduces blade shear through turbulent flow patterns and results in improved useful air delivery, reduced input horsepower requirements, and greatly reduced noise generation.
In the preferred embodiment, a labyrinthian fan is constructed by disposing a U-shaped rotating shroud around the circumference of the fan. The fore and aft disc portions of the U-channel extend radially outwardly from the fan circumference. The stationary shroud, a box-like structure, includes a circular orifice of lesser dimension than the sides of the box. This orifree is disposed between the disc portions of the rotating shroud forming a labyrinth seal in the shroud gap. Thus, the recirculation flows are reduced and the concurrent benefits of reduced noise, increased airflow, and reduced horsepower are realized.
BRIEF DESCRIPTION OF THE DRAWINGS The features of this invention will become more apparent in the following detailed description of a preferred embodiment when read in conjunction with the figures in which:
FIG. I is a plan view of a fan and shroud constructed in accordance with the principles of this invention.
FIG. 2 is a cross-sectional view of the fan and shroud shown in FIG. 1.
FIG. 3 schematically depicts the problem in the prior art solved by this invention.
FIG. 4 schematically depicts the air flow associated with fans constructed in accordance with this inventron.
FIGS. 5-9 schematically illustrate exemplary alternate embodiments of the invention.
DETAILED DESCRIPTION OF A PREFERRED EMBODIMENT A labyrinthian fan constructed in accordance with the principles of this invention is denoted generally by the reference numeral 10 in FIGS. 1 and 2. The fan includes a central hub 12 with mounting holes 14. A plurality of blades 16 emanate radially from the hub 12. The particular type of fan is immaterial to this invention and thus the fan 10 has been illustrated somewhat diagrammatically. However, this invention may be used with any type of fan such as flex-fans, temperature sensitive fans and the like.
A sealing member 18 is affixed to the tips of the fan blades 16. In this preferred embodiment the sealing member 18 is in the form of a U-shaped channel, however, as will be treated in detail hereinafter, other configurations could be used. The U-shape is preferred because of its rigidity in resisting deformation and the resulting stresses when the fan is rotating. The sealing member 18 may be attached to the fan blades in any conventional manner; i.e., bolts, rivets, welds and the like.
As seen in FIG. 2 the fan 10 is positioned behind a radiator 20. A box-like stationary shroud 22 surrounds the fan 10. The shroud 22 includes a downwardly turned flange 24 which operates in conjunction with the sealing member 18 to form a labyrinth seal at the shroud gap 30.
Turning now to FIGS. 3 and 4, the operating principles of this invention, as now understood, will be described. FIG. 3 illustrates a conventional fan blade 26, which is rotatably mounted behind a heat exchanger or radiator to the engine 34 by conventional means (not shown) and a shroud 28. Because the engine to which the fan is mounted moves relative to the shroud 28, a shroud gap is provided to prevent contact between the fan 26 and the shroud 28. As stated earlier, the shroud gap 30 is generally from %to 1 inch radially. This relatively large shroud gap 30 permits undesirable turbulent airflows to occur about the fan blade tips. These flow conditions have been schematically depicted in FlG. 3.
The flow indicated as 32 is the desirable flow which provides useful heat exchanger cooling air. Flow path 38, indicated as a torous pattern in the shroud gap 30, and flow 39, depicted as a localized flow at each blade tip, are undesirable. They produce no useful cooling air movement, cause fan noise, and create losses in fan efficiency.
In FIG. 4, the preferred embodiment flow conditions are schematically illustrated. It is readily apparent that any recirculating flow 38 in the shroud gap 30 will have to follow a twisted or tortuous path because of the labyrinth seal formed by the flange 24 and the sealing member 18. The tortured nature of the shroud gap greatly increases the paths resistance to fluid flow and consequently reduces the amount of recirculating air. By reducing the recirculating air 38, the amount of desirable flow 32 is increased and the noise caused by the recirculating air 38 is reduced. Additional benefits are achieved since the clearance between the fan blades and the rotating shroud is extremely small, thereby essentially eliminating flow 39. However, the rotating shroud 18 could be spaced somewhat from the blade 16.
In the preferred embodiment it has been determined that the best results are achieved when the tips of the sealing member 18 and the flange 24 are either in alignment as shown in FIG. 4 or if the flange enters the bight of the U as shown in FlG. 5. Some benefit of this invention may be realized when the flange 24 is outside of the bight of the sealing member 18 (FIG. 6) but tests have shown that the benefits are reduced.
The benefits of increased useful airflow, reduced noise generation, and reduced horsepower requirements are realized by developing a labyrinth seal in the shroud gap and by minimizing the localized flow over each blade tip. These two actions coupled with the barrier effect which prevents the interaction between the remaining, though greatly reduced, toroidal recirculation in the shroud gap and flow circulation over the fan tips affords the advantages noted. There are any number of configurations which would achieve this goal. FIGS. 7-9 schematically illustrate three possible configurations. Many more could be used. The embodiment discussed is preferred because of the strength requirements in vehicular systems with high rotational speeds. In low speed applications other constructions may be preferred. Many other designs can be utilized without departing from the scope and spirit of the invention as is set forth in the appended claims.
What is claimed is:
1. In an automotive cooling system the combination comprising:
a heat exchanger and an automotive engine mounted for both axial and radial movement with respect to each other;
a fan rotatably mounted to said engine and having a plurality of blades and including sealing means for creating a labyrinth seal; and
a shroud mounted to said heat exchanger and encircling said fan, said shroud having means for coacting with said sealing means on said fan to form a labyrinth seal in the gap between said shroud and said fan;
said means on said fan and said shroud which form said labyrinth seal being disposed such that relative axial and radial movement therebetween does not interfere with the rotation of said fan.
2. The system set forth in claim 1 wherein said sealing means is a U-shaped hoop circumferentially disposed about said fan blades and said coacting means is an inwardly turned flange on said shroud.
3. The system set forth in claim 2 wherein the tip of said flange is substantially aligned with the tips of said U-shaped sealing means.
4. The system set forth in claim 2 wherein the tip of said flange is disposed within the bight of said U-shaped sealing means.
5. In an automotive cooling system the combination comprising:
a radiator and an automotive engine mounted for movement with respect to each other;
a fan rotatably mounted to said engine and having a pluarlity of blades and including a substantially U- shaped hoop disposed about the perimeter of said blades for creating a labyrinth seal; and
a shroud mounted to said heat exchanger and encircling said fan, said shroud having an inwardly depending flange entering the bight of said hoop for coacting with said hoop to form a labyrinth seal in the gap between said shroud and said fan;
said hoop and said flange which form said labyrinth seal being disposed such that relative axial and radial movement therebetween does not interfere with the rotation of said fan.

Claims (5)

1. In an automotive cooling system the combination comprising: a heat exchanger and an automotive engine mounted for both axial and radial movement with respect to each other; a fan rotatably mounted to said engine and having a plurality of blades and including sealing means for creating a labyrinth seal; and a shroud mounted to said heat exchanger and encircling said fan, said shroud having means for coacting with said sealing means on said fan to form a labyrinth seal in the gap between said shroud and said fan; said means on said fan and said shroud which form said labyrinth seal being disposed such that relative axial and radial movement therebetween does not interfere with the rotation of said fan.
2. The system set forth in claim 1 wherein said sealing means is a U-shaped hoop circumferentially disposed about said fan blades and said coacting means is an inwardly turned flange on said shroud.
3. The system set forth in claim 2 wherein the tip of said flange is substantially aligned with the tips of said U-shaped sealing means.
4. The system set forth in claim 2 wherein the tip of said flange is disposed within the bight of said U-shaped sealing means.
5. In an automotive cooling system the combination comprising: a radiator and an automotive engine mounted for movement with respect to each other; a fan rotatably mounted to said engine and having a pluarlity of blades and including a substantially U-shaped hoop disposed about the perimeter of said blades for creating a labyrinth seal; and a shroud mounted to said heat exchanger and encircling said fan, said shroud having an inwardly depending flange entering the bight of said hoop for coacting with said hoop to form a labyrinth seal in the gap between said shroud and said fan; said hoop and said flange which form said labyrinth seal being disposed such that relative axial and radial movement therebetween does not interfere with the rotation of said fan.
US00376692A 1973-07-05 1973-07-05 Labyrinthian fan Expired - Lifetime US3842902A (en)

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US20120244000A1 (en) * 2009-09-29 2012-09-27 Sylvain Turcas Propeller, Engine Cooling Device Comprising Such A Propeller, And Mould For Producing Said Propeller
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USD860427S1 (en) 2017-09-18 2019-09-17 Horton, Inc. Ring fan
US11142038B2 (en) * 2017-12-18 2021-10-12 Carrier Corporation Labyrinth seal for fan assembly

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US20100229810A1 (en) * 2009-03-10 2010-09-16 Uwe Blass Cooling apparatus for a motor vehicle
US8573931B2 (en) * 2009-03-10 2013-11-05 Behr Gmbh & Co. Kg Cooling apparatus for a motor vehicle
US9790954B2 (en) * 2009-09-29 2017-10-17 Valeo Systemes Thermiques Propeller, engine cooling device comprising such a propeller, and mould for producing said propeller
US20120244000A1 (en) * 2009-09-29 2012-09-27 Sylvain Turcas Propeller, Engine Cooling Device Comprising Such A Propeller, And Mould For Producing Said Propeller
EP3626974A1 (en) * 2010-10-27 2020-03-25 LG Electronics Inc. Air conditioner with outdoor unit
US20120108161A1 (en) * 2010-10-27 2012-05-03 Lg Electronics Inc. Air conditioner with outdoor unit
US9228591B2 (en) * 2010-10-27 2016-01-05 Lg Electronics Inc. Air conditioner with outdoor unit
US20150211541A1 (en) * 2012-09-12 2015-07-30 Soler & Palau Research, S.L. Coupling between a centrifugal fan and the suction inlet thereof
US20150176860A1 (en) * 2013-12-19 2015-06-25 Smiths Medical Asd, Inc. Low noise air circulation device
US20170051834A1 (en) * 2015-08-18 2017-02-23 Rolls-Royce Plc Sealing arrangements
CN110050127A (en) * 2016-12-15 2019-07-23 大金工业株式会社 Pressure fan and refrigerating plant with pressure fan
EP3557077A4 (en) * 2016-12-15 2019-12-04 Daikin Industries, Ltd. BLOWER AND REFRIGERATION DEVICE COMPRISING A BLOWER
US10955146B2 (en) 2016-12-15 2021-03-23 Daikin Industries, Ltd. Fan and refrigeration apparatus including fan
US20180306207A1 (en) * 2017-04-24 2018-10-25 Asia Components Co., Ltd. Fan structure
US10808726B2 (en) * 2017-04-24 2020-10-20 Asia Vital Components Co., Ltd. Fan structure
USD860427S1 (en) 2017-09-18 2019-09-17 Horton, Inc. Ring fan
US11142038B2 (en) * 2017-12-18 2021-10-12 Carrier Corporation Labyrinth seal for fan assembly

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