US20110014052A1 - Fan with structural support ring - Google Patents
Fan with structural support ring Download PDFInfo
- Publication number
- US20110014052A1 US20110014052A1 US12/678,140 US67814008A US2011014052A1 US 20110014052 A1 US20110014052 A1 US 20110014052A1 US 67814008 A US67814008 A US 67814008A US 2011014052 A1 US2011014052 A1 US 2011014052A1
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- United States
- Prior art keywords
- fan
- blades
- fan assembly
- ring
- blade
- 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
Links
- 239000004033 plastic Substances 0.000 claims abstract description 10
- 238000002347 injection Methods 0.000 claims abstract description 3
- 239000007924 injection Substances 0.000 claims abstract description 3
- 239000000463 material Substances 0.000 claims description 13
- 239000002184 metal Substances 0.000 claims description 8
- 238000004519 manufacturing process Methods 0.000 claims description 6
- 238000001746 injection moulding Methods 0.000 claims description 4
- 239000004677 Nylon Substances 0.000 claims description 3
- 239000011521 glass Substances 0.000 claims description 3
- 229920001778 nylon Polymers 0.000 claims description 3
- 238000001816 cooling Methods 0.000 abstract description 25
- 238000000034 method Methods 0.000 description 6
- 238000000465 moulding Methods 0.000 description 6
- 239000002861 polymer material Substances 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000007246 mechanism Effects 0.000 description 2
- 229920000642 polymer Polymers 0.000 description 2
- 239000004743 Polypropylene Substances 0.000 description 1
- 230000001154 acute effect Effects 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 239000002826 coolant Substances 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000010137 moulding (plastic) Methods 0.000 description 1
- -1 polypropylene Polymers 0.000 description 1
- 229920001155 polypropylene Polymers 0.000 description 1
- 230000001737 promoting effect Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 239000011342 resin composition Substances 0.000 description 1
Images
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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/325—Rotors specially for elastic fluids for axial flow pumps for axial flow fans
-
- 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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/325—Rotors specially for elastic fluids for axial flow pumps for axial flow fans
- F04D29/326—Rotors specially for elastic fluids for axial flow pumps for axial flow fans comprising a rotating shroud
-
- 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
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/34—Blade mountings
-
- 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
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/666—Combating 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
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
- F01P11/00—Component parts, details, or accessories not provided for in, or of interest apart from, groups F01P1/00 - F01P9/00
- F01P11/12—Filtering, cooling, or silencing cooling-air
Definitions
- the present invention relates to cooling fans and more particularly to fans used in cooling systems for vehicles and industrial applications.
- the present invention relates to cooling fans such as fans used in connection with an automobile or industrial cooling system. More specifically, the invention pertains to fans with integral blades formed in a molding process, such as an injection molding procedure.
- an engine-driven cooling fan is utilized to force air across a coolant radiator.
- the fan is driven through a belt-drive mechanism connected to the engine crankshaft.
- a typical cooling fan includes a plurality of blades mounted to a central hub member.
- the hub member can be configured to provide a rotary connection to the belt drive mechanism, for example.
- the size and number of fan blades is determined by the cooling requirements for the particular application. For instance, a small automotive fan may only require four blades having a diameter of only 9′′ (229 mm). In larger applications, a greater number of blades are required. In one typical heavy-duty automotive application, nine blades are included in the fan design, the blades having an outer diameter of 28′′ (711 mm).
- the cooling capacity of a particular fan is also governed by the airflow volume that can be generated by the fan at its operating speed. This airflow volume is dependent upon the particular blade geometry, such as the blade area and curvature or profile, and the rotational speed of the fan.
- cooling fan designs incorporate a ring around the circumference of the fan. Specifically, the blade tips are attached to the ring, which provides stability to the blade tips. The ring also helps reduce vortex shedding at the blade tip, particularly when the ring is combined with a U-shaped shroud that follows the circumference of the ring.
- the ring fan design therefore, eliminates some of the structural difficulties encountered with prior unsupported cooling fan configurations.
- the nominal operating conditions for these fans has been increased to again push the envelope of the ring fan's capability.
- the mass inertia of the circumferential ring increases the centrifugal force exerted on the blade-ring interface causing potential failures.
- the weakest point on molded ring fans is along the outer ring between the blade tips, again limiting the life of the fans.
- the present invention contemplates an engine driven cooling fan for use in an engine cooling system, in which the fan has a structural support ring.
- the fan includes a central hub and a plurality of fan blades projecting radially outwardly from the hub, each of the blades having a blade root connected to the hub and a blade tip at an opposite end thereof. Each of the blades further defines a loading edge at an inlet side of the fan and a trailing edge at an outlet side of the fan.
- the cooling fan also includes an annular support ring positioned on the blades between their roots and tips.
- the support ring provides support and stiffness to the fan blades similar to that provided by ring fans which have circumferential rings connected to the blade tips.
- the fan with a mid-type support ring in accordance with the present invention provides a stronger integral structure for the fan and blades, and also improves the strength of the molded materials.
- the invention further provides a cooling fan, particularly for large vehicles and heavy duty industrial applications, which can be manufactured in less expensive and uncomplex basic injection molded techniques.
- FIG. 1 is a perspective view of a fan in accordance with one embodiment of the present invention.
- FIG. 2 is a side view of the fan depicted in FIG. 1 .
- FIG. 3 is a front view of the fan depicted in FIG. 1 .
- FIG. 4 is a cross-sectional view of the fan depicted in FIG. 1 .
- FIG. 5 is a rear view of the fan depicted in FIG. 1 .
- FIGS. 6-9 depict an alternate embodiment of the invention, with FIG. 6 being a perspective view, FIG. 7 being a front view, FIG. 8 being a cross-sectional view, and FIG. 9 being a rear view.
- One-piece molded fans eliminate the welds and rivets commonly associated with prior metal fans.
- the plastic molding process facilitates the generation of smooth rounded contours, which reduce internal stresses within the fan structure.
- the present invention provides an improved one-piece molded fan structure with improved strength and molding characteristics.
- the fan structure eliminates an outer ring and its associated molding, manufacturing and durability issues, such as weld lines on the outer ring between the blade tips.
- the present invention provides a rigid and strong fan structure with an integral structure and excellent air flow characteristics.
- FIGS. 1-5 A preferred embodiment of the invention is shown in FIGS. 1-5 .
- FIG. 1 is a perspective view of the fan embodiment, while FIGS. 3 and 5 are front and rear elevational views.
- FIG. 2 is a side view and FIG. 4 is a cross-sectional view.
- the new fan structure is referred to by the reference number 10 .
- the fan structure 10 includes a number of blades 15 mounted on a central hub member 20 .
- the hub member preferably includes a metal mounting bolt ring 25 which can be insert molded into the fan structure when the fan is manufactured.
- the fan 10 further includes a structural support ring 30 which is positioned on the blades 15 between the roots 15 r of the blades at the hub member 20 and the tips 15 t of the blades.
- the support ring 30 is preferably positioned approximately midway between the roots and tips of the blades. It is understood, however, that the ring can be positioned at other locations on the blades.
- the fan structure 10 is preferably made of a plastic or polymer material and is made by a plastic injection molding process.
- the locations and positioning of the blades, as well as the shape and positioning of the structural ring, preferably allow molding without expensive moveable mold inserts, slides or other complex molding devices.
- the plastic material used for the fan 10 is preferably a nylon material, although it could also be polypropylene or other resin compositions commonly in use today on plastic molded cooling fans for vehicles.
- the material also preferably is a glass-filled material which provides improved strength to the fan structure.
- a 30% glass filled nylon is a preferred type of material for the fan 10 .
- Each of the blades 15 include a front face 16 that is the effective inlet to the fan 10 . Likewise, each blade includes an opposite rear face 17 .
- Each of the blades 15 also can have a swept formed configuration as shown in the drawings.
- the leading edges 18 and trailing edges 19 of each fan blade are curved in the duration or rotation of the fan structure.
- the direction of rotation of the fan structure 10 is indicated by the arrows 100 in FIGS. 3 and 5 .
- the swept forward structure of the fan blades is only used in the preferred embodiments, but is not essential to the invention. Blades without any curved structure or even a reverse curved structure can be utilized in accordance with the present invention, as shown, for example, in FIGS. 6-9 .
- the cross-sections of the blades 15 also are preferably curved as shown to provide air-foil type configurations.
- the curvatures and varying thicknesses of the blades are selected to provide maximum airflow when the fan is operated within its standard rotational speed operational range.
- blades 15 are shown in the embodiment depicted in the drawings. However, the precise number of blades depends on the use and airflow characteristics needed for the cooling application. For example, a fan structure with five, seven or more blades could be utilized within the scope of the present invention.
- the blades 15 do not overlap one another in the axial direction of the fan structure. This allows use of an uncomplex injection molding operation for manufacture of the fans.
- the width W and thickness T of the structural support ring 30 are selected based on the desired use and operation characteristics of the fan structure.
- the width W is preferably less than the overall width OW of the fan structure due to space considerations in the intended use of the fan.
- the thickness T is selected based on the strength needed for the use and operation characteristics of the tan.
- the ring 30 is provided to provide the requisite rigidity and strength of the blades as needed based on the operating conditions for the fan.
- the cross-sectional shape of the structural ring 30 can be flat (as shown in the drawings) or curved in some manner. Many circumferential rings on ring fans are curved or have various shapes to improve the air flow around the outer edges of the fans and the centrally located support ring 30 used with the present invention could also have similar configurations if found to improve the airflow and other operational characteristics of the fan structure 10 .
- junction 40 (or blend region) of the hub member 20 between each pair of adjacent blades also has a rounded or radius curvature, as shown in FIGS. 3 and 5 . This eliminates possible points of weakness in the molded fan structure 10 .
- FIGS. 6-9 illustrate an alternate embodiment 90 of the invention.
- FIG. 6 is a perspective view and shows the hub member 102 , a plurality of fan blade members 104 and a support ring 106 .
- the fan blades are not angled in plan view in the direction of the rotation 110 as with the embodiment described above, although the angle of attack of the fan blades relative to the airflow, as shown in FIG. 6 , is still present.
- the fan blades have a curved cross-sectional shape.
- the fan embodiment 90 is preferably made from a plastic material, similar to the embodiment described above, and also has a metal mounting support ring 120 which is insert molded into the plastic fan material when it is made.
- the fan embodiment 90 is preferably made from a plastic material, similar to the embodiment described above, and also has a metal mounting support ring 120 which is insert molded into the plastic fan material when it is made.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
A cooling fan with an integral structural support ring. The fan has a hub member and a plurality of blades extending therefrom. The fan is a one-piece plastic injection structure. The support ring is positioned between the root and tips of the blades.
Description
- The present invention relates to cooling fans and more particularly to fans used in cooling systems for vehicles and industrial applications.
- The present invention relates to cooling fans such as fans used in connection with an automobile or industrial cooling system. More specifically, the invention pertains to fans with integral blades formed in a molding process, such as an injection molding procedure.
- In most industrial and automotive engine applications, an engine-driven cooling fan is utilized to force air across a coolant radiator. Usually, the fan is driven through a belt-drive mechanism connected to the engine crankshaft.
- A typical cooling fan includes a plurality of blades mounted to a central hub member. The hub member can be configured to provide a rotary connection to the belt drive mechanism, for example. The size and number of fan blades is determined by the cooling requirements for the particular application. For instance, a small automotive fan may only require four blades having a diameter of only 9″ (229 mm). In larger applications, a greater number of blades are required. In one typical heavy-duty automotive application, nine blades are included in the fan design, the blades having an outer diameter of 28″ (711 mm).
- In addition to the number and diameter of blades, the cooling capacity of a particular fan is also governed by the airflow volume that can be generated by the fan at its operating speed. This airflow volume is dependent upon the particular blade geometry, such as the blade area and curvature or profile, and the rotational speed of the fan.
- As the cooling fan dimensions and airflow capacity increase, the loads experienced by the fan, and particularly the blades, also increase. In addition, higher rotational speeds and increased airflow through the fan can lead to deformation or twisting of the blades and significant noise problems. In order to address these problems to some degree, certain cooling fan designs incorporate a ring around the circumference of the fan. Specifically, the blade tips are attached to the ring, which provides stability to the blade tips. The ring also helps reduce vortex shedding at the blade tip, particularly when the ring is combined with a U-shaped shroud that follows the circumference of the ring.
- The ring fan design, therefore, eliminates some of the structural difficulties encountered with prior unsupported cooling fan configurations. However, with the increased strength and improved vibration characteristics provided by the ring fan, the nominal operating conditions for these fans has been increased to again push the envelope of the ring fan's capability. The mass inertia of the circumferential ring increases the centrifugal force exerted on the blade-ring interface causing potential failures. Also, the weakest point on molded ring fans is along the outer ring between the blade tips, again limiting the life of the fans.
- Consequently, a need has again developed for ways to improve cooling airflow capacity of fans, while at the same time increasing their strength. This need becomes particularly acute as the operational rotational speeds of the fan increase to meet the increasing cooling demands for large industrial and automotive engines.
- A need also exists for a fan meeting these requirements, but also is less costly and easy to manufacture.
- To address these needs, the present invention contemplates an engine driven cooling fan for use in an engine cooling system, in which the fan has a structural support ring. The fan includes a central hub and a plurality of fan blades projecting radially outwardly from the hub, each of the blades having a blade root connected to the hub and a blade tip at an opposite end thereof. Each of the blades further defines a loading edge at an inlet side of the fan and a trailing edge at an outlet side of the fan. The cooling fan also includes an annular support ring positioned on the blades between their roots and tips.
- The support ring provides support and stiffness to the fan blades similar to that provided by ring fans which have circumferential rings connected to the blade tips. However, the fan with a mid-type support ring in accordance with the present invention provides a stronger integral structure for the fan and blades, and also improves the strength of the molded materials. The invention further provides a cooling fan, particularly for large vehicles and heavy duty industrial applications, which can be manufactured in less expensive and uncomplex basic injection molded techniques.
- It is an object of the present invention to provide an improved molded fan, particularly for cooling systems for large vehicles and large industrial applications. It is another object of the present invention to provide a cooling fan with improved strength and ease of manufacture.
- It is a still further object of the present invention to provide a fan with a structural support ring for improved material and operational strength, but with the ring positioned between the fan hub and blade tip and not at the blade tips.
- Other objects and benefits of the present invention in its various embodiments will be appreciated upon consideration of the following written description and accompanying figures.
-
FIG. 1 is a perspective view of a fan in accordance with one embodiment of the present invention. -
FIG. 2 is a side view of the fan depicted inFIG. 1 . -
FIG. 3 is a front view of the fan depicted inFIG. 1 . -
FIG. 4 is a cross-sectional view of the fan depicted inFIG. 1 . -
FIG. 5 is a rear view of the fan depicted inFIG. 1 . -
FIGS. 6-9 depict an alternate embodiment of the invention, withFIG. 6 being a perspective view,FIG. 7 being a front view,FIG. 8 being a cross-sectional view, andFIG. 9 being a rear view. - For the purposes of promoting an understanding of the principles of the invention, reference will now be made to the embodiments illustrated in the drawings and specific language will be used to describe the same. It will nevertheless be understood that no limitation as to the scope of the invention is thereby intended. The inventions include any alterations and further modifications in the illustrated devices and described methods and further applications of the principles of the invention which would normally occur to one skilled in the art to which the invention relates.
- In the early designs of cooling fans, metal blades were mounted to a metal hub, which hub was then attached to the fan drive. In recent years, high-strength polymer materials have been used to form various components of the fan. The polymer fan design has been found to be capable of withstanding the normal forces and stresses endured by a cooling fan, including in heavy duty automotive and industrial applications. The use of polymer materials also provides a significant reduction in weight of the cooling fan. Moreover, and perhaps most significantly, the use of polymers generates significant benefits in the manufacture of the fan, since materials of this type readily lend themselves to a variety of common molding processes.
- One-piece molded fans eliminate the welds and rivets commonly associated with prior metal fans. In addition, the plastic molding process facilitates the generation of smooth rounded contours, which reduce internal stresses within the fan structure.
- The present invention provides an improved one-piece molded fan structure with improved strength and molding characteristics. The fan structure eliminates an outer ring and its associated molding, manufacturing and durability issues, such as weld lines on the outer ring between the blade tips. At the same time, the present invention provides a rigid and strong fan structure with an integral structure and excellent air flow characteristics.
- A preferred embodiment of the invention is shown in
FIGS. 1-5 .FIG. 1 is a perspective view of the fan embodiment, whileFIGS. 3 and 5 are front and rear elevational views.FIG. 2 is a side view andFIG. 4 is a cross-sectional view. The new fan structure is referred to by thereference number 10. - The
fan structure 10 includes a number ofblades 15 mounted on acentral hub member 20. The hub member preferably includes a metalmounting bolt ring 25 which can be insert molded into the fan structure when the fan is manufactured. - The
fan 10 further includes astructural support ring 30 which is positioned on theblades 15 between theroots 15 r of the blades at thehub member 20 and thetips 15 t of the blades. Thesupport ring 30 is preferably positioned approximately midway between the roots and tips of the blades. It is understood, however, that the ring can be positioned at other locations on the blades. - As indicated, the
fan structure 10 is preferably made of a plastic or polymer material and is made by a plastic injection molding process. The locations and positioning of the blades, as well as the shape and positioning of the structural ring, preferably allow molding without expensive moveable mold inserts, slides or other complex molding devices. - The plastic material used for the
fan 10 is preferably a nylon material, although it could also be polypropylene or other resin compositions commonly in use today on plastic molded cooling fans for vehicles. The material also preferably is a glass-filled material which provides improved strength to the fan structure. A 30% glass filled nylon is a preferred type of material for thefan 10. - Each of the
blades 15 include afront face 16 that is the effective inlet to thefan 10. Likewise, each blade includes an oppositerear face 17. - Each of the
blades 15 also can have a swept formed configuration as shown in the drawings. The leadingedges 18 and trailingedges 19 of each fan blade are curved in the duration or rotation of the fan structure. In this regard, the direction of rotation of thefan structure 10 is indicated by thearrows 100 inFIGS. 3 and 5 . - The swept forward structure of the fan blades is only used in the preferred embodiments, but is not essential to the invention. Blades without any curved structure or even a reverse curved structure can be utilized in accordance with the present invention, as shown, for example, in
FIGS. 6-9 . - The cross-sections of the
blades 15 also are preferably curved as shown to provide air-foil type configurations. The curvatures and varying thicknesses of the blades are selected to provide maximum airflow when the fan is operated within its standard rotational speed operational range. - Six
blades 15 are shown in the embodiment depicted in the drawings. However, the precise number of blades depends on the use and airflow characteristics needed for the cooling application. For example, a fan structure with five, seven or more blades could be utilized within the scope of the present invention. - Also, as shown in the draw pings, the
blades 15 do not overlap one another in the axial direction of the fan structure. This allows use of an uncomplex injection molding operation for manufacture of the fans. - The width W and thickness T of the structural support ring 30 (see
FIG. 4 ) are selected based on the desired use and operation characteristics of the fan structure. The width W is preferably less than the overall width OW of the fan structure due to space considerations in the intended use of the fan. The thickness T is selected based on the strength needed for the use and operation characteristics of the tan. - The
ring 30 is provided to provide the requisite rigidity and strength of the blades as needed based on the operating conditions for the fan. - The cross-sectional shape of the
structural ring 30 can be flat (as shown in the drawings) or curved in some manner. Many circumferential rings on ring fans are curved or have various shapes to improve the air flow around the outer edges of the fans and the centrally locatedsupport ring 30 used with the present invention could also have similar configurations if found to improve the airflow and other operational characteristics of thefan structure 10. - The junction 40 (or blend region) of the
hub member 20 between each pair of adjacent blades also has a rounded or radius curvature, as shown inFIGS. 3 and 5 . This eliminates possible points of weakness in the moldedfan structure 10. -
FIGS. 6-9 illustrate analternate embodiment 90 of the invention.FIG. 6 is a perspective view and shows thehub member 102, a plurality offan blade members 104 and asupport ring 106. In this embodiment, the fan blades are not angled in plan view in the direction of therotation 110 as with the embodiment described above, although the angle of attack of the fan blades relative to the airflow, as shown inFIG. 6 , is still present. Also as shown inFIG. 6 , the fan blades have a curved cross-sectional shape. - The
fan embodiment 90 is preferably made from a plastic material, similar to the embodiment described above, and also has a metal mountingsupport ring 120 which is insert molded into the plastic fan material when it is made. - The
fan embodiment 90 is preferably made from a plastic material, similar to the embodiment described above, and also has a metal mountingsupport ring 120 which is insert molded into the plastic fan material when it is made. - While preferred embodiments of the present invention have been shown and described herein, numerous variations and alternative embodiments will occur to those skilled in the art. Accordingly, it is intended that the invention is not limited to the preferred embodiments described herein but instead limited to the terms of the appended claims.
Claims (7)
1. A fan assembly comprising:
a central hub member;
a plurality of blades extending outwardly from said hub member, each of said blades having a blade root at the junction with said hub member and a blade tip at the distal end thereof; and
an annular supporting ring member, said ring member being positioned between said blade roots and said blade tips of said blades.
2. The fan assembly as described in claim 1 wherein said ring member is positioned substantially midway between said blade roots and said blade tips of said blades.
3. The fan assembly as described in claim 1 wherein said blades and said ring member are positioned to facilitate ease of manufacture of said fan assembly by an injection molding process without the use of moveable mold slides or insert members.
4. The fan assembly as described in claim 1 wherein said fan assembly is a one-piece plastic injection molded structure.
5. The fan assembly as described claim 1 wherein said fan assembly is made from a glass-filled nylon material.
6. The fan assembly described in claim her comprising a metal mounting bolt ring positioned in said hub member.
7. The fan assembly as described in claim 6 wherein said metal mounting bolt ring is insert molded into said fan assembly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/678,140 US20110014052A1 (en) | 2007-09-13 | 2008-09-13 | Fan with structural support ring |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US97192907P | 2007-09-13 | 2007-09-13 | |
| PCT/US2008/076332 WO2009036403A2 (en) | 2007-09-13 | 2008-09-13 | Fan with structural support ring |
| US12/678,140 US20110014052A1 (en) | 2007-09-13 | 2008-09-13 | Fan with structural support ring |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20110014052A1 true US20110014052A1 (en) | 2011-01-20 |
Family
ID=40452871
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US12/678,140 Abandoned US20110014052A1 (en) | 2007-09-13 | 2008-09-13 | Fan with structural support ring |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US20110014052A1 (en) |
| WO (1) | WO2009036403A2 (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100086405A1 (en) * | 2008-10-08 | 2010-04-08 | Nidec Servo Corporation | Impeller, fan apparatus using the same, and method of manufacturing impeller |
| US20100260608A1 (en) * | 2008-04-18 | 2010-10-14 | Mitsubishi Heavy Industries, Ltd. | Propeller fan |
| US20120244008A1 (en) * | 2011-03-25 | 2012-09-27 | Shun-Chen Chang | Impeller structure |
| US20130170995A1 (en) * | 2012-01-04 | 2013-07-04 | Ming-Ju Chen | Axial flow fan blade structure and axial flow fan thereof |
| WO2017071175A1 (en) * | 2015-10-26 | 2017-05-04 | 杭州微光电子股份有限公司 | Impeller device of outer rotor axial flow fan with heat dissipation structure |
| US11053950B2 (en) | 2018-03-14 | 2021-07-06 | Carrier Corporation | Centrifugal compressor open impeller |
| US20250163929A1 (en) * | 2023-11-20 | 2025-05-22 | Mahle International Gmbh | Method for the production of a shielded impeller, shielded impeller and fan |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IT1404252B1 (en) * | 2011-01-25 | 2013-11-15 | Gate Srl | VENTILATION GROUP, PARTICULARLY FOR A HEAT EXCHANGER FOR A MOTOR VEHICLE |
| ITBO20120042A1 (en) * | 2012-01-31 | 2013-08-01 | Comex Europ S R L | FAN DEVICE |
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| US5399070A (en) * | 1992-07-22 | 1995-03-21 | Valeo Thermique Moteur | Fan hub |
| US20010041138A1 (en) * | 1999-12-23 | 2001-11-15 | Borgwarner, Inc. | Molded cooling fan |
| US20020141871A1 (en) * | 2001-01-30 | 2002-10-03 | Lakshimikantha Medamaranahally | Axial-flow fan having inner and outer blades |
| US6514052B2 (en) * | 2001-03-30 | 2003-02-04 | Emerson Electric Co. | Two sided radial fan for motor cooling |
| US20070128038A1 (en) * | 2005-12-01 | 2007-06-07 | Nett Jonathan M | Engine cooling fan with ring reinforcement |
| US20080056899A1 (en) * | 2006-08-30 | 2008-03-06 | Delta Electronics, Inc. | Fan and impeller thereof |
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| JPS58162299U (en) * | 1982-04-26 | 1983-10-28 | 日産自動車株式会社 | cooling fan |
| GB0229355D0 (en) * | 2002-12-17 | 2003-01-22 | Boc Group Plc | Vacuum pumping arrangement |
| JP4619901B2 (en) * | 2005-08-29 | 2011-01-26 | アイシン化工株式会社 | cooling fan |
-
2008
- 2008-09-13 WO PCT/US2008/076332 patent/WO2009036403A2/en not_active Ceased
- 2008-09-13 US US12/678,140 patent/US20110014052A1/en not_active Abandoned
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5399070A (en) * | 1992-07-22 | 1995-03-21 | Valeo Thermique Moteur | Fan hub |
| US20010041138A1 (en) * | 1999-12-23 | 2001-11-15 | Borgwarner, Inc. | Molded cooling fan |
| US20020141871A1 (en) * | 2001-01-30 | 2002-10-03 | Lakshimikantha Medamaranahally | Axial-flow fan having inner and outer blades |
| US6514052B2 (en) * | 2001-03-30 | 2003-02-04 | Emerson Electric Co. | Two sided radial fan for motor cooling |
| US20070128038A1 (en) * | 2005-12-01 | 2007-06-07 | Nett Jonathan M | Engine cooling fan with ring reinforcement |
| US20080056899A1 (en) * | 2006-08-30 | 2008-03-06 | Delta Electronics, Inc. | Fan and impeller thereof |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20100260608A1 (en) * | 2008-04-18 | 2010-10-14 | Mitsubishi Heavy Industries, Ltd. | Propeller fan |
| US8556587B2 (en) * | 2008-04-18 | 2013-10-15 | Mitsubishi Heavy Industries, Ltd. | Propeller fan |
| US20100086405A1 (en) * | 2008-10-08 | 2010-04-08 | Nidec Servo Corporation | Impeller, fan apparatus using the same, and method of manufacturing impeller |
| US8317478B2 (en) * | 2008-10-08 | 2012-11-27 | Nidec Servo Corporation | Impeller, fan apparatus using the same, and method of manufacturing impeller |
| US20120244008A1 (en) * | 2011-03-25 | 2012-09-27 | Shun-Chen Chang | Impeller structure |
| US20130170995A1 (en) * | 2012-01-04 | 2013-07-04 | Ming-Ju Chen | Axial flow fan blade structure and axial flow fan thereof |
| WO2017071175A1 (en) * | 2015-10-26 | 2017-05-04 | 杭州微光电子股份有限公司 | Impeller device of outer rotor axial flow fan with heat dissipation structure |
| US11053950B2 (en) | 2018-03-14 | 2021-07-06 | Carrier Corporation | Centrifugal compressor open impeller |
| US20250163929A1 (en) * | 2023-11-20 | 2025-05-22 | Mahle International Gmbh | Method for the production of a shielded impeller, shielded impeller and fan |
| US12416314B2 (en) * | 2023-11-20 | 2025-09-16 | Mahle International Gmbh | Method for the production of a shielded impeller, shielded impeller and fan |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2009036403A2 (en) | 2009-03-19 |
| WO2009036403A3 (en) | 2009-05-22 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |