Fan

Information

  • Patent Grant
  • 8764412
  • Patent Number
    8,764,412
  • Date Filed
    Wednesday, February 27, 2013
    11 years ago
  • Date Issued
    Tuesday, July 1, 2014
    10 years ago
Abstract
A fan assembly for creating an air current includes a bladeless fan assembly including a nozzle and a device for creating an air flow through the nozzle. The nozzle includes an interior passage and a mouth receiving the air flow from the interior passage. A Coanda surface located adjacent the mouth and over which the mouth is arranged to direct the air flow. The fan provides an arrangement producing an air current and a flow of cooling air created without requiring a bladed fan, that is, the air flow is created by a bladeless fan.
Description
FIELD OF THE INVENTION

The present invention relates to a fan appliance. Particularly, but not exclusively, the present invention relates to a domestic fan, such as a desk fan, for creating air circulation and air current in a room, in an office or other domestic environment.


BACKGROUND OF THE INVENTION

A number of types of domestic fan are known. It is common for a conventional fan to include a single set of blades or vanes mounted for rotation about an axis, and driving apparatus mounted about the axis for rotating the set of blades. Domestic fans are available in a variety of sizes and diameters, for example, a ceiling fan can be at least 1 m in diameter and is usually mounted in a suspended manner from the ceiling and positioned to provide a downward flow of air and cooling throughout a room.


Desk fans, on the other hand, are often around 30 cm in diameter and are usually free standing and portable. In standard desk fan arrangements the single set of blades is positioned close to the user and the rotation of the fan blades provides a forward flow of air current in a room or into a part of a room, and towards the user. Other types of fan can be attached to the floor or mounted on a wall. The movement and circulation of the air creates a so called ‘wind chill’ or breeze and, as a result, the user experiences a cooling effect as heat is dissipated through convection and evaporation. Fans such as that disclosed in U.S. D 103,476 are suitable for standing on a desk or a table. U.S. Pat. No. 2,620,127 discloses a dual purpose fan suitable for use either mounted in a window or as a portable desk fan.


In a domestic environment it is desirable for appliances to be as small and compact as possible. U.S. Pat. No. 1,767,060 describes a desk fan with an oscillating function that aims to provide an air circulation equivalent to two or more prior art fans. In a domestic environment it is undesirable for parts to project from the appliance, or for the user to be able to touch any moving parts of the fan, such as the blades. U.S. D 103,476 includes a cage around the blades. Other types of fan or circulator are described in U.S. Pat. No. 2,488,467, U.S. Pat. No. 2,433,795 and JP 56-167897. The fan of U.S. Pat. No. 2,433,795 has spiral slots in a rotating shroud instead of fan blades.


Some of the above prior art arrangements have safety features such as a cage or shroud around the blades to protect a user from injuring himself on the moving parts of the fan. However, caged blade parts can be difficult to clean and the movement of blades through air can be noisy and disruptive in a home or office environment.


A disadvantage of certain of the prior art arrangements is that the air flow produced by the fan is not felt uniformly by the user due to variations across the blade surface or across the outward facing surface of the fan. Uneven or ‘choppy’ air flow can be felt as a series of pulses or blasts of air. A further disadvantage is that the cooling effect created by the fan diminishes with distance from the user. This means the fan must be placed in close proximity to the user in order for the user to receive the benefit of the fan.


Locating fans such as those described above close to a user is not always possible as the bulky shape and structure mean that the fan occupies a significant amount of the user's work space area. In the particular case of a fan placed on, or close to, a desk the fan body reduces the area available for paperwork, a computer or other office equipment. The shape and structure of a fan at a desk not only reduces the working area available to a user but can block natural light (or light from artificial sources) from reaching the desk area. A well lit desk area is desirable for close work and for reading. In addition, a well lit area can reduce eye strain and the related health problems that may result from prolonged periods working in reduced light levels.


SUMMARY OF THE INVENTION

The present invention seeks to provide an improved fan assembly which obviates disadvantages of the prior art. It is an object of the present invention to provide a fan assembly which, in use, generates air flow at an even rate over the emission output area of the fan. It is another object to provide an improved fan assembly whereby a user at a distance from the fan feels an improved air flow and cooling effect in comparison to prior art fans.


According to the invention, there is provided a bladeless fan assembly for creating an air current, the fan assembly comprising a nozzle and means for creating an air flow through the nozzle, the nozzle comprising an interior passage, a mouth for receiving the air flow from the interior passage, and a Coanda surface located adjacent the mouth and over which the mouth is arranged to direct the air flow.


Advantageously, by this arrangement an air current is generated and a cooling effect is created without requiring a bladed fan. The bladeless arrangement leads to lower noise emissions due to the absence of the sound of a fan blade moving through the air, and a reduction in moving parts and complexity.


In the following description of fans and, in particular a fan of the preferred embodiment, the term ‘bladeless’ is used to describe apparatus in which air flow is emitted or projected forwards from the fan assembly without the use of blades. By this definition a bladeless fan assembly can be considered to have an output area or emission zone absent blades or vanes from which the air flow is released or emitted in a direction appropriate for the user. A bladeless fan assembly may be supplied with a primary source of air from a variety of sources or generating means such as pumps, generators, motors or other fluid transfer devices, which include rotating devices such as a motor rotor and a bladed impeller for generating air flow. The supply of air generated by the motor causes a flow of air to pass from the room space or environment outside the fan assembly through the interior passage to the nozzle and then out through the mouth.


Hence, the description of a fan assembly as bladeless is not intended to extend to the description of the power source and components such as motors that are required for secondary fan functions. Examples of secondary fan functions can include lighting, adjustment and oscillation of the fan.


The bladeless fan assembly achieves the output and cooling effect described above with a nozzle which includes a Coanda surface to provide an amplifying region utilising the Coanda effect. A Coanda surface is a known type of surface over which fluid flow exiting an output orifice close to the surface exhibits the Coanda effect. The fluid tends to flow over the surface closely, almost ‘clinging to’ or ‘hugging’ the surface. The Coanda effect is already a proven, well documented method of entrainment whereby a primary air flow is directed over the Coanda surface. A description of the features of a Coanda surface, and the effect of fluid flow over a Coanda surface, can be found in articles such as Reba, Scientific American, Volume 214, June 1963 pages 84 to 92.


Preferably the nozzle defines an opening through which air from outside the fan assembly is drawn by the air flow directed over the Coanda surface. Air from the external environment is drawn through the opening by the air flow directed over the Coanda surface. Advantageously, by this arrangement the assembly can be produced and manufactured with a reduced number of parts than those required in prior art fans. This reduces manufacturing cost and complexity.


In the present invention an air flow is created through the nozzle of the fan assembly. In the following description this air flow will be referred to as primary air flow. The primary air flow exits the nozzle via the mouth and passes over the Coanda surface. The primary air flow entrains the air surrounding the mouth of the nozzle, which acts as an air amplifier to supply both the primary air flow and the entrained air to the user. The entrained air will be referred to here as a secondary air flow. The secondary air flow is drawn from the room space, region or external environment surrounding the mouth of the nozzle and, by displacement, from other regions around the fan assembly. The primary air flow directed over the Coanda surface combined with the secondary air flow entrained by the air amplifier gives a total air flow emitted or projected forward to a user from the opening defined by the nozzle. The total air flow is sufficient for the fan assembly to create an air current suitable for cooling.


The air current delivered by the fan assembly to the user has the benefit of being an air flow with low turbulence and with a more linear air flow profile than that provided by other prior art devices. Linear air flow with low turbulence travels efficiently out from the point of emission and loses less energy and less velocity to turbulence than the air flow generated by prior art fans. An advantage for a user is that the cooling effect can be felt even at a distance and the overall efficiency of the fan increases. This means that the user can choose to site the fan some distance from a work area or desk and still be able to feel the cooling benefit of the fan.


Advantageously, the assembly results in the entrainment of air surrounding the mouth of the nozzle such that the primary air flow is amplified by at least 15%, whilst a smooth overall output is maintained. The entrainment and amplification features of the fan assembly result in a fan with a higher efficiency than prior art devices. The air current emitted from the opening defined by the nozzle has an approximately flat velocity profile across the diameter of the nozzle. Overall the flow rate and profile can be described as plug flow with some regions having a laminar or partial laminar flow.


Preferably the nozzle comprises a loop. The shape of the nozzle is not constrained by the requirement to include space for a bladed fan. In a preferred embodiment the nozzle is annular. By providing an annular nozzle the fan can potentially reach a broad area. In a further preferred embodiment the nozzle is at least partially circular. This arrangement can provide a variety of design options for the fan, increasing the choice available to a user or customer.


Preferably, the interior passage is continuous. This allows smooth, unimpeded air flow within the nozzle and reduces frictional losses and noise. In this arrangement the nozzle can be manufactured as a single piece, reducing the complexity of the fan assembly and thereby reducing manufacturing costs.


It is preferred that the mouth is substantially annular. By providing a substantially annular mouth the total air flow can be emitted towards a user over a broad area. Advantageously, an illumination source in the room or at the desk fan location or natural light can reach the user through the central opening.


Preferably, the mouth is concentric with the interior passage. This arrangement will be visually appealing and the concentric location of the mouth with the passage facilitates manufacture. Preferably, the Coanda surface extends symmetrically about an axis. More preferably, the angle subtended between the Coanda surface and the axis is in the range from 7° to 20°, preferably around 15°. This provides an efficient primary air flow over the Coanda surface and leads to maximum air entrainment and secondary air flow.


Preferably the nozzle extends by a distance of at least 5 cm in the direction of the axis. Preferably the nozzle extends about the axis in the shape of a loop and preferably by a distance in the range from 30 cm to 180 cm. This provides options for emission of air over a range of different output areas and opening sizes, such as may be suitable for cooling the upper body and face of a user when working at a desk, for example. In the preferred embodiment the nozzle comprises a diffuser located downstream of the Coanda surface. An angular arrangement of the diffuser surface and an aerofoil-type shaping of the nozzle and diffuser surface can enhance the amplification properties of the fan assembly whilst minimising noise and frictional losses.


In a preferred arrangement the nozzle comprises at least one wall defining the interior passage and the mouth, and the at least one wall comprises opposing surfaces defining the mouth. Preferably, the mouth has an outlet, and the spacing between the opposing surfaces at the outlet of the mouth is in the range from 1 mm to 5 mm, more preferably around 1.3 mm. By this arrangement a nozzle can be provided with the desired flow properties to guide the primary air flow over the Coanda surface and provide a relatively uniform, or close to uniform, total air flow reaching the user.


In the preferred fan arrangement the means for creating an air flow through the nozzle comprises an impeller driven by a motor. This arrangement provides a fan with efficient air flow generation. More preferably the means for creating an air flow comprises a DC brushless motor and a mixed flow impeller. This arrangement reduces frictional losses from motor brushes and also reduces carbon debris from the brushes in a traditional motor. Reducing carbon debris and emissions is advantageous in a clean or pollutant sensitive environment such as a hospital or around those with allergies.


The nozzle may be rotatable or pivotable relative to a base portion, or other portion, of the fan assembly. This enables the nozzle to be directed towards or away from a user as required. The fan assembly may be desk, floor, wall or ceiling mountable. This can increase the portion of a room over which the user experiences cooling.





BRIEF DESCRIPTION OF THE DRAWINGS

An embodiment of the invention will now be described with reference to the accompanying drawings, in which:



FIG. 1 is a front view of a fan assembly;



FIG. 2 is a perspective view of a portion of the fan assembly of FIG. 1;



FIG. 3 is a side sectional view through a portion of the fan assembly of FIG. 1 taken at line A-A;



FIG. 4 is an enlarged side sectional detail of a portion of the fan assembly of FIG. 1; and



FIG. 5 is a sectional view of the fan assembly taken along line B-B of FIG. 3 and viewed from direction F of FIG. 3.





DETAILED DESCRIPTION OF THE INVENTION


FIG. 1 shows an example of a fan assembly 100 viewed from the front of the device. The fan assembly 100 comprises an annular nozzle 1 defining a central opening 2. With reference also to FIGS. 2 and 3, nozzle 1 comprises an interior passage 10, a mouth 12 and a Coanda surface 14 adjacent the mouth 12. The Coanda surface 14 is arranged so that a primary air flow exiting the mouth 12 and directed over the Coanda surface 14 is amplified by the Coanda effect. The nozzle 1 is connected to, and supported by, a base 16 having an outer casing 18. The base 16 includes a plurality of selection buttons 20 accessible through the outer casing 18 and through which the fan assembly 100 can be operated.



FIGS. 3, 4 and 5 show further specific details of the fan assembly 100. A motor 22 for creating an air flow through the nozzle 1 is located inside the base 16. The base 16 further comprises an air inlet 24 formed in the outer casing 18. A motor housing 26 is located inside the base 16. The motor 22 is supported by the motor housing 26 and held in a secure position by a rubber mount or seal member 28.


In the illustrated embodiment, the motor 22 is a DC brushless motor. An impeller 30 is connected to a rotary shaft extending outwardly from the motor 22, and a diffuser 32 is positioned downstream of the impeller 30. The diffuser 32 comprises a fixed, stationary disc having spiral blades.


An inlet 34 to the impeller 30 communicates with the air inlet 24 formed in the outer casing 18 of the base 16. The outlet 36 of the diffuser 32 and the exhaust from the impeller 30 communicate with hollow passageway portions or ducts located inside the base 16 in order to establish air flow from the impeller 30 to the interior passage 10 of the nozzle 1. The motor 22 is connected to an electrical connection and power supply and is controlled by a controller (not shown). Communication between the controller and the plurality of selection buttons 20 enable a user to operate the fan assembly 100.


The features of the nozzle 1 will now be described with reference to FIGS. 3 and 4. The shape of the nozzle 1 is annular. In this embodiment the nozzle 1 has a diameter of around 350 mm, but the nozzle may have any desired diameter, for example around 300 mm. The interior passage 10 is annular and is formed as a continuous loop or duct within the nozzle 1. The nozzle 1 is formed from at least one wall defining the interior passage 10 and the mouth 12. In this embodiment the nozzle 1 comprises an inner wall 38 and an outer wall 40. In the illustrated embodiment the walls 38, 40 are arranged in a looped or folded shape such that the inner wall 38 and outer wall 40 approach one another. The inner wall 38 and the outer wall 40 together define the mouth 12, and the mouth 12 extends about the axis X. The mouth 12 comprises a tapered region 42 narrowing to an outlet 44. The outlet 44 comprises a gap or spacing formed between the inner wall 38 of the nozzle 1 and the outer wall 40 of the nozzle 1. The spacing between the opposing surfaces of the walls 38, 40 at the outlet 44 of the mouth 12 is chosen to be in the range from 1 mm to 5 mm. The choice of spacing will depend on the desired performance characteristics of the fan. In this embodiment the outlet 44 is around 1.3 mm wide, and the mouth 12 and the outlet 44 are concentric with the interior passage 10.


The mouth 12 is adjacent the Coanda surface 14. The nozzle 1 further comprises a diffuser portion located downstream of the Coanda surface. The diffuser portion includes a diffuser surface 46 to further assist the flow of air current delivered or output from the fan assembly 100. In the example illustrated in FIG. 3 the mouth 12 and the overall arrangement of the nozzle 1 is such that the angle subtended between the Coanda surface 14 and the axis X is around 15°. The angle is chosen for efficient air flow over the Coanda surface 14. The base 16 and the nozzle 1 have a depth in the direction of the axis X. The nozzle 1 extends by a distance of around 5 cm in the direction of the axis. The diffuser surface 46 and the overall profile of the nozzle 1 are based on an aerofoil shape, and in the example shown the diffuser portion extends by a distance of around two thirds the overall depth of the nozzle 1.


The fan assembly 100 described above operates in the following manner. When a user makes a suitable selection from the plurality of buttons 20 to operate or activate the fan assembly 100, a signal or other communication is sent to drive the motor 22. The motor 22 is thus activated and air is drawn into the fan assembly 100 via the air inlet 24. In the preferred embodiment air is drawn in at a rate of approximately 20 to 30 liters per second, preferably around 27 l/s (liters per second). The air passes through the outer casing 18 and along the route illustrated by arrow F of FIG. 3 to the inlet 34 of the impeller 30. The air flow leaving the outlet 36 of the diffuser 32 and the exhaust of the impeller 30 is divided into two air flows that proceed in opposite directions through the interior passage 10. The air flow is constricted as it enters the mouth 12 and is further constricted at the outlet 44 of the mouth 12. The air flow exits through the outlet 44 as a primary air flow.


The output and emission of the primary air flow creates a low pressure area at the air inlet 24 with the effect of drawing additional air into the fan assembly 100. The operation of the fan assembly 100 induces high air flow through the nozzle 1 and out through the opening 2. The primary air flow is directed over the Coanda surface 14 and the diffuser surface 46, and is amplified by the Coanda effect. A secondary air flow is generated by entrainment of air from the external environment, specifically from the region around the outlet 44 and from around the outer edge of the nozzle 1. A portion of the secondary air flow entrained by the primary air flow may also be guided over the diffuser surface 46. This secondary air flow passes through the opening 2, where it combines with the primary air flow to produce a total air flow projected forward from the fan assembly 100 in the region of 500 to 700 l/s.


The combination of entrainment and amplification results in a total air flow from the opening 2 of the fan assembly 100 that is greater than the air flow output from a fan assembly without such a Coanda or amplification surface adjacent the emission area.


The amplification and laminar type of air flow produced results in a sustained flow of air being directed towards a user from the nozzle 1. The flow rate at a distance of up to 3 nozzle diameters (i.e. around 1000 to 1200 mm) from a user is around 400 to 500 l/s. The total air flow has a velocity of around 3 to 4 m/s (meters per second). Higher velocities are achievable by reducing the angle subtended between the Coanda surface 14 and the axis X. A smaller angle results in the total air flow being emitted in a more focussed and directed manner. This type of air flow tends to be emitted at a higher velocity but with a reduced mass flow rate. Conversely, greater mass flow can be achieved by increasing the angle between the Coanda surface and the axis. In this case the velocity of the emitted air flow is reduced but the mass flow generated increases. Thus the performance of the fan assembly can be altered by altering the angle subtended between the Coanda surface and the axis X.


The invention is not limited to the detailed description given above. Variations will be apparent to the person skilled in the art. For example, the fan could be of a different height or diameter. The fan need not be located on a desk, but could be free standing, wall mounted or ceiling mounted. The fan shape could be adapted to suit any kind of situation or location where a cooling flow of air is desired. A portable fan could have a smaller nozzle, say 5 cm in diameter. The means for creating an air flow through the nozzle can be a motor or other air emitting device, such as any air blower or vacuum source that can be used so that the fan assembly can create an air current in a room. Examples include a motor such as an AC induction motor or types of DC brushless motor, but may also comprise any suitable air movement or air transport device such as a pump or other means of providing directed fluid flow to generate and create an air flow. Features of a motor may include a diffuser or a secondary diffuser located downstream of the motor to recover some of the static pressure lost in the motor housing and through the motor.


The outlet of the mouth may be modified. The outlet of the mouth may be widened or narrowed to a variety of spacings to maximise air flow. The Coanda effect may be made to occur over a number of different surfaces, or a number of internal or external designs may be used in combination to achieve the flow and entrainment required.


Other shapes of nozzle are envisaged. For example, a nozzle comprising an oval, or ‘racetrack’ shape, a single strip or line, or block shape could be used. The fan assembly provides access to the central part of the fan as there are no blades. This means that additional features such as lighting or a clock or LCD display could be provided in the opening defined by the nozzle.


Other features could include a pivotable or tiltable base for ease of movement and adjustment of the position of the nozzle for the user.

Claims
  • 1. A bladeless fan assembly for creating an air current, the fan assembly comprising: a nozzle, anda device for creating an air flow through the nozzle, the nozzle comprising an interior passage, located between a first wall and a second wall, wherein a distal end of the first wall overlaps a distal end of the second wall to form, near the distal ends of the first and second walls, a mouth for receiving the air flow from the interior passage,a tapered region, located downstream from the mouth, andan outlet, located downstream of the tapered region, for releasing the air flow from the nozzle, wherein a distance between the first wall and the second wall is greater at the mouth than at the outlet, anda Coanda surface located adjacent the outlet,wherein the first wall is curved proximate to its distal end to direct the air flow over the Coanda surface, andwherein the nozzle is substantially annular, and defines an opening through which air from outside the fan assembly is drawn by the air flow directed over the Coanda surface.
  • 2. The fan assembly of claim 1, wherein the nozzle comprises a loop.
  • 3. The fan assembly of claim 1, wherein the nozzle is at least partially circular.
  • 4. The fan assembly of claim 1, wherein the interior passage is continuous.
  • 5. The fan assembly of claim 1, wherein the interior passage is substantially annular.
  • 6. The fan assembly of claim 1, wherein the mouth is substantially annular.
  • 7. The fan assembly of claim 1, wherein the mouth is concentric with the interior passage.
  • 8. The fan assembly of claim 1, wherein the Coanda surface extends symmetrically about an axis.
  • 9. The fan assembly of claim 8, wherein an angle subtended between the Coanda surface and the axis is in a range from 7° to 20°.
  • 10. The fan assembly of claim 8, wherein the nozzle extends by a distance of at least 5 cm in a direction of the axis.
  • 11. The fan assembly of claim 8, wherein the nozzle extends about the axis by a distance in the range from 30 cm to 180 cm.
  • 12. The fan assembly of claim 1, wherein a spacing between opposing surfaces of the first wall and the second wall at the outlet is in a range from 1 mm to 5 mm.
  • 13. The fan assembly of claim 1, wherein the device for creating the air flow through the nozzle comprises an impeller driven by a motor.
  • 14. The fan assembly of claim 13, wherein the motor is a DC brushless motor and the impeller is a mixed flow impeller.
  • 15. A nozzle for a bladeless fan assembly for creating an air current, the nozzle comprising: an interior passage, located between a first wall and a second wall, wherein a distal end of the first wall overlaps a distal end of the second wall to form, near the distal ends of the first and second walls, a mouth for receiving an air flow from the interior passage,a tapered region, located downstream from the mouth, andan outlet, located downstream of the tapered region, for releasing the air flow from the nozzle, wherein a distance between the first wall and the second wall is greater at the mouth than at the outlet, anda Coanda surface located adjacent the outlet,wherein the first wall is curved proximate to its distal end to direct the air flow over the Coanda surface, andwherein the nozzle is substantially annular, and defines an opening through which air from outside the fan assembly is drawn by the air flow directed over the Coanda surface.
  • 16. The nozzle of claim 15, wherein the nozzle comprises a loop.
  • 17. The nozzle of claim 15, wherein the nozzle is at least partially circular.
  • 18. The nozzle of claim 15, wherein the interior passage is continuous.
  • 19. The nozzle of claim 15, wherein the interior passage is substantially annular.
  • 20. The nozzle of claim 15, wherein the mouth is substantially annular.
Priority Claims (5)
Number Date Country Kind
0717148.1 Sep 2007 GB national
0717151.5 Sep 2007 GB national
0717154.9 Sep 2007 GB national
0717155.6 Sep 2007 GB national
0814835.5 Aug 2008 GB national
REFERENCE TO RELATED APPLICATIONS

This application is a continuation of U.S. patent application Ser. No. 13/114,707, filed May 24, 2011, which is a continuation of U.S. patent application Ser. No. 12/203,698, filed Sep. 3, 2008, now U.S. Pat. No. 8,308,445, issued Nov. 13, 2012, which claims the priority of United Kingdom Application Nos. 0717155.6, 0717148.1, 0717151.5 and 0717154.9, all filed Sep. 4, 2007, and United Kingdom Application No. 0814835.5, filed Aug. 14, 2008, the entire contents of which prior applications are incorporated herein by reference.

US Referenced Citations (235)
Number Name Date Kind
1357261 Svoboda Nov 1920 A
1767060 Ferguson Jun 1930 A
1896869 Larsh Feb 1933 A
2014185 Martin Sep 1935 A
2035733 Wall Mar 1936 A
2071266 Schmidt Feb 1937 A
D103476 Weber Mar 1937 S
2115883 Sher May 1938 A
D115344 Chapman Jun 1939 S
2210458 Keilholtz Aug 1940 A
2258961 Saathoff Oct 1941 A
2295502 Lamb Sep 1942 A
2336295 Reimuller Dec 1943 A
2363839 Demuth Nov 1944 A
2433795 Stokes Dec 1947 A
2473325 Aufiero Jun 1949 A
2476002 Stalker Jul 1949 A
2488467 De Lisio Nov 1949 A
2510132 Morrison Jun 1950 A
2544379 Davenport Mar 1951 A
2547448 Demuth Apr 1951 A
2583374 Hoffman Jan 1952 A
2620127 Radcliffe Dec 1952 A
2765977 Morrison Oct 1956 A
2808198 Morrison Oct 1957 A
2813673 Smith Nov 1957 A
2830779 Wentling Apr 1958 A
2838229 Belanger Jun 1958 A
2922277 Bertin Jan 1960 A
2922570 Allen Jan 1960 A
3004403 Laporte Oct 1961 A
3047208 Coanda Jul 1962 A
3270655 Guirl et al. Sep 1966 A
D206973 De Lisio Feb 1967 S
3503138 Fuchs et al. Mar 1970 A
3518776 Wolff et al. Jul 1970 A
3724092 McCleerey Apr 1973 A
3729934 Denning et al. May 1973 A
3743186 Mocarski Jul 1973 A
3795367 Mocarski Mar 1974 A
3872916 Beck Mar 1975 A
3875745 Franklin Apr 1975 A
3885891 Throndson May 1975 A
3943329 Hlavac Mar 1976 A
4037991 Taylor Jul 1977 A
4046492 Inglis Sep 1977 A
4061188 Beck Dec 1977 A
4073613 Desty Feb 1978 A
4090814 Teodorescu et al. May 1978 A
4113416 Kataoka et al. Sep 1978 A
4136735 Beck et al. Jan 1979 A
4173995 Beck Nov 1979 A
4180130 Beck et al. Dec 1979 A
4184541 Beck et al. Jan 1980 A
4192461 Arborg Mar 1980 A
4332529 Alperin Jun 1982 A
4336017 Desty Jun 1982 A
4342204 Melikian et al. Aug 1982 A
4448354 Reznick et al. May 1984 A
4568243 Schubert et al. Feb 1986 A
4630475 Mizoguchi Dec 1986 A
4643351 Fukamachi et al. Feb 1987 A
4703152 Shih-Chin Oct 1987 A
4718870 Watts Jan 1988 A
4732539 Shin-Chin Mar 1988 A
4734017 Levin Mar 1988 A
4790133 Stuart Dec 1988 A
4850804 Huang Jul 1989 A
4878620 Tarleton Nov 1989 A
4893990 Tomohiro et al. Jan 1990 A
4978281 Conger Dec 1990 A
5061405 Stanek et al. Oct 1991 A
D325435 Coup et al. Apr 1992 S
5110266 Toyoshima et al. May 1992 A
5168722 Brock Dec 1992 A
5176856 Takahashi et al. Jan 1993 A
5188508 Scott et al. Feb 1993 A
5296769 Havens et al. Mar 1994 A
5310313 Chen May 1994 A
5317815 Hwang Jun 1994 A
5402938 Sweeney Apr 1995 A
5407324 Starnes, Jr. et al. Apr 1995 A
5425902 Miller et al. Jun 1995 A
5435489 Jenkins et al. Jul 1995 A
5518370 Wang et al. May 1996 A
5609473 Litvin Mar 1997 A
5645769 Tamaru et al. Jul 1997 A
5649370 Russo Jul 1997 A
5671321 Bagnuolo Sep 1997 A
5735683 Muschelknautz Apr 1998 A
5762034 Foss Jun 1998 A
5762661 Kleinberger et al. Jun 1998 A
5783117 Byassee et al. Jul 1998 A
D398983 Keller et al. Sep 1998 S
5841080 Iida et al. Nov 1998 A
5843344 Junkel et al. Dec 1998 A
5862037 Behl Jan 1999 A
5868197 Potier Feb 1999 A
5881685 Foss et al. Mar 1999 A
D415271 Feer Oct 1999 S
6015274 Bias et al. Jan 2000 A
6073881 Chen Jun 2000 A
D429808 Krauss et al. Aug 2000 S
6123618 Day Sep 2000 A
6155782 Hsu Dec 2000 A
D435899 Melwani Jan 2001 S
6254337 Arnold Jul 2001 B1
6269549 Carlucci et al. Aug 2001 B1
6278248 Hong et al. Aug 2001 B1
6282746 Schleeter Sep 2001 B1
6293121 Labrador Sep 2001 B1
6321034 Jones-Lawlor et al. Nov 2001 B2
6386845 Bedard May 2002 B1
6480672 Rosenzweig et al. Nov 2002 B1
6599088 Stagg Jul 2003 B2
6604694 Kordas et al. Aug 2003 B1
D485895 Melwani Jan 2004 S
6789787 Stutts Sep 2004 B2
6791056 VanOtteren et al. Sep 2004 B2
6830433 Birdsell et al. Dec 2004 B2
7059826 Lasko Jun 2006 B2
7088913 Verhoorn et al. Aug 2006 B1
7147336 Chou Dec 2006 B1
D539414 Russak et al. Mar 2007 S
7192258 Kuo et al. Mar 2007 B2
7412781 Mattinger et al. Aug 2008 B2
7478993 Hong et al. Jan 2009 B2
7540474 Huang et al. Jun 2009 B1
D598532 Dyson et al. Aug 2009 S
D602143 Gammack et al. Oct 2009 S
D602144 Dyson et al. Oct 2009 S
D605748 Gammack et al. Dec 2009 S
7660110 Vinson et al. Feb 2010 B2
7664377 Liao Feb 2010 B2
D614280 Dyson et al. Apr 2010 S
7731050 Parks et al. Jun 2010 B2
7775848 Auerbach Aug 2010 B1
7806388 Junkel et al. Oct 2010 B2
7841045 Shaanan et al. Nov 2010 B2
8002520 Dawson et al. Aug 2011 B2
8092166 Nicolas et al. Jan 2012 B2
8113490 Chen Feb 2012 B2
8152495 Boggess, Jr. et al. Apr 2012 B2
8246317 Gammack Aug 2012 B2
8356804 Fitton et al. Jan 2013 B2
8544826 Ediger et al. Oct 2013 B2
20020106547 Sugawara et al. Aug 2002 A1
20030059307 Moreno et al. Mar 2003 A1
20030164367 Bucher et al. Sep 2003 A1
20030171093 Gumucio Del Pozo Sep 2003 A1
20030190183 Hsing Oct 2003 A1
20040022631 Birdsell et al. Feb 2004 A1
20040049842 Prehodka Mar 2004 A1
20040106370 Honda et al. Jun 2004 A1
20040149881 Allen Aug 2004 A1
20050031448 Lasko et al. Feb 2005 A1
20050053465 Roach et al. Mar 2005 A1
20050069407 Winkler et al. Mar 2005 A1
20050128698 Huang Jun 2005 A1
20050163670 Alleyne et al. Jul 2005 A1
20050173997 Schmid et al. Aug 2005 A1
20050281672 Parker et al. Dec 2005 A1
20060172682 Orr et al. Aug 2006 A1
20060199515 Lasko et al. Sep 2006 A1
20060263073 Clarke et al. Nov 2006 A1
20060279927 Strohm Dec 2006 A1
20070035189 Matsumoto Feb 2007 A1
20070041857 Fleig Feb 2007 A1
20070065280 Fok Mar 2007 A1
20070166160 Russak et al. Jul 2007 A1
20070176502 Kasai et al. Aug 2007 A1
20070224044 Hong et al. Sep 2007 A1
20070269323 Zhou et al. Nov 2007 A1
20080020698 Spaggiari Jan 2008 A1
20080124060 Gao May 2008 A1
20080152482 Patel Jun 2008 A1
20080166224 Giffin Jul 2008 A1
20080286130 Purvines Nov 2008 A1
20080314250 Cowie et al. Dec 2008 A1
20090026850 Fu Jan 2009 A1
20090032130 Dumas et al. Feb 2009 A1
20090039805 Tang Feb 2009 A1
20090060710 Gammack et al. Mar 2009 A1
20090060711 Gammack et al. Mar 2009 A1
20090120925 Lasko May 2009 A1
20090191054 Winkler Jul 2009 A1
20090214341 Craig Aug 2009 A1
20100150699 Nicolas et al. Jun 2010 A1
20100162011 Min Jun 2010 A1
20100171465 Seal et al. Jul 2010 A1
20100225012 Fitton et al. Sep 2010 A1
20100226749 Gammack et al. Sep 2010 A1
20100226750 Gammack Sep 2010 A1
20100226751 Gammack et al. Sep 2010 A1
20100226752 Gammack et al. Sep 2010 A1
20100226753 Dyson et al. Sep 2010 A1
20100226754 Hutton et al. Sep 2010 A1
20100226758 Cookson et al. Sep 2010 A1
20100226763 Gammack et al. Sep 2010 A1
20100226764 Gammack et al. Sep 2010 A1
20100226769 Helps Sep 2010 A1
20100226771 Crawford et al. Sep 2010 A1
20100226787 Gammack et al. Sep 2010 A1
20100226797 Fitton et al. Sep 2010 A1
20100226801 Gammack Sep 2010 A1
20100254800 Fitton et al. Oct 2010 A1
20110058935 Gammack et al. Mar 2011 A1
20110110805 Gammack et al. May 2011 A1
20110164959 Fitton et al. Jul 2011 A1
20110223014 Crawford et al. Sep 2011 A1
20110223015 Gammack et al. Sep 2011 A1
20120031509 Wallace et al. Feb 2012 A1
20120033952 Wallace et al. Feb 2012 A1
20120034108 Wallace et al. Feb 2012 A1
20120039705 Gammack Feb 2012 A1
20120045315 Gammack Feb 2012 A1
20120045316 Gammack Feb 2012 A1
20120057959 Hodgson et al. Mar 2012 A1
20120082561 Gammack et al. Apr 2012 A1
20120093629 Fitton et al. Apr 2012 A1
20120093630 Fitton et al. Apr 2012 A1
20120114513 Simmonds et al. May 2012 A1
20120230658 Fitton et al. Sep 2012 A1
20120308375 Gammack Dec 2012 A1
20130026664 Staniforth et al. Jan 2013 A1
20130028763 Staniforth et al. Jan 2013 A1
20130028766 Staniforth et al. Jan 2013 A1
20130129490 Dos Reis et al. May 2013 A1
20130161842 Fitton et al. Jun 2013 A1
20130199372 Nock et al. Aug 2013 A1
20130272858 Stickney et al. Oct 2013 A1
20130280051 Nicolas et al. Oct 2013 A1
20130280061 Stickney Oct 2013 A1
20130280096 Gammack et al. Oct 2013 A1
20130323100 Poulton et al. Dec 2013 A1
Foreign Referenced Citations (221)
Number Date Country
560119 Aug 1957 BE
1055344 May 1979 CA
2155482 Sep 1996 CA
346643 May 1960 CH
2085866 Oct 1991 CN
2111392 Jul 1992 CN
1437300 Aug 2003 CN
2650005 Oct 2004 CN
2713643 Jul 2005 CN
1680727 Oct 2005 CN
2833197 Nov 2006 CN
201180678 Jan 2009 CN
201221477 Apr 2009 CN
201281416 Jul 2009 CN
201349269 Nov 2009 CN
201486901 May 2010 CN
101749288 Jun 2010 CN
201502549 Jun 2010 CN
101825103 Sep 2010 CN
201568337 Sep 2010 CN
101936310 Jan 2011 CN
201696365 Jan 2011 CN
201739199 Feb 2011 CN
101984299 Mar 2011 CN
101985948 Mar 2011 CN
201763705 Mar 2011 CN
201763706 Mar 2011 CN
201770513 Mar 2011 CN
201779080 Mar 2011 CN
201802648 Apr 2011 CN
102095236 Jun 2011 CN
201874901 Jun 2011 CN
201917047 Aug 2011 CN
102251973 Nov 2011 CN
102367813 Mar 2012 CN
1 291 090 Mar 1969 DE
24 51 557 May 1976 DE
27 48 724 May 1978 DE
3644567 Jul 1988 DE
195 10 397 Sep 1996 DE
197 12 228 Oct 1998 DE
100 00 400 Mar 2001 DE
10041805 Jun 2002 DE
10 2009 007 Aug 2010 DE
0 044 494 Jan 1982 EP
0186581 Jul 1986 EP
0 784 947 Jul 1997 EP
1 094 224 Apr 2001 EP
1 138 954 Oct 2001 EP
1357296 Oct 2003 EP
1 779 745 May 2007 EP
1 939 456 Jul 2008 EP
1 980 432 Oct 2008 EP
2 000 675 Dec 2008 EP
2191142 Jun 2010 EP
1033034 Jul 1953 FR
1119439 Jun 1956 FR
1.387.334 Jan 1965 FR
2 375 471 Jul 1978 FR
2 534 983 Apr 1984 FR
2 640 857 Jun 1990 FR
2 658 593 Aug 1991 FR
2794195 Dec 2000 FR
2 874 409 Feb 2006 FR
2 906 980 Apr 2008 FR
2928706 Sep 2009 FR
22235 Jun 1914 GB
383498 Nov 1932 GB
593828 Oct 1947 GB
601222 Apr 1948 GB
633273 Dec 1949 GB
641622 Aug 1950 GB
661747 Nov 1951 GB
863 124 Mar 1961 GB
1067956 May 1967 GB
1 262 131 Feb 1972 GB
1 265 341 Mar 1972 GB
1 278 606 Jun 1972 GB
1 304 560 Jan 1973 GB
1 403 188 Aug 1975 GB
1 434 226 May 1976 GB
1 501 473 Feb 1978 GB
2 094 400 Sep 1982 GB
2 107 787 May 1983 GB
2 111 125 Jun 1983 GB
2 178 256 Feb 1987 GB
2 185 531 Jul 1987 GB
2 185 533 Jul 1987 GB
2 218 196 Nov 1989 GB
2 236 804 Apr 1991 GB
2 240 268 Jul 1991 GB
2 242 935 Oct 1991 GB
2 285 504 Jul 1995 GB
2 289 087 Nov 1995 GB
2383277 Jun 2003 GB
2 428 569 Feb 2007 GB
2 452 593 Mar 2009 GB
2452490 Mar 2009 GB
2463698 Mar 2010 GB
2464736 Apr 2010 GB
2466058 Jun 2010 GB
2468312 Sep 2010 GB
2468313 Sep 2010 GB
2468315 Sep 2010 GB
2468317 Sep 2010 GB
2468319 Sep 2010 GB
2468320 Sep 2010 GB
2468323 Sep 2010 GB
2468328 Sep 2010 GB
2468331 Sep 2010 GB
2468369 Sep 2010 GB
2468498 Sep 2010 GB
2473037 Mar 2011 GB
2479760 Oct 2011 GB
2482547 Feb 2012 GB
2484695 Apr 2012 GB
2493231 Jan 2013 GB
2493505 Feb 2013 GB
2493507 Feb 2013 GB
31-13055 Aug 1956 JP
35-4369 Mar 1960 JP
39-7297 Mar 1964 JP
49-150403 Dec 1974 JP
51-7258 Jan 1976 JP
53-60100 May 1978 JP
56-167897 Dec 1981 JP
57-71000 May 1982 JP
57-157097 Sep 1982 JP
61-31830 Feb 1986 JP
61-116093 Jun 1986 JP
61-280787 Dec 1986 JP
62-223494 Oct 1987 JP
63-179198 Jul 1988 JP
63-306340 Dec 1988 JP
64-21300 Feb 1989 JP
64-83884 Mar 1989 JP
1-138399 May 1989 JP
1-224598 Sep 1989 JP
2-146294 Jun 1990 JP
2-218890 Aug 1990 JP
2-248690 Oct 1990 JP
3-52515 May 1991 JP
3-267598 Nov 1991 JP
4-43895 Feb 1992 JP
4-366330 Dec 1992 JP
5-157093 Jun 1993 JP
5-164089 Jun 1993 JP
5-263786 Oct 1993 JP
6-74190 Mar 1994 JP
6-86898 Mar 1994 JP
6-147188 May 1994 JP
6-257591 Sep 1994 JP
6-280800 Oct 1994 JP
6-336113 Dec 1994 JP
7-190443 Jul 1995 JP
8-21400 Jan 1996 JP
9-100800 Apr 1997 JP
9-178083 Jul 1997 JP
9-287600 Nov 1997 JP
11-502586 Mar 1999 JP
11-227866 Aug 1999 JP
2000-116179 Apr 2000 JP
2000-201723 Jul 2000 JP
2001-17358 Jan 2001 JP
2002-21797 Jan 2002 JP
2002-138829 May 2002 JP
2002-213388 Jul 2002 JP
2003-329273 Nov 2003 JP
2004-8275 Jan 2004 JP
2004-208935 Jul 2004 JP
2004-216221 Aug 2004 JP
2005-201507 Jul 2005 JP
2005-307985 Nov 2005 JP
2006-089096 Apr 2006 JP
3127331 Nov 2006 JP
2007-138763 Jun 2007 JP
2007-138789 Jun 2007 JP
2008-39316 Feb 2008 JP
2008-100204 May 2008 JP
3146538 Oct 2008 JP
2008-294243 Dec 2008 JP
2009-44568 Feb 2009 JP
2009-62986 Mar 2009 JP
2010-131259 Jun 2010 JP
2010-203764 Sep 2010 JP
2012-31806 Feb 2012 JP
1999-002660 Jan 1999 KR
10-2005-0102317 Oct 2005 KR
2007-0007997 Jan 2007 KR
20-0448319 Mar 2010 KR
10-2010-0055611 May 2010 KR
10-0985378 Sep 2010 KR
M399207 Mar 2001 TW
517825 Jan 2003 TW
589932 Jun 2004 TW
M394383 Dec 2010 TW
M407299 Jul 2011 TW
WO-9013478 Nov 1990 WO
WO-9506822 Mar 1995 WO
WO-02073096 Sep 2002 WO
WO-03058795 Jul 2003 WO
WO-03069931 Aug 2003 WO
WO-2005050026 Jun 2005 WO
WO 2005057091 Jun 2005 WO
WO-2006008021 Jan 2006 WO
WO-2006012526 Feb 2006 WO
WO-2007024955 Mar 2007 WO
WO-2007048205 May 2007 WO
WO-2008014641 Feb 2008 WO
WO-2008024569 Feb 2008 WO
WO-2008139491 Nov 2008 WO
WO-2009030879 Mar 2009 WO
WO-2009030881 Mar 2009 WO
WO-2010100449 Sep 2010 WO
WO-2010100451 Sep 2010 WO
WO-2010100452 Sep 2010 WO
WO-2010100453 Sep 2010 WO
WO-2010100462 Sep 2010 WO
WO-2012006882 Jan 2012 WO
WO-2012033517 Mar 2012 WO
WO-2013014419 Jan 2013 WO
Non-Patent Literature Citations (41)
Entry
Gammack et al., U.S. Office Action mailed Sep. 6, 2013, directed to U.S. Appl. No. 12/716,740; 15 pages.
Gammack et al., Office Action mailed Sep. 27, 2013, directed to U.S. Appl. No. 13/588,666; 10 pages.
Wallace et al., Office Action mailed Oct. 23, 2013, directed to U.S. Appl. No. 13/192,223; 18 pages.
Fitton et al., U.S. Office Action mailed Dec. 31, 2013, directed to U.S. Appl. No. 13/718,693; 8 pages.
Gammack et al., Office Action mailed Jun. 12, 2013, directed towards U.S. Appl. No. 12/945,558; 20 pages.
Gammack et al., Office Action mailed May 29, 2013, directed towards U.S. Appl. No. 13/588,666; 11 pages.
Wallace et al., Office Action mailed Jun. 7, 2013, directed towards U.S. Appl. No. 13/192,223; 30 pages.
Gammack et al., U.S. Office Action mailed Feb. 28, 2013, directed to U.S. Appl. No. 12/945,558; 16 pages.
Gammack et al., U.S. Office Action mailed Feb. 14, 2013, directed to U.S. Appl. No. 12/716,515; 21 pages.
Gammack et al., U.S. Office Action mailed Mar. 14, 2013, directed to U.S. Appl. No. 12/716,740; 15 pages.
Gammack, P. et al., Office Action mailed Aug. 19, 2013, directed to U.S. Appl. No. 12/716,515; 20 pages.
GB Search Report directed to related application GB0717151.5 mailed on Dec. 17, 2007; 2 pages.476.
GB Search Report directed to related application GB0717155.6 mailed on Dec. 19, 2007; 2 pages.
GB Search Report directed to related application GB0717154.9 mailed on Dec. 17, 2007; 2 pages.
GB Search Report directed to related application GB0717148.1 mailed on Dec. 20, 2007; 1 page.
International Search Report and Written Opinion mailed Oct. 29, 2008, directed to International Application No. PCT/GB2008/002891; 11 pages.
International Search Report and Written Opinion mailed Oct. 31, 2008, directed to International Application No. PCT/GB2008/002874; 12 pages.
Gammack, P. et al., U.S. Office Action mailed Dec. 9, 2010, directed to U.S. Appl. No. 12/203,698; 10 pages.
Gammack, P. et al., U.S. Office Action mailed Jun. 21, 2011, directed to U.S. Appl. No. 12/203,698; 11 pages.
Gammack et al., Office Action mailed Sep. 17, 2012, directed to U.S. Appl. No. 13/114,707; 12 pages.
Gammack, P. et al., U.S. Office Action mailed Dec. 10, 2010, directed to U.S. Appl. No. 12/230,613; 12 pages.
Gammack, P. et al., U.S. Office Action mailed May 13, 2011, directed to U.S. Appl. No. 12/230,613; 13 pages.
Gammack, P. et al., U.S. Office Action mailed Sep. 7, 2011, directed to U.S. Appl. No. 12/230,613; 15 pages.
Gammack, P. et al., U.S. Office Action mailed Jun. 8, 2012, directed to U.S. Appl. No. 12/230,613; 15 pages.
Gammack et al., U.S. Office Action mailed Aug. 20, 2012, directed to U.S. Appl. No. 12/945,558; 15 pages.
Fitton et al., U.S. Office Action mailed Nov. 30, 2010 directed to U.S. Appl. No. 12/560,232; 9 pages.
Nicolas, F. et al., U.S. Office Action mailed Mar. 7, 2011, directed to U.S. Appl. No. 12/622,844; 10 pages.
Nicolas, F. et al., U.S. Office Action mailed Sep. 8, 2011, directed to U.S. Appl. No. 12/622,844; 11 pages.
Helps, D. F. et al., U.S. Office Action mailed Feb. 15, 2013, directed to U.S. Appl. No. 12/716,694; 12 pages.
Fitton, et al., U.S. Office Action mailed Mar. 8, 2011, directed to U.S. Appl. No. 12/716,780; 12 pages.
Fitton, et al., U.S. Office Action mailed Sep. 6, 2011, directed to U.S. Appl. No. 12/716,780; 16 pages.
Gammack, P. et al., U.S. Office Action mailed Dec. 9, 2010, directed to U.S. Appl. No. 12/716,781; 17 pages.
Gammack, P. et al., U.S. Final Office Action mailed Jun. 24, 2011, directed to U.S. Appl. No. 12/716,781; 19 pages.
Gammack, P. et al., U.S. Office Action mailed Apr. 12, 2011, directed to U.S. Appl. No. 12/716,749; 8 pages.
Gammack, P. et al., U.S. Office Action mailed Sep. 1, 2011, directed to U.S. Appl. No. 12/716,749; 9 pages.
Gammack, P. et al., U.S. Office Action mailed Jun. 25, 2012, directed to U.S. Appl. No. 12/716,749; 11 pages.
Fitton et al., U.S. Office Action mailed Mar. 30, 2012, directed to U.S. Appl. No. 12/716,707; 7 pages.
Gammack, P. et al., U.S. Office Action mailed May 24, 2011, directed to U.S. Appl. No. 12/716,613; 9 pages.
Gammack, P. et al. U.S. Office Action mailed Oct. 18, 2012, directed to U.S. Appl. No. 12/917,247; pages.
Reba, I. (1966). “Applications of the Coanda Effect,” Scientific American 214:84-92.
Third Party Submission Under 37 CFR 1.99 filed Jun. 2, 2011, directed towards U.S. Appl. No. 12/203,698; 3 pages.
Related Publications (1)
Number Date Country
20140079566 A1 Mar 2014 US
Continuations (2)
Number Date Country
Parent 13114707 May 2011 US
Child 13779285 US
Parent 12203698 Sep 2008 US
Child 13114707 US