Fan

Information

  • Patent Grant
  • 9328739
  • Patent Number
    9,328,739
  • Date Filed
    Thursday, January 17, 2013
    12 years ago
  • Date Issued
    Tuesday, May 3, 2016
    8 years ago
Abstract
A fan includes an outer casing having an air inlet and an air outlet, and an impeller housing located within the casing. An impeller is provided within the impeller housing for generating an air flow along a path extending from the air inlet to the air outlet through the impeller housing. A motor for driving the impeller is located within a motor housing connected to the impeller housing. A foam annular seal is located between the impeller housing and a seat to inhibit the leakage of air between the impeller housing and the casing. A plurality of resilient supports is provided between the impeller housing and the seat to reduce the load on the annular seal.
Description
REFERENCE TO RELATED APPLICATIONS

This application claims the priority of United Kingdom Application No. 1200899.1, filed Jan. 19, 2012, the entire contents of which are incorporated herein by reference.


FIELD OF THE INVENTION

The present invention relates to a fan. Particularly, but not exclusively, the present invention relates to a floor or table-top fan, such as a desk, tower or pedestal fan.


BACKGROUND OF THE INVENTION

A conventional domestic fan typically includes a set of blades or vanes mounted for rotation about an axis, and drive apparatus for rotating the set of blades to generate an air flow. The movement and circulation of the air flow creates a ‘wind chill’ or breeze and, as a result, the user experiences a cooling effect as heat is dissipated through convection and evaporation. The blades are generated located within a cage which allows an air flow to pass through the housing while preventing users from coming into contact with the rotating blades during use of the fan.


WO 2009/030879 describes a fan assembly which does not use caged blades to project air from the fan assembly. Instead, the fan assembly comprises a cylindrical base which houses a motor-driven impeller for drawing a primary air flow into the base, and an annular nozzle connected to the base and comprising an annular air outlet through which the primary air flow is emitted from the fan. The nozzle defines a central opening through which air in the local environment of the fan assembly is drawn by the primary air flow emitted from the mouth, amplifying the primary air flow.


WO 2010/100452 also describes such a fan assembly. Within the base, the impeller is located within an impeller housing, and the motor for driving the impeller is located within a motor bucket which is mounted on the impeller housing. The impeller housing is supported within the base by a plurality of angularly spaced supports. Each support is, in turn, mounted on a respective support surface extending radially inwardly from the inner surface of the base. In order to provide an air tight seal between the impeller housing and the base, a lip seal is located on an external side surface of the impeller housing for engaging the internal side surface of the base.


SUMMARY OF THE INVENTION

The present invention provides a fan comprising a casing having an air inlet and an air outlet, an impeller housing mounted on an annular seat located within the casing, an impeller located within the impeller housing for generating an air flow along a path extending from the air inlet to the air outlet through the impeller housing, a motor housing connected to the impeller housing, a motor located within the motor housing for driving the impeller, an annular seal in sealing engagement with the impeller housing and the seat, and at least one resilient support located between the impeller housing and the seat for reducing the compressive load applied to the annular seal.


The fan assembly thus comprises both an annular seal and at least one resilient support located between the impeller housing and a seat upon which the impeller housing is mounted. The compression of the annular seal between the impeller housing and the seat forms an air tight seal which prevents air from leaking back towards the air inlet of the casing along a path extending between the casing and the impeller housing, and so forces the pressurized air flow generated by the impeller to pass to the air outlet of the casing.


The annular seal is preferably a foam annular seal. Forming the annular seal from a foam material, as opposed to an elastomeric or rubber material, can reduce the transmission of vibrations to the casing through the annular seal. The resilient support(s) are also disposed between the impeller housing and the seat so as to bear some of the combined weight of the impeller housing, impeller, motor housing and motor, and thereby reduce the compressive load acting on the annular seal. This reduces the extent of the deformation of the annular seal; an excessive compression of the annular seal between the impeller housing and the seat could result in an undesirable increase in the transmission of the vibrations from the motor housing to the casing through the annular seal.


The compressive force acting on the annular seal is preferably aligned with the direction of the greatest stiffness of the surface from which the vibrations are to be isolated, that is, the casing of the fan. In a preferred embodiment, this direction is parallel to the longitudinal axis of the casing. The annular seal is preferably spaced from the inner surface of the casing so that vibrations are not transferred radially outwardly from the annular seal to the casing.


In addition to forming an air-tight seal between the impeller housing and the casing, the annular seal can also provide a damping action for reducing the vibration of the resilient support(s) during use of the fan assembly, and so reduce the transmission of the vibrations from the motor housing to the casing through the resilient support(s).


The annular seal is preferably formed from material which exhibits no more than 0.01 MPa of stress at 10% compression. In a preferred embodiment, the annular seal is formed from a closed cell foam material. The foam material is preferably formed from a synthetic rubber, such as EPDM (ethylene propylene diene monomer) rubber.


The impeller housing may be provided with a recessed section defining an annular channel for receiving the seal. The recessed section of the impeller housing preferably comprises a seal engaging surface, for example a flange, which extends radially outwardly from the impeller housing and generally parallel to the seat, and which is in sealing engagement with the seal.


The fan may comprise means for inhibiting rotation of the seal relative to the impeller housing. External peripheries of both the recessed section of the impeller housing and the seal may be non-circular or otherwise shaped to inhibit rotation of the seal within the annular channel. For example, the external peripheries of both the recessed section of the impeller housing and the seal may be scalloped. Alternatively, or additionally, the seat may comprise means for inhibiting rotation of the seal relative to the impeller housing.


The resilient support(s) preferably extend about the annular seal. The fan may comprise a single, annular resilient support. Alternatively, the fan may comprise a plurality of resilient supports. The resilient supports are preferably angularly spaced about the impeller housing. To reduce the width of the casing, the internal or external periphery of the annular seal may be scalloped or otherwise profiled to form a plurality of recesses each for at least partially accommodating a respective resilient support. Alternatively, the annular seal may be provided with a plurality of apertures, with each resilient support extending through a respective aperture.


The, or each resilient support may comprise a respective spring. Alternatively, each resilient support may be formed from an elastomeric material. For example, a single annular resilient support may be provided in the form of a bellows support arranged about the impeller housing. Where the fan comprises a plurality of resilient supports, each support may comprise a rod or shaft formed from rubber or other resilient or elastomeric material.


The fan preferably comprises means for inhibiting angular movement of the impeller housing, that is, about the rotational axis of the impeller, relative to the seat. For example, the fan may comprise means for inhibiting angular movement of the resilient support(s) relative to the seat. The seat may be provided with one or more stop members for engaging the resilient support(s) to prevent movement of the resilient support(s) along the seat. The stop members may be in the form of raised or recessed portions of the seat. The fan may also comprise means for inhibiting angular movement of the resilient support(s) relative to the impeller housing. For example, the impeller housing may comprise one or more stop members for engaging the resilient support(s) to prevent movement of the resilient support(s) along the impeller housing. Where the fan comprises a plurality of resilient supports, the impeller housing may comprise a plurality of mounts each connected to a respective resilient support.


The seat may be connected to an upper end of a base of the fan so as to be located within the casing. However, the seat is preferably connected to the casing. The seat preferably extends radially inwardly from a side wall of the casing.





BRIEF DESCRIPTION OF THE DRAWINGS

Preferred features of the invention will now be described, by way of example only, with reference to the accompanying drawings, in which:



FIG. 1 is a front view of a fan;



FIG. 2 is a front perspective view, from above, of the air outlet of the fan;



FIG. 3 is a side sectional view of the body of the fan;



FIG. 4 is an exploded view, from below, of an impeller housing, an annular seal and resilient supports of the lower part of the fan; and



FIG. 5 is an exploded view, from above, of the same components of the fan as illustrated in FIG. 4, and a lower part of the main body section of the body of the casing.





DETAILED DESCRIPTION OF THE INVENTION


FIG. 1 is a front view of a fan 10. The fan comprises a body 12 having an air inlet 14 in the form of a plurality of apertures formed in the outer casing 16 of the body 12, and through which a primary air flow is drawn into the body 12 from the external environment. An annular nozzle 18 having an air outlet 20 for emitting the primary air flow from the fan 10 is connected to the body 12. The body 12 further comprises a user interface for allowing a user to control the operation of the fan 10. The user interface comprises a plurality of user-operable buttons 22, 24 and a user-operable dial 26.


As also shown in FIG. 2, the nozzle 18 comprises an annular outer casing section 28 connected to and extending about an annular inner casing section 30. The annular sections 28, 30 of the nozzle 18 extend about and define an opening 32. Each of these sections may be formed from a plurality of connected parts, but in this embodiment each of the outer casing section 28 and the inner casing section 30 is formed from a respective, single moulded part. During assembly, the outer casing section 28 is inserted into a slot located at the front of the inner casing section 30, as illustrated in FIGS. 3 and 4. The outer and inner casing sections 28, 30 may be connected together using an adhesive introduced to the slot. The outer casing section 28 comprises a base 34 which is connected to the open upper end of the outer casing 16 of the body 12, and which has an open lower end for receiving the primary air flow from the body 12.


The outer casing section 28 and the inner casing section 30 together define an annular interior passage for conveying the primary air flow to the air outlet 20. The interior passage is bounded by the internal surface of the outer casing section 28 and the internal surface of the inner casing section 30. The base 34 of the outer casing section 28 is shaped to convey the primary air flow into the interior passage of the nozzle 18.


The air outlet 20 is located towards the rear of the nozzle 18, and is arranged to emit the primary air flow towards the front of the fan 10, through the opening 32. The air outlet 20 extends at least partially about the opening 32, and preferably surrounds the opening 32. The air outlet 20 is defined by overlapping, or facing, portions of the internal surface of the outer casing section 28 and the external surface of the inner casing section 30, respectively, and is in the form of an annular slot, preferably having a relatively constant width in the range from 0.5 to 5 mm. In this example the air outlet has a width of around 1 mm. Spacers may be spaced about the air outlet 20 for urging apart the overlapping portions of the outer casing section 28 and the inner casing section 30 to maintain the width of the air outlet 20 at the desired level. These spacers may be integral with either the outer casing section 28 or the inner casing section 30.


The air outlet 20 is shaped to direct the primary air flow over the external surface of the inner casing section 30. The external surface of the inner casing section 30 comprises a Coanda surface 36 located adjacent the air outlet 20 and over which the air outlet 20 directs the air emitted from the fan 10, a diffuser surface 38 located downstream of the Coanda surface 36 and a guide surface 40 located downstream of the diffuser surface 38. The diffuser surface 38 is arranged to taper away from the central axis X of the opening 32 in such a way so as to assist the flow of air emitted from the fan 10. The angle subtended between the diffuser surface 38 and the central axis X of the opening 32 is in the range from 5 to 25°, and in this example is around 15°. The guide surface 40 is arranged at an angle to the diffuser surface 38 to further assist the efficient delivery of a cooling air flow from the fan 10. The guide surface 40 is preferably arranged substantially parallel to the central axis X of the opening 32 to present a substantially flat and substantially smooth face to the air flow emitted from the air outlet 20. A visually appealing tapered surface 42 is located downstream from the guide surface 40, terminating at a tip surface 44 lying substantially perpendicular to the central axis X of the opening 32. The angle subtended between the tapered surface 42 and the central axis X of the opening 32 is preferably around 45°.



FIG. 3 illustrates a side sectional view through the body 12 of the fan 10. The body 12 comprises a substantially cylindrical main body section 50 mounted on a substantially cylindrical lower body section 52. The main body section 50 and the lower body section 52 are preferably formed from plastics material. The main body section 50 and the lower body section 52 preferably have substantially the same external diameter so that the external surface of the main body section 50 is substantially flush with the external surface of the lower body section 52.


The main body section 50 comprises the air inlet 14 through which the primary air flow enters the fan assembly 10. In this embodiment the air inlet 14 comprises an array of apertures formed in the main body section 50. Alternatively, the air inlet 14 may comprise one or more grilles or meshes mounted within windows formed in the main body section 50. The main body section 50 is open at the upper end (as illustrated) thereof to provide an air outlet 54 through which the primary air flow is exhausted from the body 12 to the nozzle 18.


The main body section 50 may be tilted relative to the lower body section 52 to adjust the direction in which the primary air flow is emitted from the fan assembly 10. For example, the upper surface of the lower body section 52 and the lower surface of the main body section 50 may be provided with interconnecting features which allow the main body section 50 to move relative to the lower body section 52 while preventing the main body section 50 from being lifted from the lower body section 52. For example, the lower body section 52 and the main body section 50 may comprise interlocking L-shaped members.


The lower body section 52 is mounted on a base 56 for engaging a surface on which the fan assembly 10 is located. The lower body section 52 comprises the aforementioned user interface and a control circuit, indicated generally at 58, for controlling various functions of the fan 10 in response to operation of the user interface. The lower body section 52 also houses a mechanism for oscillating the lower body section 52 relative to the base 56. The operation of the oscillation mechanism is controlled by the control circuit 58 in response to the user's depression of the button 24 of the user interface. The range of each oscillation cycle of the lower body section 52 relative to the base 56 is preferably between 60° and 120°, and the oscillation mechanism is arranged to perform around 3 to 5 oscillation cycles per minute. A mains power cable (not shown) for supplying electrical power to the fan 10 extends through an aperture formed in the base 56.


The main body section 50 houses an impeller 60 for drawing the primary air flow through the air inlet 14 and into the body 12. The impeller 60 is connected to a rotary shaft 62 extending outwardly from a motor 64. In this embodiment, the motor 64 is a DC brushless motor having a speed which is variable by the control circuit 58 in response to user manipulation of the dial 26. The maximum speed of the motor 64 is preferably in the range from 5,000 to 10,000 rpm.


The motor 64 is housed within a motor housing. The motor housing comprises a lower section 66 which supports the motor 64, and an upper section 68 connected to the lower section 66. The shaft 62 protrudes through an aperture formed in the lower section 66 of the motor housing to allow the impeller to be connected to the shaft 62. The motor 64 is inserted into the lower section 66 of the motor housing before the upper section 68 is connected to the lower section 66. The upper section 68 comprises an annular diffuser 70 having a plurality of blades for receiving the primary air flow exhausted from the impeller 64 and for guiding the air flow to the air outlet 54 of the main body section 50. A shroud 72 is connected to the outer edges of the blades of the impeller 60.


The motor housing is supported within the main body section 50 by an impeller housing 74. The impeller housing 74 is generally frusto-conical in shape, and comprises an air inlet 76 at the relatively small, outwardly flared lower end thereof (as illustrated) for receiving the primary air flow, and an air outlet 78 at the relatively large, upper end thereof (as illustrated) which is located immediately upstream from the diffuser 72 when the motor housing is supported within the impeller housing 74. The impeller 60, the shroud 72 and the impeller housing 74 are shaped so that when the impeller 60 is supported by the impeller housing 74, the shroud 72 is in close proximity to, but does not contact, the inner surface of the impeller housing 74, and the impeller 60 is substantially co-axial with the impeller housing 74.


An annular inlet member 80 guides an air flow from the air inlet 14 of the outer casing 16 to the air inlet 76 of the impeller housing 74. A disc-shaped foam silencing member 82 is located within the main body section 50, beneath the air inlet 76 of the impeller housing 74. An annular foam silencing member 84 is located within the motor housing.


With reference also to FIGS. 4 and 5, the impeller housing 74 is located within the main body section 50 so that the rotational axis of the impeller 60 is substantially co-linear with the longitudinal axis of the main body section 50. The impeller housing 74 is mounted on an annular seat 86 located within the main body section 50. The seat 86 extends radially inwardly from the inner surface of the main body section 50 so that an upper surface of the seat 86 is substantially orthogonal to the rotational axis of the impeller 60.


An annular seal 88 is located between the impeller housing 74 and the seat 86. The annular seal 88 is preferably a foam annular seal, and is preferably formed from a closed cell foam material. In this example, the annular seal 88 is formed from EPDM (ethylene propylene diene monomer) rubber, but the annular seal 88 may be formed from other closed cell foam material which preferably exhibits no more than 0.01 MPa of stress at 10% compression. The outer diameter of the annular seal 88 is preferably smaller than the inner diameter of the main body section 50, so that the annular seal 88 is spaced from the inner surface of the main body section 50.


The annular seal 88 has a lower surface which is in sealing engagement with the upper surface of the seat 86, and an upper surface which is in sealing engagement with the impeller housing 74. In this example, the impeller housing 74 comprises a recessed seal engaging section 90 extending about an outer wall of the impeller housing. The seal engaging section 90 of the impeller housing 74 comprises a flange 92 which defines an annular channel 94 for receiving the annular seal 88. The flange 92 extends radially outwardly from the outer surface of the impeller housing 74 so that a lower surface of the flange 92 is substantially orthogonal to the rotational axis of the impeller 60. The internal periphery of a circumferential lip 96 of the flange 92 and the external periphery of the annular seal 88 are preferably scalloped or otherwise shaped to define a plurality of recesses 98, 100 to inhibit relative rotation between the impeller housing 74 and the annular seal 88.


The seat 86 comprises an aperture 102 to enable a cable (not shown) to pass from the control circuit 58 to the motor 64. Each of the flange 92 of the impeller housing 74 and the annular seal 88 is shaped to define a respective recess 104, 106 to accommodate part of the cable. One or more grommets or other sealing members may be provided about the cable to inhibit the leakage of air through the aperture 102, and between the recesses 104, 106 and the internal surface of the main body section 50.


A plurality of resilient supports 108 are also provided between the impeller housing 74 and the seat 86 for bearing part of the weight of the motor 64, motor housing, impeller 60 and impeller housing 74. The resilient supports 108 are equally spaced from, and equally spaced about, the longitudinal axis of the main body section 50. Each resilient support 108 has a first end which is connected to a respective mount 110 located on the flange 92 of the impeller housing 74, and a second end which is received within a recess 112 formed in the seat 86 to inhibit movement of the resilient support 108 along the seat 86 and about the longitudinal axis of the main body section 50. In this example, each resilient support 108 comprises a spring 114 which is located over a respective mount 110, and a rubber foot 116 which is located with a respective recess 112. Alternatively, the spring 114 and the foot 116 may be replaced by a rod or shaft formed from rubber or other elastic or elastomeric material. As a further alternative, the plurality of resilient supports 108 may be replaced by a single annular resilient support extending about the annular seal 88. In this example, the external periphery of the annular seal 88 is further scalloped or otherwise shaped to form a plurality of recesses 118 each for at least partially receiving a respective resilient support 88. This allows the resilient supports 88 to be located closer to the longitudinal axis of the main body section 50 without either decreasing the radial thickness of the annular seal 80 or increasing the diameter of the main body section 50.


To operate the fan 10 the user presses button 22 of the user interface, in response to which the control circuit 58 activates the motor 64 to rotate the impeller 60. The rotation of the impeller 60 causes a primary air flow to be drawn into the body 12 through the air inlet 14. The user may control the speed of the motor 64, and therefore the rate at which air is drawn into the body 12 through the air inlet 14, by manipulating the dial 26. Depending on the speed of the motor 64, the primary air flow generated by the impeller 60 may be between 20 and 30 liters per second.


The rotation of the impeller 60 by the motor 64 generates vibrations which are transferred through the motor housing and the impeller housing 74 towards the seat 86. The annular seal 88 located between the impeller housing 74 and the seat 86 is compressed under the weight of the motor housing, motor 64, impeller 60 and impeller housing 74 so that it is in sealing engagement with the upper surface of the seat 86 and the lower surface of the flange 92 of the impeller housing 74. The annular seal 88 thus not only prevents the primary air flow from returning to the air inlet 76 of the impeller housing 74 along a path extending between the inner surface of the main body section 50 and the outer surface of the impeller housing 74, but also reduces the transmission of these vibrations to the seat 86, and thus to the body 12 of the fan 10. The presence of the resilient supports 108 between the impeller housing 74 and the seat 86 inhibits any over-compression of the annular seal 88 over time, which otherwise could increase the transmission of vibrations through the annular seal 88 to the seat 86. The flexibility of the resilient supports 108 allows the resilient supports to flex both axially and radially relative to the seat 86, which reduces the transmission of vibrations to the seat 86 through the resilient supports 88. The annular seal 88 serves to damp the flexing movement of the resilient supports 108 relative to the seat 86.


The primary air flow passes sequentially between the impeller 60 and the impeller housing 74, and through the diffuser 72, before passing through the air outlet 54 of the body 12 and into the nozzle 18. Within the nozzle 18, the primary air flow is divided into two air streams which pass in opposite directions around the opening 32 of the nozzle 18. As the air streams pass through the nozzle 18, air is emitted through the air outlet 20. The primary air flow emitted from the air outlet 20 is directed over the Coanda surface 36 of the nozzle 18, causing a secondary air flow to be generated by the entrainment of air from the external environment, specifically from the region around the air outlet 20 and from around the rear of the nozzle 18. This secondary air flow passes through the central opening 32 of the nozzle 18, where it combines with the primary air flow to produce a total air flow, or air current, projected forward from the nozzle 18.

Claims
  • 1. A fan comprising: a casing having an air inlet and an air outlet;an impeller housing mounted on an annular seat located within the casing, wherein the seat is connected to the casing;an impeller located within the impeller housing for generating an air flow along a path extending from the air inlet to the air outlet through the impeller housing;a motor housing connected to the impeller housing;a motor located within the motor housing for driving the impeller;an annular seal in sealing engagement with the impeller housing and the seat; andat least one resilient support located between the impeller housing and the seat for reducing the compressive load applied to the annular seal.
  • 2. The fan of claim 1, wherein the seat extends radially inwardly from a side wall of the casing.
  • 3. The fan of claim 1, wherein the impeller housing comprises a recessed section defining an annular channel for receiving the seal.
  • 4. The fan of claim 3, wherein the recessed section comprises a seal engaging surface extending radially outwardly from a side wall of the impeller housing and parallel to the seat.
  • 5. The fan of claim 1, wherein a periphery of the impeller housing and a periphery of the seal are shaped to inhibit rotation of the seal relative to the impeller housing.
  • 6. The fan of claim 1, wherein the at least one resilient support comprises a plurality of resilient supports.
  • 7. The fan of claim 6, wherein the resilient supports are angularly spaced about the impeller housing.
  • 8. The fan of claim 6, wherein a peripheral surface of the seal is profiled so as to form a plurality of recesses each for at least partially receiving a respective resilient support.
  • 9. The fan of claim 6, wherein the impeller housing comprises a plurality of mounts each connected to a respective resilient support.
  • 10. The fan of claim 6, wherein the annular seal comprises a plurality of recesses each for receiving a respective resilient support.
  • 11. The fan of claim 6, wherein each resilient support comprises a respective spring.
  • 12. The fan of claim 1, wherein the annular seal is a foam annular seal.
  • 13. The fan of claim 1, wherein the annular seal is formed from a closed cell foam material.
  • 14. The fan of claim 1, wherein the annular seal is spaced from an inner side surface of the casing.
Priority Claims (1)
Number Date Country Kind
1200899.1 Jan 2012 GB national
US Referenced Citations (228)
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
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
2336295 Reimuller Dec 1943 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
3339867 Bayless Sep 1967 A
3444817 Caldwell May 1969 A
3503138 Fuchs et al. Mar 1970 A
3518776 Wolff et al. Jul 1970 A
3724092 McCleerey Apr 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
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
4502837 Blair et al. Mar 1985 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
4790133 Stuart Dec 1988 A
4850804 Huang Jul 1989 A
4878620 Tarleton Nov 1989 A
4893990 Tomohiro et al. Jan 1990 A
4978281 Conger, IV Dec 1990 A
5061405 Stanek et al. Oct 1991 A
D325435 Coup et al. Apr 1992 S
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
5518370 Wang et al. May 1996 A
5609473 Litvin Mar 1997 A
5645769 Tamaru et al. Jul 1997 A
5649370 Russo Jul 1997 A
5730582 Heitmann Mar 1998 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 Junket 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
6065936 Shingai et al. May 2000 A
6073881 Chen Jun 2000 A
6082969 Carroll et al. Jul 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
6338610 Harada et al. Jan 2002 B1
6348106 Embree et al. Feb 2002 B1
6386845 Bedard May 2002 B1
6454527 Nishiyama et al. Sep 2002 B2
6480672 Rosenzweig et al. Nov 2002 B1
6511288 Gatley, Jr. Jan 2003 B1
6599088 Stagg Jul 2003 B2
D485895 Melwani Jan 2004 S
6709236 Hoelzer Mar 2004 B1
6752711 Yeung Jun 2004 B1
6789787 Stutts 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
7186075 Winkler et al. Mar 2007 B2
7189053 Winkler Mar 2007 B2
7241214 Sixsmith Jul 2007 B2
7317267 Schmid et al. Jan 2008 B2
7455504 Hill et al. Nov 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
7664377 Liao Feb 2010 B2
D614280 Dyson et al. Apr 2010 S
7775848 Auerbach Aug 2010 B1
7806388 Junkel et al. Oct 2010 B2
7921962 Liddell Apr 2011 B2
8033783 Ishikawa et al. Oct 2011 B2
8092166 Nicolas et al. Jan 2012 B2
8430624 Cookson et al. Apr 2013 B2
8469658 Gammack et al. Jun 2013 B2
20020015640 Nishiyama et al. Feb 2002 A1
20020106547 Sugawara et al. Aug 2002 A1
20030059307 Moreno et al. Mar 2003 A1
20030171093 Gumucio Del Pozo Sep 2003 A1
20040022631 Birdsell et al. Feb 2004 A1
20040049842 Prehodka Mar 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
20050276684 Huang et al. Dec 2005 A1
20050281672 Parker et al. Dec 2005 A1
20060172682 Orr et al. Aug 2006 A1
20060199515 Lasko et al. Sep 2006 A1
20070035189 Matsumoto Feb 2007 A1
20070041857 Fleig Feb 2007 A1
20070048159 DiMatteo et al. Mar 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
20080152482 Patel Jun 2008 A1
20080166224 Giffin Jul 2008 A1
20080286130 Purvines Nov 2008 A1
20080304986 Kenyon et al. Dec 2008 A1
20080314250 Cowie et al. Dec 2008 A1
20090026850 Fu Jan 2009 A1
20090039805 Tang Feb 2009 A1
20090060710 Gammack et al. Mar 2009 A1
20090060711 Gammack et al. Mar 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
20100219013 Liddell Sep 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
20110002775 Ma et al. Jan 2011 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
20130011252 Crawford et al. Jan 2013 A1
20130045084 Tu et al. Feb 2013 A1
20130302156 Nurzynski Nov 2013 A1
20130309065 Johnson et al. Nov 2013 A1
20130309066 Atkinson et al. Nov 2013 A1
20130309080 Johnson et al. Nov 2013 A1
20130323025 Crawford et al. Dec 2013 A1
20140017069 Peters Jan 2014 A1
Foreign Referenced Citations (223)
Number Date Country
201100923 Sep 2011 AU
560119 Aug 1957 BE
1055344 May 1979 CA
2155482 Sep 1996 CA
346643 May 1960 CH
2085866 Oct 1991 CN
2111392 Jul 1992 CN
2228996 Jun 1996 CN
1232143 Oct 1999 CN
1288506 Mar 2001 CN
1336482 Feb 2002 CN
1437300 Aug 2003 CN
2650005 Oct 2004 CN
2713643 Jul 2005 CN
1680727 Oct 2005 CN
2833197 Nov 2006 CN
101046318 Oct 2007 CN
201180678 Jan 2009 CN
201221477 Apr 2009 CN
201281416 Jul 2009 CN
201349269 Nov 2009 CN
101749288 Jun 2010 CN
201502549 Jun 2010 CN
101816534 Sep 2010 CN
101825095 Sep 2010 CN
101825102 Sep 2010 CN
201568337 Sep 2010 CN
101936310 Jan 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
102305220 Jan 2012 CN
102367813 Mar 2012 CN
202165330 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
41 27 134 Feb 1993 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 007 037 Aug 2010 DE
10 2009 044 349 May 2011 DE
0 044 494 Jan 1982 EP
0186581 Jul 1986 EP
0 837 245 Apr 1998 EP
0 955 469 Nov 1999 EP
1 094 224 Apr 2001 EP
1 138 954 Oct 2001 EP
1 566 548 Aug 2005 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
2 534 983 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
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
2 237 323 May 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
2 452 490 Mar 2009 GB
2 452 593 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
2468319 Sep 2010 GB
2468320 Sep 2010 GB
2468323 Sep 2010 GB
2468328 Sep 2010 GB
2468331 Sep 2010 GB
2468369 Sep 2010 GB
2473037 Mar 2011 GB
2479760 Oct 2011 GB
2482547 Feb 2012 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
53-51608 May 1978 JP
53-60100 May 1978 JP
56-167897 Dec 1981 JP
57-71000 May 1982 JP
57-157097 Sep 1982 JP
59-90797 May 1984 JP
59-167984 Nov 1984 JP
60-105896 Jul 1985 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
3-3419 Jan 1991 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
7-247991 Sep 1995 JP
8-21400 Jan 1996 JP
9-100800 Apr 1997 JP
9-287600 Nov 1997 JP
10-122188 May 1998 JP
11-227866 Aug 1999 JP
2000-116179 Apr 2000 JP
2000-201723 Jul 2000 JP
2001-17358 Jan 2001 JP
2001-295785 Oct 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
2006-89096 Apr 2006 JP
3127331 Nov 2006 JP
2007-92697 Apr 2007 JP
2007-138763 Jun 2007 JP
2007-138789 Jun 2007 JP
2008-39316 Feb 2008 JP
2008-100204 May 2008 JP
2008-151081 Jul 2008 JP
3146538 Oct 2008 JP
2008-294243 Dec 2008 JP
2009-44568 Feb 2009 JP
2009-264121 Nov 2009 JP
2010-131259 Jun 2010 JP
2012-36897 Feb 2012 JP
2012-57619 Mar 2012 JP
2002-0061691 Jul 2002 KR
2002-0067468 Aug 2002 KR
10-2005-0102317 Oct 2005 KR
2007-0007997 Jan 2007 KR
10-2010-0055611 May 2010 KR
2000-0032363 Jun 2010 KR
10-0985378 Sep 2010 KR
M394383 Dec 2010 TW
M407299 Jul 2011 TW
WO-9013478 Nov 1990 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-2009030879 Mar 2009 WO
WO-2009030881 Mar 2009 WO
WO-2010100448 Sep 2010 WO
WO-2010100451 Sep 2010 WO
WO-2010100452 Sep 2010 WO
WO-2010100453 Sep 2010 WO
WO-2010100462 Sep 2010 WO
WO-2011055134 May 2011 WO
Non-Patent Literature Citations (28)
Entry
International Search Report and Written Opinion mailed Oct. 14, 2013, directed to International Application No. PCT/GB2012/053100; 11 pages.
Hodgson et al., U.S. Office Action mailed Mar. 24, 2014, directed to U.S. Appl. No. 13/207,212; 10 pages.
Search Report dated Apr. 26, 2012, directed to GB Application No. 1200899.1, 1 page.
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.
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 Nov. 29, 2012, directed to U.S. Appl. No. 12/716,742; 9 pages.
Cookson, M. et al., U.S. Office Action mailed Dec. 19, 2012, directed to U.S. Appl. No. 12/716,778; 8 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.
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.
Atkinson et al., U.S. Office Action mailed Dec. 17, 2015, directed to U.S. Appl. No. 13/895,691; 11 pages.
Related Publications (1)
Number Date Country
20130189083 A1 Jul 2013 US