This application claims the priority of United Kingdom Application No. 1017551.1 filed Oct. 18, 2010, and United Kingdom Application No. 1105687.6, filed Apr. 4, 2011, the entire contents of which are incorporated herein by reference.
The present invention relates to a fan assembly. Particularly, but not exclusively, the present invention relates to a floor or table-top fan assembly, such as a desk, tower or pedestal fan.
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 generally 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 mouth through which the primary air flow is emitted from the fan. The nozzle defines an 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. The nozzle includes a Coanda surface over which the mouth is arranged to direct the primary air flow. The Coanda surface extends symmetrically about the central axis of the opening so that the air flow generated by the fan assembly is in the form of an annular jet having a cylindrical or frusto-conical profile.
In a first aspect the present invention provides a fan assembly comprising a nozzle and a system for creating a primary air flow through the nozzle. The nozzle comprises at least one outlet for emitting the primary air flow, and defines an opening through which a secondary air flow from outside the fan assembly is drawn by the primary air flow emitted from the at least one outlet. To allow at least one parameter of an air flow, formed from the combination of the primary and secondary air flows, to be adjusted by a user, the nozzle has an adjustable configuration.
The at least one parameter of the combined air flow may comprise at least one of the profile, orientation, direction, flow rate (as measured, for example, in liters per second), and velocity of the combined air flow. Thus, through adjusting the configuration of the nozzle a user may adjust the direction in which the combined air flow is projected forward from the fan assembly, for example to angle the air flow towards or away from a person in the vicinity of the fan assembly. Alternatively, or additionally, the user may expand or restrict the profile of the combined air flow to increase or decrease the number of users within the path of the air flow. As another alternative the user may change the orientation of the air flow, for example through the rotation of a relatively narrow air flow to provide a relatively wide air flow for cooling a number of users.
The nozzle may be adjustable to adopt one of a number of discrete configurations. The nozzle may be locked in a selected configuration so that the configuration of the nozzle cannot be adjusted later by a user. However, it is preferred that the nozzle may be releasable or otherwise moveable from a selected configuration to allow a user to adjust the configuration of the nozzle as required during the use of the fan assembly.
The configuration of the nozzle may be adjusted manually by the user, or it may be adjusted automatically by an automated mechanism of the fan assembly, for example in response to a user operation of a user interface of the fan assembly. This user interface may be located on a body of the fan assembly, or it may be provided by a remote control connected wirelessly to the fan assembly.
The configuration of the nozzle may be adjusted by altering the position, shape or state of at least one part of the nozzle. This part of the nozzle may be rotated, translated, pivoted, extended, retracted, expanded, contracted, slid or otherwise moved relative to another part of the nozzle to adjust the configuration of the nozzle.
For example, the size and shape of the opening may be fixed, and so a part of the nozzle may be moved relative to the opening to adjust the configuration of the nozzle. Alternatively, or additionally, the size and shape of the at least one outlet may be fixed, and so a part of the nozzle may be moved relative to the at least one outlet to adjust the configuration of the nozzle. This moveable part of the nozzle may be located upstream or downstream of the at least one outlet, but in a preferred embodiment the moveable part of the nozzle is located downstream of the at least one outlet.
The nozzle may comprise a first part, and a second part which is moveable relative to the first part, thereby adjusting the configuration of the nozzle. As mentioned above, this second part of the nozzle may be moveable relative to the opening, which may remain in a fixed configuration as the second part of the nozzle is moved relative thereto. Alternatively, or additionally, this second part of the nozzle may be moveable relative to the at least one outlet, which may remain in a fixed configuration as the second part of the nozzle is moved relative thereto.
The second part of the nozzle preferably comprises a flow guiding member. The flow guiding member may be selectively exposed to at least the primary air flow to vary said at least one parameter of the combined air flow. Alternatively, or additionally, at least one of the position and the orientation of the flow guiding member relative to the opening or the at least one air outlet may be adjusted to vary said at least one parameter of the combined air flow.
The second part of the nozzle is preferably rotatable relative to the first part of the nozzle. Alternatively, or additionally, the second part of the nozzle may be slidably moveable relative to the first part of the nozzle.
The second part of the nozzle may be mounted on an external surface of the nozzle. The second part of the nozzle may be moved over this external surface to vary the configuration of the nozzle.
The second part of the nozzle may be moveable relative to the first part of the nozzle between a stowed position and at least one deployed position, for example, to vary a parameter of the combined air flow generated by the fan assembly. In the stowed position the first part of the nozzle may be shielded from the air flow, whereas in each of the deployed positions the first part of the nozzle may be exposed to the combined air flow to adjust a parameter of the air flow generated by the fan assembly by a respective different amount. For example, in each of the deployed positions the second part of the nozzle may be exposed to the air flow by a respective different amount.
The second part of the nozzle may be moveable between a first position in which the combined air flow generated by the fan assembly has a first parameter, for example a first orientation, a first shape or a first direction, and a second position in which the combined air flow generated by the fan assembly has a second parameter, for example a second orientation, a second shape or a second direction, which is different from the first parameter. In each position, the second part of the nozzle may be exposed to the primary air flow.
The first part of the nozzle may be located downstream from the at least one outlet. The first part of the nozzle is preferably maintained in a fixed position relative to the at least one outlet as the second part of the nozzle is moved between the stowed position and the at least one deployed position. In the at least one deployed position, the second part of the nozzle is preferably located downstream from the first part of the nozzle.
The first part of the nozzle preferably comprises a surface over which the at least one outlet is arranged to direct the air flow. Preferably, the surface over which the at least one outlet is arranged to direct the air flow comprises a Coanda surface. 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 in which a primary air flow is directed over a 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 1966 pages 84 to 92. Through use of a Coanda surface, an increased amount of air from outside the fan assembly is drawn through the opening by the air emitted from the at least one outlet.
In a preferred embodiment an air flow is created through the nozzle of the fan assembly. In the following description this air flow will be referred to as the primary air flow. The primary air flow is emitted from the nozzle and preferably passes over a Coanda surface. The primary air flow entrains air surrounding 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 nozzle and, by displacement, from other regions around the fan assembly, and passes predominantly through the opening defined by the nozzle. The primary air flow directed over the Coanda surface combined with the entrained secondary air flow equates to a total air flow emitted or projected forward from the opening defined by the nozzle.
The surface over which the primary air flow is directed preferably comprises a diffuser portion downstream from the at least one outlet. The diffuser portion may thus form part of a Coanda surface. The diffuser portion preferably extends about an axis, and preferably tapers towards or away from the axis.
The surface of the nozzle may also include a guide portion located downstream of the diffuser portion and angled thereto for channelling the combined air flow generated by the fan assembly. The guide portion is preferably tapered inwardly, that is, towards the axis, relative to the diffuser portion. The guide portion may itself taper towards or away from the axis. For example, the diffuser portion may taper away from the axis, and the guide portion may taper towards the axis. Alternatively, the diffuser portion may taper away from the axis, and the guide portion may be substantially cylindrical.
The surface of the nozzle may comprise a cutaway portion, with the second part of the nozzle being moveable to at least partially cover the cutaway portion. The surface may comprise a plurality of cutaway portions, with the second part of the nozzle being moveable to at least partially cover at least one of the cutaway portions. For example, the second part of the nozzle may be moveable relative to the surface to cover a selected one of the cutaway portions by a desired amount. Alternatively, the second part of the nozzle may be moveable to cover simultaneously each of the cutaway portions by a desired amount.
The cutaway portions may be regularly or irregularly spaced about the nozzle. The cutaway portions are preferably arranged in an annular array. The cutaway portions may have the same or different sizes and/or shapes. The, or each, cutaway portion may have any desired shape. In a preferred embodiment the, or each, cutaway portion has a shape which is generally arcuate, but the, or each, cutaway portion may be circular, oval, polygonal or irregular.
The, or each, cutaway portion may be located in the diffuser portion of the surface, or in the guide portion of the surface. The, or each, cutaway portion is preferably located at or towards a front edge of the nozzle. For example, the nozzle may comprise cutaway portions located on opposite sides of the guide portion. These cutaway portions may be located at side extremities of the nozzle, and/or at upper and lower extremities of the nozzle.
The second part of the nozzle may be generally annular in shape, and rotated relative to the Coanda surface by the user. This can allow one or more of the cutaway portions to be selectively covered. The inner surface of the second part of the nozzle preferably has substantially the same shape as the inner surface of the guide portion.
As an alternative to arranging the second part of the nozzle to cover cutaway portions of the surface of the nozzle, the second part of the nozzle may be moveable between a stowed position and at least one deployed position in which the second part of the nozzle is located downstream from the surface of the nozzle. In its stowed position, the second part of the nozzle may extend about the surface so that it is shielded from the combined air flow. As mentioned above, the second part of the nozzle may be located on an external surface of the nozzle, but alternatively the second part of the nozzle may be located within the nozzle when in its stowed position. The second part of the nozzle may then be pulled from the nozzle to move it from its stowed position to a deployed position. For example, a front part of the nozzle may comprise a slot from which the second part of the nozzle is pulled to withdraw the second part from the nozzle and into one of its deployed positions. A tab or other graspable member may be located on the second part to facilitate its withdrawal from the stowed position.
The second part of the nozzle may comprise a guide surface for changing the profile of the combined air flow. The guide surface may have a similar configuration to the guide portion discussed above. The guide surface may have a cylindrical or a frusto-conical shape. The guide surface preferably tapers inwardly relative to the surface of the nozzle. In the deployed position, the guide surface may converge inwardly in a direction extending away from the surface in order to focus the combined air flow towards a user located in front of the fan assembly.
As mentioned above, the second part of the nozzle is preferably generally annular in shape, and may be in the form of a hoop which is moveable relative to the other parts of the nozzle.
The nozzle is preferably in the form of a loop extending about the opening.
The nozzle may have a single outlet from which the primary air flow is emitted. Alternatively, the nozzle may comprise a plurality of outlets each for emitting a respective portion of the primary air flow. In this case, the outlets are preferably spaced about the opening. The nozzle preferably comprises a mouth for receiving the primary air flow, and for conveying the primary air flow to the outlet(s). The mouth preferably extends about the opening, more preferably continuously about the opening.
The spacing between opposing surfaces of the nozzle at the outlet(s) is preferably in the range from 0.5 mm to 5 mm. The nozzle preferably comprises an interior passage which extends about the opening, preferably continuously about the opening so that the opening is an enclosed opening which is surrounded by the interior passage.
The nozzle is preferably mounted on a base housing said system for creating an air flow. In the preferred fan assembly the system for creating an air flow through the nozzle comprises an impeller driven by a motor.
In a second aspect the present invention provides a fan assembly comprising a nozzle and a system for creating an air flow through the nozzle, the nozzle comprising an interior passage, at least one outlet for receiving at least a portion of the air flow from the interior passage, and a surface located adjacent said at least one outlet and over which said at least one outlet is arranged to direct said at least a portion of the air flow, characterized in that the nozzle has an adjustable configuration.
In a third aspect, the present invention provides a nozzle for a fan assembly, the nozzle comprising at least one outlet for emitting a primary air flow, and defining an opening through which a secondary air flow from outside the fan assembly is drawn by the primary air flow emitted from the at least one outlet, the nozzle comprising a first part and a second part which is moveable relative to the first part. The first part of the nozzle may be located upstream or downstream from the at least one outlet. The second part is preferably moveable relative to the first part between a stowed position in which it is shielded from the air flow and a deployed position in which it may be located downstream from the first part. Each part of the nozzle may comprise a surface over which the air flow is directed by said at least one outlet.
In a fourth aspect, the present invention provides a nozzle for a fan assembly, the nozzle comprising an interior passage, at least one outlet for receiving at least a portion of the air flow from the interior passage, and a surface located adjacent said at least one air outlet and over which said at least one outlet is arranged to direct said at least a portion of the air flow, characterized in that the nozzle has an adjustable configuration. The nozzle preferably comprises a moveable part which is moveable between a stowed position in which it is shielded from the air flow and a deployed position in which it is located downstream from the surface.
Features described above in connection with the first aspect of the invention are equally applicable to each of the second to fourth aspects of the invention, and vice versa.
Preferred features of the invention will now be described, by way of example only, with reference to the accompanying drawings, in which:
The body 12 comprises a substantially cylindrical main body section 20 mounted on a substantially cylindrical lower body section 22. The main body section 20 and the lower body section 22 preferably have substantially the same external diameter so that the external surface of the upper body section 20 is substantially flush with the external surface of the lower body section 22. In this embodiment the body 12 has a height in the range from 100 to 300 mm, and a diameter in the range from 100 to 200 mm.
The main body section 20 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 20. Alternatively, the air inlet 14 may comprise one or more grilles or meshes mounted within windows formed in the main body section 20. The main body section 20 is open at the upper end (as illustrated) thereof to provide an air outlet 23 through which the primary air flow is exhausted from the body 12.
The main body section 20 may be tilted relative to the lower body section 22 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 22 and the lower surface of the main body section 20 may be provided with interconnecting features which allow the main body section 20 to move relative to the lower body section 22 while preventing the main body section 20 from being lifted from the lower body section 22. For example, the lower body section 22 and the main body section 20 may comprise interlocking L-shaped members.
The lower body section 22 comprises a user interface of the fan assembly 10. The user interface comprises a plurality of user-operable buttons 24, 26, a dial 28 for enabling a user to control various functions of the fan assembly 10, and user interface control circuit 30 connected to the buttons 24, 26 and the dial 28. The lower body section 22 is mounted on a base 32 for engaging a surface on which the fan assembly 10 is located.
The lower body section 22 also houses a mechanism, indicated generally at 36, for oscillating the lower body section 22 relative to the base 32. The operation of the oscillating mechanism 36 is controlled by the main control circuit 34 in response to the user operation of the button 26. The range of each oscillation cycle of the lower body section 22 relative to the base 32 is preferably between 60° and 120°, and in this embodiment is around 80°. In this embodiment, the oscillating mechanism 36 is arranged to perform around 3 to 5 oscillation cycles per minute. A mains power cable 38 for supplying electrical power to the fan assembly 10 extends through an aperture formed in the base 32. The cable 38 is connected to a plug (not shown) for connection to a mains power supply.
The main body section 20 houses an impeller 40 for drawing the primary air flow through the air inlet 14 and into the body 12. Preferably, the impeller 40 is in the form of a mixed flow impeller. The impeller 40 is connected to a rotary shaft 42 extending outwardly from a motor 44. In this embodiment, the motor 44 is a DC brushless motor having a speed which is variable by the main control circuit 34 in response to user manipulation of the dial 28. The maximum speed of the motor 44 is preferably in the range from 5,000 to 10,000 rpm. The motor 44 is housed within a motor bucket comprising an upper portion 46 connected to a lower portion 48. The upper portion 46 of the motor bucket comprises a diffuser 50 in the form of a stationary disc having spiral blades.
The motor bucket is located within, and mounted on, a generally frusto-conical impeller housing 52. The impeller housing 52 is, in turn, mounted on a plurality of angularly spaced supports 54, in this example three supports, located within and connected to the main body section 20 of the base 12. The impeller 40 and the impeller housing 52 are shaped so that the impeller 40 is in close proximity to, but does not contact, the inner surface of the impeller housing 52. A substantially annular inlet member 56 is connected to the bottom of the impeller housing 52 for guiding the primary air flow into the impeller housing 52. An electrical cable 58 passes from the main control circuit 34 to the motor 44 through apertures formed in the main body section 20 and the lower body section 22 of the body 12, and in the impeller housing 52 and the motor bucket.
Preferably, the body 12 includes silencing foam for reducing noise emissions from the body 12. In this embodiment, the main body section 20 of the body 12 comprises a first foam member 60 located beneath the air inlet 14, and a second annular foam member 62 located within the motor bucket.
A flexible sealing member 64 is mounted on the impeller housing 52. The flexible sealing member prevents air from passing around the outer surface of the impeller housing 52 to the inlet member 56. The sealing member 64 preferably comprises an annular lip seal, preferably formed from rubber. The sealing member 64 further comprises a guide portion in the form of a grommet for guiding the electrical cable 58 to the motor 44.
Returning to
The nozzle 16 comprises an annular front casing section 76 connected to and extending about an annular rear casing section 78. The annular sections 76, 78 of the nozzle 16 extend about the central axis X. Each of these sections may be formed from a plurality of connected parts, but in this embodiment each of the front casing section 76 and the rear casing section 78 is formed from a respective, single molded part. The rear casing section 78 comprises a base 80 which is connected to the open upper end of the main body section 20 of the body 12, and which has an open lower end for receiving the primary air flow from the body 12.
With reference also to
The front casing section 76 defines the Coanda surface 72 of the nozzle 16. The front casing section 76 and the rear casing section 78 together define an annular interior passage 88 for conveying the primary air flow to the mouth 18. The interior passage 88 extends about the axis X, and is bounded by the internal surface 90 of the front casing section 76 and the internal surface 92 of the rear casing section 78. The base 80 of the front casing section 76 is shaped to convey the primary air flow into the interior passage 88 of the nozzle 16.
The mouth 18 is defined by overlapping, or facing, portions of the internal surface 92 of the rear casing section 78 and the external surface 94 of the front casing section 76, respectively. The mouth 18 preferably comprises an air outlet in the form of an annular slot. The slot is preferably generally circular in shape, and preferably has 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 mouth 18 for urging apart the overlapping portions of the front casing section 76 and the rear casing section 78 to control the width of the air outlet of the mouth 18. These spacers may be integral with either the front casing section 76 or the rear casing section 78. The mouth 18 is shaped to direct the primary air flow over the external surface 94 of the front casing section 76.
The external surface of the nozzle 16 also comprises a guide portion 96 located downstream from the diffuser portion 74 and angled thereto. The guide portion 96 similarly extends about the axis X. The guide portion 96 may be inclined to the axis X by an angle in the range from −30 to 30°, but in this example the guide portion 96 is generally cylindrical and is centered on the axis X. The depth of the guide portion 96, as measured along the axis X, is preferably in the range from 20 to 80% of the depth of the diffuser portion 74, and in this example is around 60%.
The guide portion 96 comprises a first section 98 which is connected to, and preferably integral with, the diffuser portion 74 of the Coanda surface 72, and a second section 100 which is moveable relative to the first section 98 to adjust a parameter of the air flow generated by the fan assembly 10. In this example, the first section 98 of the guide portion 96 of the nozzle 16 comprises an upper portion 102 and a lower portion 104. Each of the upper portion 102 and the lower portion 104 is in the form of a partially cylindrical surface centered on the axis X, and which extends about the axis X by an angle which is preferably in the range from 30 to 150°, and in this example is around 120°. The upper and lower portions 102, 104 are separated by a pair of cutaway portions 106, 108 of the first section 98. In this example each cutaway portion 106, 108 is located at a respective side of the first section 98, and extends from the front edge 110 of the first section 98 to the substantially circular front edge 112 of the diffuser portion 74. The cutaway portions 106, 108 have generally the same size and shape, and in this example each extend around 60° about the axis X.
The second section 100 of the guide portion 96 is generally annular in shape, and is mounted on the external surface of the nozzle 16 so as to extend about the first section 98 of the guide portion 96. The second section 100 has a generally cylindrical curvature, and is also centered on the axis X. The front edge 114 of the second section 100 is substantially co-planar with the front edge 110 of the first section 98, whereas the substantially circular rear edge 116 is located rearwardly of the first section 96 so as to surround the diffuser portion 74 of the Coanda surface 72.
The depth of the second section 100 of the guide portion 96, as measured along the axis X, varies about the axis X. The second section 100 comprises two forwardly extending portions 118, 120 which are connected by arcuate connectors 122, 124. The forwardly extending portions 118, 120 of the second section 100 have generally the same size and shape as the upper and lower portions 102, 104 of the front section 98. The connectors 122, 124 are relatively narrow, and are located behind the front edge 112 of the diffuser portion 74 of the Coanda surface 72 so that these connectors 122, 124 are not exposed to the air flow generated by the fan assembly 10.
As mentioned above, the second section 100 of the guide portion 96 is moveable relative to the first section 98 of the guide portion 96. In this example, the second section 100 is located about the first section 98 so as to be rotatable about the axis X. The second section 100 comprises a pair of tabs 126 which extend radially outwardly to allow a user to grip the tabs to rotate the second section 100 relative to the first section 98. In this example, the second section 100 slides over the first section 98 as it is moved relative thereto. The inner surface of the second section 100 may comprise a radially inwardly extending ridge, which may extend partially or fully about the axis X, which is received within an annular groove formed on the outer surface of the front casing section 76 and which guides the movement of the second section 100 relative to the first section 98.
To operate the fan assembly 10 the user the user presses button 24 of the user interface. The user interface control circuit 30 communicates this action to the main control circuit 34, in response to which the main control circuit 34 activates the motor 44 to rotate the impeller 40. The rotation of the impeller 40 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 44, and therefore the rate at which air is drawn into the body 12 through the air inlet 14, by manipulating the dial 28 of the user interface. Depending on the speed of the motor 44, the primary air flow generated by the impeller 40 may be between 10 and 30 liters per second. The primary air flow passes sequentially through the impeller housing 52 and the air outlet 23 at the open upper end of the main body portion 20 to enter the interior passage 88 of the nozzle 16. The pressure of the primary air flow at the air outlet 23 of the body 12 may be at least 150 Pa, and is preferably in the range from 250 to 1.5 kPa.
Within the interior passage 88 of the nozzle 16, the primary air flow is divided into two air streams which pass in opposite directions around the opening 70 of the nozzle 16. As the air streams pass through the interior passage 70, air is emitted through the mouth 18. The primary air flow emitted from the mouth 18 is directed over the Coanda surface 72 of the nozzle 16, causing a secondary air flow to be generated by the entrainment of air from the external environment, specifically from the region around the mouth 18 and from around the rear of the nozzle 16. This secondary air flow passes through the central opening 70 of the nozzle 16, where it combines with the primary air flow to produce a combined, or total, air flow, or air current, projected forward from the nozzle 16.
As part of the nozzle 16, in this example the second section 100 of the guide portion 96 of the nozzle 16, is moveable relative to the remainder of the nozzle 16, the nozzle 16 may adopt one of a number of different configurations.
As the angle of the diffuser portion 74 of the Coanda surface 72 is relatively wide, in this example around 28°, the profile of the combined air flow projected forward from the fan assembly 10 will be relatively wide. However, in view of the partial guiding of the combined air flow towards the axis X, the profile of the air current generated by the fan assembly 10 is non-circular. The profile is generally oval, with the height of the profile being smaller than the width of the profile. This flattening, or widening, of the profile of the air current in this nozzle configuration can make the fan assembly 10 particularly suitable for use as a desk fan in a room, office or other environment to deliver a cooling air current simultaneously to a number of users in proximity to the fan assembly 10.
By gripping the tabs 126 of the second section 100 of the guide portion 96, a user may rotate the second section 100 relative to the first section 98 to change the configuration of the nozzle 16.
The movement of the nozzle 16 between these configurations also varies the flow rate and the velocity of the combined air flow generated by the fan assembly 10. When the second section 100 is in the stowed position, the combined air flow has a relatively high flow rate but a relatively low velocity. When the second section 100 is in the fully deployed position, the combined air flow has a relatively low flow rate but a relatively high velocity.
As an alternative to locating the portions 102, 104 of the front section 98 at the upper and lower extremities of the guide portion 96, these portions may be located at the side extremities of the guide portion 96. Thus, when the second section 100 is in its stowed position, the height of the profile of the air current may be greater than the width of the profile. This stretching of the profile of the air current in a vertical direction can make the fan assembly particularly suitable for use as a floor standing tower or pedestal fan.
In the fan assembly 10, the second section 100 is arranged to cover simultaneously both of the cutaway portions 106, 108 when in its fully deployed position.
In this example, the change in the orientation of the combined air flow between the first and second fully deployed positions is around 180°. Thus, the movement of the nozzle 16 between these two configurations, in which the second section 100 is in the first fully deployed position and the second fully deployed position respectively, can produce an effect which is similar to that produced by oscillating the lower body section 22 relative to the base 32, that is, a sweeping of the combined air flow over an arc during the use of the fan assembly 10′. Mechanizing the movement of the second section 100 relative to the first section 98 can thus provide an alternative means of sweeping the combined air flow over an arc.
The nozzle 202 comprises an annular front casing section 212 connected to and extending about an annular rear casing section 214. The annular sections 212, 214 of the nozzle 202 extend about the central axis X. Each of these sections may be formed from a plurality of connected parts, but in this embodiment each of the front casing section 212 and the rear casing section 214 is formed from a respective, single molded part. The rear casing section 214 comprises a base 216 which is connected to the open upper end of the main body section 20 of the body 12, and which has an open lower end for receiving the primary air flow from the body 12. As with the nozzle 16 of the fan assembly 10, during assembly the front end of the rear casing section 214 is inserted into a slot located in the front casing section 212. The casing sections 212, 214 may be connected together using an adhesive introduced to the slot.
The front casing section 212 defines the Coanda surface 208 of the nozzle 202. The front casing section 212 and the rear casing section 214 together define an annular interior passage 218 for conveying the primary air flow to the mouth 204. The interior passage 218 extends about the axis X, and is bounded by the internal surface 220 of the front casing section 212 and the internal surface 222 of the rear casing section 214. The base 216 of the front casing section 212 is shaped to convey the primary air flow into the interior passage 218 of the nozzle 202.
The mouth 204 is defined by overlapping, or facing, portions of the internal surface 222 of the rear casing section 214 and the external surface 224 of the front casing section 212, respectively. The mouth 204 preferably comprises an air outlet in the form of an annular slot. The air outlet is preferably generally circular in shape, and preferably has 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 mouth 204 for urging apart the overlapping portions of the front casing section 212 and the rear casing section 214 to control the width of the air outlet of the mouth 204. These spacers may be integral with either the front casing section 212 or the rear casing section 214. The mouth 204 is shaped to direct the primary air flow over the external surface 224 of the front casing section 212.
The nozzle 202 further comprises a guide surface 226. The guide surface 226 extends about the axis X, and is angled relative to the diffuser portion 210 of the Coanda surface 208. The guide surface 226 may be inclined to the axis X by an angle in the range from −30 to 30°, but in this example the guide surface 226 is generally cylindrical and is centered on the axis X. The depth of the guide surface 226, as measured along the axis X, is preferably in the range from 20 to 80% of the depth of the diffuser portion 210, and in this example is around 50%.
The guide surface 226 is moveable relative to the diffuser portion 210 of the Coanda surface 208 to adjust a parameter of the air flow generated by the fan assembly 10. In this fan assembly 200, the guide surface 226 is mounted on the external surface of the nozzle 202 so as to be rotatable about the axis X. The guide surface 226 comprises a pair of tabs 228 which extend radially outwardly from the outer surface of the guide surface 226 to allow a user to grip the tabs 228 to rotate the guide surface 226 relative to the diffuser portion 210. In this example, the guide surface 226 slides over the outer surface of the nozzle 16 as it is moved by the user.
The inner surface of the guide surface 226 comprises a plurality of helical grooves 230 which each receive a respective helical ridge 232 which extends outwardly from the outer surface of the nozzle. The engagement between the groves 230 and the ridges 232 guides the movement of the guide surface 226 relative to the diffuser portion 210 so that as the guide surface 226 is rotated relative to the nozzle 202, it moves along the axis X.
As an alternative to providing helical grooves 230 and ridges 232, the grooves 230 and ridges 232 may each extend substantially parallel to the axis X. In this case, the guide surface 226 may be pulled over the external surface of the nozzle 202 to move the guide surface 226 relative to the diffuser portion 210.
The guide surface 226 is moveable relative to the diffuser portion 210 between a stowed position and a deployed position to adjust the configuration of the nozzle 202.
By gripping the tabs 228 of the guide surface 226, a user may rotate the guide surface 226 to move the guide surface 226 along the axis X, and thereby change the configuration of the nozzle 202.
The innermost, external surface of the nozzle 302 comprises a Coanda surface 308 located adjacent the mouth 304, and over which the mouth 304 is arranged to direct the air emitted from the nozzle 16. The Coanda surface 308 comprises a diffuser portion 310 tapering away from the central axis X. In this example, the diffuser portion 310 is in the form of a generally frusto-conical surface extending about the axis X, and which is inclined to the axis X at an angle in the range from 5 to 35°, and in this example is around 20°.
The nozzle 302 comprises an annular front casing section 312 connected to an annular rear casing section 314. The annular sections 312, 314 of the nozzle 302 extend about the central axis X. Each of these sections may be formed from a single component or a plurality of connected parts. In this embodiment, the front casing section 312 is integral with the rear casing section 314. The rear casing section 314 comprises a base 316 which is connected to the open upper end of the main body section 20 of the body 12, and which has an open lower end for receiving the primary air flow from the body 12. The front casing section 312 defines the Coanda surface 308 of the nozzle 302. The front casing section 312 and the rear casing section 314 together define an annular interior passage 318 for conveying the primary air flow to the mouth 304. The interior passage 318 extends about the axis X, and is bounded by the internal surface 320 of the front casing section 312 and the internal surface 322 of the rear casing section 314. The base 316 of the front casing section 312 is shaped to convey the primary air flow into the interior passage 318 of the nozzle 302.
The mouth 304 is defined by overlapping, or facing, portions of the internal surface 322 of the rear casing section 314 and the external surface 324 of the front casing section 312, respectively. The mouth 304 is shaped to direct the primary air flow over the external surface 324 of the front casing section 312. The mouth 304 preferably comprises an air outlet in the form of an annular slot. The air outlet is preferably generally circular in shape, and preferably has 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. Where the front casing section 312 and the rear casing section 314 are formed from separate components, spacers may be spaced about the mouth 304 for urging apart the overlapping portions of the front casing section 312 and the rear casing section 314 to control the width of the air outlet of the mouth 304. These spacers may be integral with either the front casing section 312 or the rear casing section 314. Where the front casing section 312 is integral with the rear casing section 314, the nozzle 302 may be formed with a series of fins which are spaced about, and extend across, the mouth 304 between the internal surface 322 of the rear casing section 314 and the external surface 324 of the front casing section 312.
The nozzle 302 further comprises a guide surface 326. The guide surface 326 extends about the axis X, and is centered on the axis X. The guide surface 326 is angled relative to the diffuser portion 310 of the Coanda surface 308. In this fan assembly 300, the guide surface 326 converges inwardly towards the axis X, and is inclined to the axis X by an angle of around 15°. The depth of the guide surface 326, as measured along the axis X, is preferably in the range from 20 to 80% of the depth of the diffuser portion 310, and in this example is around 30%.
The nozzle 302 further comprises an annular outer casing section 328 which extends about the front portion of the external surface 324 of the front casing section 312. An annular housing 330 is defined between the front casing section 312 and the outer casing section 328. The housing 330 has an opening in the form of an annular slot 332 which is located at the front of the nozzle 302.
The guide surface 326 is moveable relative to the diffuser portion 310 between a stowed position and a deployed position to adjust the configuration of the nozzle 302.
When the guide surface 326 is in the stowed position, the combined air flow generated by the fan assembly 300 has a relatively high flow rate but a relatively low velocity.
The guide surface 326 comprises a tab 334 which extends forwardly from the front of the guide surface 326 so as to protrude from the housing 330 when the guide surface 326 is in its stowed position. To move the guide surface 326 from its stowed position, the user grips the tab 334 and rotates the guide surface 326 relative to the diffuser portion 310 in a clockwise direction as viewed in
Alternatively, the guide surface 326 may be pulled over the external surface of the nozzle 302 to move the guide surface 326 from its stowed position.
By moving the guide surface 326 along the axis X, the user changes the configuration of the nozzle 302.
Number | Date | Country | Kind |
---|---|---|---|
1017551.1 | Oct 2010 | GB | national |
1105687.6 | Apr 2011 | GB | national |
Number | Name | Date | Kind |
---|---|---|---|
284962 | Huston | Sep 1883 | A |
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 Salvatore | 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 |
2711682 | Drechsel | Jun 1955 | 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 |
4184417 | Chancellor | Jan 1980 | 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, IV | 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 |
5794306 | Firdaus | Aug 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 |
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 |
7198473 | Stickland et al. | Apr 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 |
8308445 | Gammack et al. | Nov 2012 | B2 |
8348629 | Fitton et al. | Jan 2013 | B2 |
8356804 | Fitton et al. | Jan 2013 | B2 |
8454322 | Gammack et al. | Jun 2013 | B2 |
8529226 | Li | Sep 2013 | B2 |
8544826 | Ediger et al. | Oct 2013 | B2 |
8721307 | Li | May 2014 | 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 |
20090078120 | Kummer et al. | Mar 2009 | A1 |
20090120925 | Lasko | May 2009 | A1 |
20090191054 | Winkler | Jul 2009 | A1 |
20090214341 | Craig | Aug 2009 | A1 |
20100133707 | Huang | Jun 2010 | 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 |
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 |
20140079566 | Gammack et al. | Mar 2014 | A1 |
20140084492 | Staniforth et al. | Mar 2014 | A1 |
20140210114 | Staniforth et al. | Jul 2014 | A1 |
20140255173 | Poulton et al. | Sep 2014 | A1 |
20140255217 | Li | Sep 2014 | A1 |
Number | Date | Country |
---|---|---|
560119 | Aug 1957 | BE |
1055344 | May 1979 | CA |
2155482 | Sep 1996 | CA |
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 |
201011346 | Jan 2008 | CN |
201180678 | Jan 2009 | CN |
201221477 | Apr 2009 | CN |
101424279 | May 2009 | CN |
101451754 | Jun 2009 | CN |
201281416 | Jul 2009 | CN |
201349269 | Nov 2009 | CN |
101684828 | Mar 2010 | CN |
201486901 | May 2010 | CN |
101749288 | Jun 2010 | CN |
201502549 | Jun 2010 | CN |
201507461 | Jun 2010 | CN |
101825096 | Sep 2010 | CN |
101825101 | Sep 2010 | CN |
101825102 | Sep 2010 | CN |
101825103 | Sep 2010 | CN |
101825104 | Sep 2010 | CN |
201568337 | Sep 2010 | CN |
101858355 | Oct 2010 | CN |
101936310 | Jan 2011 | CN |
201696365 | Jan 2011 | CN |
201696366 | 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 |
201771875 | Mar 2011 | CN |
201779080 | Mar 2011 | CN |
201786777 | Apr 2011 | CN |
201786778 | Apr 2011 | CN |
201802648 | Apr 2011 | CN |
102095236 | Jun 2011 | CN |
201858204 | Jun 2011 | CN |
201874898 | Jun 2011 | CN |
201874901 | Jun 2011 | CN |
201917047 | Aug 2011 | CN |
102251973 | Nov 2011 | CN |
102287357 | Dec 2011 | CN |
102367813 | Mar 2012 | CN |
202267207 | Jun 2012 | CN |
202431623 | Sep 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 007 037 | 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 |
2 578 889 | Apr 2013 | EP |
1033034 | Jul 1953 | FR |
1119439 | Jun 1956 | FR |
1387334 | 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 |
2493231 | Jan 2003 | 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 |
2484671 | Apr 2012 | GB |
2484695 | Apr 2012 | GB |
2484761 | Apr 2012 | GB |
2493505 | Feb 2013 | GB |
2493507 | Feb 2013 | GB |
2500011 | Sep 2013 | GB |
31-13055 | Aug 1956 | JP |
35-4369 | Mar 1960 | JP |
39-7297 | Mar 1964 | JP |
46-7230 | Dec 1971 | 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 |
63-36794 | Mar 1988 | 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 |
3-286775 | Dec 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 |
2006-89096 | 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 |
517825 | Jan 2003 | TW |
589932 | Jun 2004 | TW |
M394383 | Dec 2010 | TW |
M399207 | Mar 2011 | 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-2011050041 | Apr 2011 | WO |
WO-2012006882 | Jan 2012 | WO |
WO-2012033517 | Mar 2012 | WO |
WO-2013014419 | Jan 2013 | WO |
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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. 30, 2012, directed to U.S. Appl. No. 12/716,707; 7 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, P. et al., U.S. Office Action mailed Jun. 8, 2012, directed to U.S. Appl. No. 12/230,613; 15 pages. |
Gammack, P. et al., U.S. Office Action mailed Jun. 25, 2012, directed to U.S. Appl. No. 12/716,749; 11 pages. |
Gammack et al., Office Action mailed Sep. 17, 2012, directed to U.S. Appl. No. 13/114,707; 12 pages. |
Gammack et al., U.S. Office Action mailed Aug. 20, 2012, directed to U.S. Appl. No. 12/945,558; 15 pages. |
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, P. et al. U.S. Office Action mailed Oct. 18, 2012, directed to U.S. Appl. No. 12/917,247; 11 pages. |
GB Search Report dated Jan. 26, 2011, directed to GB Application No. 1017551.1; 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, 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. |
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 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 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. |
Gammack, P. et al., Office Action mailed Aug. 19, 2013, directed to U.S. Appl. No. 12/716,515; 20 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. |
Search Report dated Jan. 17, 2013, directed to GB Application No. 1216802.7; 2 pages. |
Search Report dated Jan. 17, 2013, directed to GB Application No. 1216803.5; 2 pages. |
Gammack, P. et al., U.S. Office Action mailed Feb. 10, 2014, directed to U.S. Appl. No. 12/716,515; 21 pages. |
GB Search Report dated Jan. 12, 2012, directed to GB Patent Application No. 1105687.6; 2 pages. |
International Search Report and Written Opinion mailed Jan. 20, 2012, directed to International Patent Application No. PCT/GB2011/051815; 8 pages. |
Li et al., U.S. Office Action mailed Oct. 25, 2013, directed to U.S. Appl. No. 13/686,480; 17 pages. |
Gammack et al., U.S. Office Action mailed Apr. 24, 2014, directed to U.S Appl. No. 12/716,740; 16 pages. |
Gammack et al., U.S. Office Action mailed Sep. 3, 2014, directed to U.S. Appl. No. 13/861,891; 7 pages. |
Staniforth et al., U.S. Office Action mailed Sep. 18, 2014, directed to U.S. Appl. No. 13/559,142; 18 pages. |
Fitton et al., U.S. Office Action mailed Jun. 13, 2014, directed to U.S. Appl. No. 13/274,998; 11 pages. |
Number | Date | Country | |
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20120093630 A1 | Apr 2012 | US |