Low-noise blower

Abstract
A low-noise blower has an impeller with an impeller plate and a plurality of blades each attached to the impeller plate. Each blade has a tip and a leading surface with a first portion that is proximate to the tip and has a first radius that is within a range of 0.03-0.20 inch.
Description
BACKGROUND

Field


The present disclosure generally relates to gas compressors and, in particular, to a centrifugal air blower.


Description of the Related Art


Patients with respiratory injury, such as chronic respiratory failure, may be provided with a respirator to assist with their breathing or, in severe cases, take over the breathing function entirely. Respirators typically provide a flow of air, or other breathing gases, at an elevated pressure during an inhalation interval, followed by an exhalation interval where the pressurized air is diverted so that the air within the patient's lungs can be naturally expelled. The inhalation interval may be initiated upon detection of a patient's natural inhalation or by the respirator


Respirators are available in a variety of sizes with different ranges of air flows and pressures that can be provided. For example, a neonatal patient will require a much lower pressure and volume of air per breath than an adult, and many conventional respirators cannot provide accurate delivery of pressurized air over this range of volumes and pressures.


In conventional respirators that use a blower to pressurize the gas provided to the patient, the blowers that are used are loud and the noise level in the patient's room is commonly 65 dB or more. This level of noise may disrupt the patient's rest and sleep as well as cause fatigue for the caregiver and may further obstruct diagnosis and monitoring of the patient by masking the natural breathing noises that provide an indication of the patient's condition.


SUMMARY

It is advantageous to provide a small, quiet blower that can accurately provide a flow of compressed gas over wide ranges of flow rate and pressure.


In certain embodiments, a blower is disclosed that has an impeller comprising an impeller plate and a plurality of blades each attached to the impeller plate. Each blade has a tip and a leading surface that comprises a first portion proximate to the tip. The first portion has a first radius that is within a range of 0.03-0.20 inch.


In certain embodiments, an impeller is disclosed that has an impeller plate having an outside edge with a first radius and a plurality of blades attached to the impeller plate. Each of the plurality of blades comprises a tip at the outside edge and a leading surface with a first portion extending from the tip and a second portion that extends from the first portion with a second radius that is within the range of 0.14-0.16 inch.





BRIEF DESCRIPTION OF THE DRAWINGS

The accompanying drawings, which are included to provide further understanding and are incorporated in and constitute a part of this specification, illustrate disclosed embodiments and together with the description serve to explain the principles of the disclosed embodiments. In the drawings:



FIGS. 1-2 are top and bottom perspective views of an exemplary blower according to certain aspects of the present disclosure.



FIG. 3 is an exploded view of the blower of FIG. 1 according to certain aspects of the present disclosure.



FIG. 4 is a perspective view of an exemplary impeller according to certain aspects of the present disclosure.



FIG. 5 is a close-up plan view of a vane tip of the impeller of FIG. 3 according to certain aspects of the present disclosure.



FIG. 6 is a perspective view of a conventional impeller.



FIG. 7 is a cross-section of the blower of FIG. 1 according to certain aspects of the present disclosure.



FIG. 8 is an enlarged view of a portion of FIG. 7 according to certain aspects of the present disclosure.



FIGS. 9A-9C are perspective views of the overmolded top housing according to certain aspects of the present disclosure.





DETAILED DESCRIPTION

It is advantageous to provide a relatively small, quiet blower that can accurately provide a flow of compressed gas over wide ranges of flow rate and pressure.


In the following detailed description, numerous specific details are set forth to provide a full understanding of the present disclosure. It will be apparent, however, to one ordinarily skilled in the art that embodiments of the present disclosure may be practiced without some of the specific details. In other instances, well-known structures and techniques have not been shown in detail so as not to obscure the disclosure. In the referenced drawings, like numbered elements are the same or essentially similar. Reference numbers may have letter suffixes appended to indicate separate instances of a common element while being referred to generically by the same number without a suffix letter.


While the discussion herein is directed to the provision of compressed air as part of a medical respirator, the disclosed concepts and methods may be applied to other fields that would also benefit from a quiet, portable source of compressed air. For example, conventional leaf blowers that are commonly used to blow leaves and small garden debris into piles are quite loud and a blower of this type may be advantageous in place of the current blowers.



FIGS. 1-2 are top and bottom perspective views of an exemplary blower 100 according to certain aspects of the present disclosure. In the configuration of FIG. 1, the blower 100 draws in ambient air, or other gases if connected to a source of gas, through inlet 119 of housing 112. Impeller 160 may rotate at a variable speed up to 30,000 rotations per minute (rpm), for example, to centrifugally accelerate the air and provide a flow of pressurized air at outlet 118. In this embodiment, the housing 112 comprises two parts, 112T and 112B (see FIG. 3) held together with multiple clips 114. The section line A-A indicates the cross-sectional view of FIG. 7.



FIG. 2 is a perspective view of the blower 100 of FIG. 1 with the blower 100 rotated so as to make the bottom housing portion 112B visible. A motor 120 is attached to the housing 112 and the shaft of the motor (not visible in FIG. 2) passes through the housing 112 and connects to the impeller 160.



FIG. 3 is an exploded view of the blower 100 of FIG. 1 according to certain aspects of the present disclosure. The top housing portion 112T has an impeller cavity 119. The impeller 160 is at least partially disposed within the impeller cavity 119 when the blower 100 is assembled. The housing 112 comprises a collector 116 formed when the top and bottom housing portions 112T, 112B are mated. In this example, the collector 116 is shaped as a volute having a circular cross-sectional profile along a radial plane of the housing 112, wherein the area of the profile monotonically increases as the distance around the volute from the outlet 118 decreases. In certain embodiments, the volute may have a non-circular profile. In certain embodiments, the area of the profile may be constant over a portion of the volute.


The top and bottom housing portions 112T, 112B also respectively include edges 124U, 124L that are proximate to each other when the blower 100 is assembled and surround the impeller cavity so as to cooperatively define a slot(not visible in FIG. 3) that connects the impeller cavity 119 to the collector 116. The lower housing portion 112B also includes a wall 120 and a shelf 122 adjacent to the edge 124L. This region of the blower 100 is described in greater detail with respect to FIG. 7.



FIG. 4 is a perspective view of a conventional impeller 10. This impeller 10 has a plurality of vanes 12, 20 each having a leading edge 14 and a trailing edge 16, although vanes 20 are shorter than vanes 12 and are commonly referred to as “splitters.” Conventional vanes 12, 20 have a three-dimensional curvature with a generally uniform thickness from leading edge 14 to trailing edge 16, with some rounding of the outside corners and filleting of the inside corners.



FIG. 5 is a perspective view of an exemplary impeller 160 according to certain aspects of the present disclosure. The impeller 160 comprises an impeller plate 162 having a shaped surface 166 and a circular outside edge 164 that are centered about an axis of rotation 161. In this embodiment, there is a set of long vanes 170 that alternate with a set of splitter vanes 171. The portion of the long vanes 170 that is not present in the splitter vanes 171 is referred to as the “inducer” 173. Each vane 170, 171 has an inlet edge 172, a tip 174 that is proximate to the outside edge 164, and a top surface 176 that is, in this example, flat in a generally circumferential direction about axis 161 while being curved in a generally radial direction. The region indicated by the dashed-line oval labeled “B” is shown in FIG. 6.



FIG. 6 is a close-up plan view of a vane tip 174 of the impeller 160 of FIG. 5 according to certain aspects of the present disclosure. The example vane 170 has a leading surface 180 and a trailing surface 182 that meet at the tip 174. The leading surface 180 comprises a first portion 177 and a second portion 175. In this example, the second portion 175 extends from the tip 174 with a radius R2 that is the same radius as the outside edge 164. The first portion 177 abuts the second portion 175 and continues with a radius R1 that is smaller than R2 and larger than the radii conventionally used to round outside edges. In certain embodiments, the radius R1 may be within the range of 0.03-0.20 inch. In certain embodiments, the radius R1 may be within the range of 0.12-0.18 inch. In certain embodiments, the radius R1 may be within the range of 0.14-0.16 inch. In certain embodiments, the radius R1 may be approximately 0.15 inch.


Without being bound by theory, it is believed that the effect of the radius R1 may be to control the turbulence of the air at the tip 174 and reduce the velocity gradient in the air flow as the air leaves the impeller 160, compared to a conventional vane that abruptly ends at the outside edge with a sizable angle between the leading surface and the outside edge, as is visible in the impeller 10 of FIG. 4. By smoothing this transition over a larger area, e.g. the length of the first portion 177 and possible the second portion 175, and redirecting the air flow direction, the velocity gradient is reduced and the air flow may be less turbulent as the air leaves the impeller 160 and passes through the slot 126.


Each vane 170, 171 has a centerline 179 that is coincident with and bisects the top surface 176 between the leading and trailing surfaces 180, 182. The vanes 170, 171 have a common width W taken perpendicular to the centerline 179, wherein W varies along the centerline 179. At a common distance from the tip 174 along the centerline 179, the width W of each vane 170, 171 will be the same, for at least the length of the splitter vanes 171.


The shape and width of the vanes 170, 171 proximate to the second portion 177 may be selected to simply enable the radius to be as large as R1, compared to the constant-thickness vanes of a conventional impeller. In certain embodiments, the trailing surface 182 has a minimum radius that is greater than the radius of the first portion of the leading surface 180. In certain embodiments, the shape and location of the trailing surface 182 may be chosen to cooperate with the leading surface of the adjacent vane 170, 171 to control the pressure and/or velocity of the air flowing between the leading and trailing surfaces 180,182.


The height of the vanes 170, 171, i.e. the distance from the shaped surface 166 to the top surface 176, varies from the inlet edge 172 and tip 174. In certain embodiments, the height is constant from the tip 174 over the first and second portions 177, 175 of the leading surface 180. In certain embodiments, the shaped surface 166 has an outside portion 163 that is proximate to the first and second portions 177, 175 of the leading surface 180. In certain embodiments, the shaped surface 166 is flat and perpendicular to the axis 16 in the outside portion 163.



FIG. 7 is a cross-section taken along section line A-A of the blower 100 of FIG. 1 according to certain aspects of the present disclosure. The arrows 101 and 102 respectively indicate how air is drawn in through the inlet 119 and directed by the impeller 160 into the collector 116. The motor 120 is shown in schematic form and, in this embodiment, the rotor (not shown in FIG. 7) of the motor 120 is directly connected to the impeller 160. The area indicated by the dashed-line box “C” is discussed in greater detail with respect to FIG. 8.



FIG. 8 is an enlarged view of the area C of FIG. 7 according to certain aspects of the present disclosure. The cross-section of impeller 160 shows the top surface 166, a bottom surface 167, and the outside edge 162. The upper edge 124U of the top housing portion 112T and the lower edge 124L of the bottom housing portion 112B are proximate to each other and separated by a slot 126. In this embodiment, the edges 124U and 124L both have a radius R4 on an inside corner nearest to the impeller 160, with angled surfaces that extend outward at an included angle 174 toward the collector 116. The radius R4 improves the efficiency of the nozzle formed by slot 126. The radius R4 of edges 124U and 124L induces the “Coandă effect,” wherein a flowing gas will tend to follow a curved surface more readily than a sharp edge, in the gas flowing through the slot 126. This redirection of the gas flowing through the slot 126 produces a smoother transition of flow and pressure with lower loss and reduced audible noise. In certain embodiments, R4 may be within the range of 0.01-0.30 inch. In certain embodiments, R4 may be approximately 0.020 inch.


In this example, the reference line 170 is aligned with the peak of the radius R4 of lower edge 124L and the reference line 172 is aligned with the peak of the radius R4 of upper edge 124U. Thus, the slot 126 is defined by the reference lines 170, 172. In this example, the shaped surface 166 at the outside edge 162 is aligned with reference line 170, i.e. the lower edge 124L of the slot 126, and the top surfaces 176 of the plurality of blades 170, 171 are each aligned with the reference line 172, i.e. the upper edge 124U of the slot 126.


The gap between the top surface 176 and the upper inner surface 123 of the upper housing 112T is a path of potential backflow from the edge 162 of the impeller 160 toward the center. Minimizing the gap 183 between top surface 176 and the upper inner surface 123 reduces this backflow and thereby improves the pressure recovery of the blower 100. In certain embodiments, the gap 183 may be in the range of 0.002-0.150 inch when the impeller 160 is stationary relative to the housing 112. In certain embodiments, the gap 183 may be in the range of 0.005-0.050 inch. In certain embodiments, the gap 180 may be approximately 0.010 inch.


The lower edge 124L has an adjacent wall 120 with a gap 180 between the outside edge 162 and the wall 120. In certain embodiments, the gap 180 may be in the range of 0.0035-0.110 inch when the impeller 160 is stationary relative to the housing 112. In certain embodiments, the gap 180 may be in the range of 0.005-0.050 inch. In certain embodiments, the gap 180 may be approximately 0.0073 inch. In certain embodiments, the radius R2 of the outside edge 162 of the impeller 160 may increase as the rotational velocity of the impeller 160 increases and, therefore, the gap 180 may be reduced when the impeller 160 is rotating relative to the housing 112. In certain embodiments, the impeller 160 may rotate at a rotational velocity of up to 60,000 rotations per minute (rpm) relative to the housing 112 and the gap may be reduced to as little as 0.003 inch. As there will be a boundary layer (not visible in FIG. 8) attached to each of the wall 120 and the outside edge 162, reducing this gap may decrease the portion of the gap wherein airflow may go turbulent, e.g. the portion between the two boundary layers, thereby reducing the acoustic energy generated by the turbulent air.


The wall 120 connects to a shelf 122. There is a gap 182 between the bottom surface 167 of the impeller 160 and the shelf 122 of the bottom housing portion 112B. In certain embodiments, the gap 182 may be less than or equal to 0.020 inch when the impeller 160 is stationary or moving relative to the housing 112B. In certain embodiments, the gap 182 may be less than or equal to 0.050 inch. In certain embodiments, the gap 182 may be less than or equal to 0.020 inch.



FIGS. 9A-9C are perspective views of the overmolded top housing 112T according to certain aspects of the present disclosure. FIG. 9A depicts a translucent view of a layer 200 of a sound-damping material formed so as to match the external profile of a housing shell 210 shown in FIG. 9B. In this example, the sound-damping layer 200 covers most of the external surface of the housing shell 210 with the exception of the attachment points 212 for the clips 114 (not shown in FIGS. 9A-9C). FIG. 9C shows combined top housing portion 112T with the sound-damping layer 200 on the external surface of the housing shell 210.


In certain embodiments, the sound-damping layer 200 comprises an elastomer, e.g. a silicone or rubber, having poor acoustic transmissibility. In certain embodiments, the sound-damping layer 200 may be overmolded on the housing shell 210. In certain embodiments, the sound-damping layer 200 may be applied to the housing shell 210 by one or more of the processes of transfer molding, spraying, dipping, brushing, curtain coating, or other manual or automated coating application process. In certain embodiments, the sound-damping layer 200 may comprise high-density particles, e.g. steel, that may further reduce the transmissibility of the sound-damping layer 200.


It can be seen that the disclosed embodiments of the blower may provide advantages in size, cost, performance, and reduced noise during operation. The shaping of the leading and trailing surfaces of the vanes near the outside edge of the impeller may reduce the turbulence and velocity gradient in the air flow around the tip of the vanes, thereby reducing the acoustic noise generated by the air flow. The small clearances between portions of the impeller and portions of the housing may further reduce the acoustic noise by decreasing the gaps compared to the depth of the boundary layers, thereby reducing the portion of the gap susceptible to noisy, turbulent flow.


The previous description is provided to enable any person skilled in the art to practice the various aspects described herein. While the foregoing has described what are considered to be the best mode and/or other examples, it is understood that various modifications to these aspects will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other aspects. Thus, the claims are not intended to be limited to the aspects shown herein, but is to be accorded the full scope consistent with the language claims, wherein reference to an element in the singular is not intended to mean “one and only one” unless specifically so stated, but rather “one or more.” Unless specifically stated otherwise, the terms “a set” and “some” refer to one or more. Pronouns in the masculine (e.g., his) include the feminine and neuter gender (e.g., her and its) and vice versa. Headings and subheadings, if any, are used for convenience only and do not limit the invention.


It is understood that the specific order or hierarchy of steps in the processes disclosed is an illustration of exemplary approaches. Based upon design preferences, it is understood that the specific order or hierarchy of steps in the processes may be rearranged. Some of the steps may be performed simultaneously. The accompanying method claims present elements of the various steps in a sample order, and are not meant to be limited to the specific order or hierarchy presented.


Terms such as “top,” “bottom,” “front,” “rear” and the like as used in this disclosure should be understood as referring to an arbitrary frame of reference, rather than to the ordinary gravitational frame of reference. Thus, a top surface, a bottom surface, a front surface, and a rear surface may extend upwardly, downwardly, diagonally, or horizontally in a gravitational frame of reference.


A phrase such as an “aspect” does not imply that such aspect is essential to the subject technology or that such aspect applies to all configurations of the subject technology. A disclosure relating to an aspect may apply to all configurations, or one or more configurations. A phrase such as an aspect may refer to one or more aspects and vice versa. A phrase such as an “embodiment” does not imply that such embodiment is essential to the subject technology or that such embodiment applies to all configurations of the subject technology. A disclosure relating to an embodiment may apply to all embodiments, or one or more embodiments. A phrase such an embodiment may refer to one or more embodiments and vice versa.


The word “exemplary” is used herein to mean “serving as an example or illustration.” Any aspect or design described herein as “exemplary” is not necessarily to be construed as preferred or advantageous over other aspects or designs.


All structural and functional equivalents to the elements of the various aspects described throughout this disclosure that are known or later come to be known to those of ordinary skill in the art are expressly incorporated herein by reference and are intended to be encompassed by the claims. Moreover, nothing disclosed herein is intended to be dedicated to the public regardless of whether such disclosure is explicitly recited in the claims. No claim element is to be construed under the provisions of 35 U.S.C. § 112, sixth paragraph, unless the element is expressly recited using the phrase “means for” or, in the case of a method claim, the element is recited using the phrase “step for.” Furthermore, to the extent that the term “include,” “have,” or the like is used in the description or the claims, such term is intended to be inclusive in a manner similar to the term “comprise” as “comprise” is interpreted when employed as a transitional word in a claim.

Claims
  • 1. A blower comprising: an impeller comprising:an impeller plate having a top surface; anda plurality of blades each attached to the impeller plate and comprising a top surface, a tip, and a leading surface, the leading surface comprising a first portion proximate to the tip, having a first radius; anda housing comprising:an impeller cavity, wherein the impeller plate is disposed within the impeller cavity;a collector; anda slot between the impeller cavity and the collector, the slot having an upper edge and a lower edge, wherein the upper and lower edges of the slot each comprises a respective inclined surface extending from the respective edge toward the collector and an inside rounded comer nearest the impeller, the inclined surfaces disposed relative to each other such that a distance between the inclined surfaces increases as the inclined surfaces extend away from the impeller;wherein the top surface of the impeller plate is aligned with the lower edge of the slot and the top surface of the plurality of blades is aligned with the upper edge of the slot.
  • 2. The blower of claim 1, wherein the plurality of blades comprises a tip and leading surface that comprises a first portion proximate to the tip, the first portion having a first radius, the first radius being within a range of 0.14-0.16 inch.
  • 3. The blower of claim 1, wherein: the impeller plate comprises an outside edge with a second radius; the tip is coincident with the outside edge of the impeller plate;the leading surface comprises a second portion disposed between the tip and the first portion; andthe second portion of the leading surface comprises the second radius.
  • 4. The blower of claim 1, wherein the inclined surfaces are disposed relative to each other at an angle within a range of 10-40 degrees.
  • 5. The blower of claim 1, wherein: the impeller cavity further comprises an upper inner surface;each blade comprises a top surface; anda gap between the top surface of the plurality of blades, at the tip of the respective blade and the upper inside surface of the impeller cavity is within a range of .005-0.050 inch.
  • 6. The blower of claim 1, wherein: the housing comprises an inside wall that is proximate to an outside edge of the impeller plate; and a gap between the inside wall and the outside edge is in a range of0.035-0.110 inch when the impeller is stationary.
  • 7. The blower of claim 1, wherein: the housing comprises a shelf;the impeller plate further comprises a bottom surface proximate to an outside edge of the impeller plate and disposed over a portion of the shelf; anda gap between the bottom surface of the impeller plate and the shelf of the housing is less than or equal to 0.050 inch.
  • 8. The blower of claim 1, further comprising a sound-damping layer disposed on a portion of the housing.
  • 9. The blower of claim 8, wherein the sound-damping layer comprises a layer disposed on an external surface of the housing over the collector and impeller cavity.
  • 10. The blower of claim 8, wherein the sound-damping layer comprising an elastomer.
  • 11. The blower of claim 1, wherein the collector is formed as a volute.
  • 12. The blower of claim 1, wherein the impeller is formed as a centrifugal impeller.
  • 13. The blower of claim 12, wherein: the top surface of each of the plurality of blades comprises a centerline from the tip of the respective blade to an inlet end of the respective blade; andeach of the plurality of blades comprises a maximum width that is measured perpendicular to the centerline and intersects the first portion of the leading surface.
  • 14. The blower of claim 13, wherein: each of the plurality of blades comprises an initial width proximate to the inlet end of the respective blade; andthe maximum width of each blade is at least twice the initial width of the respective blade.
  • 15. A blower comprising: an impeller comprising:an impeller plate having a top surface; anda plurality of blades, each attached to the impeller plate, and having a distal end extending away from the tope surface of the impeller plate; and a housing comprising:an impeller cavity, wherein the impeller plate is disposed within the impeller cavity;a collector; anda slot between the impeller cavity and the collector, the slot having an upper edge and a lower edge, wherein the upper and lower edges of the slot each comprises a respective inclined surface extending from the respective edge toward the collector and an inside rounded comer nearest the impeller having a radius within the range of 0.01-0.30 inches, the inclined surfaces disposed relative to each other such that a distance between the inclined surfaces increases as the inclined surfaces extend away from the impeller;wherein the top surface of the impeller plate is aligned with the lower edge of the slot and the distal end of the plurality of blades is aligned with the upper edge of the slot.
  • 16. The blower of claim 15, wherein the inclined surfaces are disposed relative to each other at an angle within a range of 10-40 degrees.
  • 17. The blower of claim 15, wherein: the housing comprises an inside wall that is proximate to an outside edge of the impeller plate; and a gap between the inside wall and the outside edge is in a range of0.035-0.110 inch when the impeller is stationary.
  • 18. The blower of claim 15, wherein: the housing comprises a shelf;the impeller plate further comprises a bottom surface proximate to an outside edge of the impeller plate and disposed over a portion of the shelf; anda gap between the bottom surface of the impeller plate and the shelf of the housing is less than or equal to 0.050 inch.
  • 19. The blower of claim 15, further comprising a sound-damping layer disposed on a portion of the housing.
  • 20. The blower of claim 19, wherein the sound-damping layer comprises a layer disposed on an external surface of the housing over the collector and impeller cavity.
CROSS-REFERENCES TO RELATED APPLICATIONS

The present application claims the benefit of priority under 35 U.S.C. § 120 as a continuation from U.S. patent application Ser. No. 13/931,465 entitled “LOW-NOISE BLOWER,” filed on Jun. 28, 2013, the disclosure of which is hereby incorporated by reference in its entirety for all purposes.

US Referenced Citations (118)
Number Name Date Kind
2037880 Charavay Apr 1936 A
2510125 Meakin Jun 1950 A
2634311 Darling Apr 1953 A
2811107 Brill Oct 1957 A
2898031 Voigt Aug 1959 A
3140042 Noriyoshi Jul 1964 A
3150823 Adams Sep 1964 A
3673541 Volinskie Jun 1972 A
3776215 Howard et al. Dec 1973 A
3788765 Rusak Jan 1974 A
4167369 Ishihara Sep 1979 A
4243357 Flynn et al. Jan 1981 A
4381668 Sato et al. May 1983 A
4543041 French et al. Sep 1985 A
4562744 Hall et al. Jan 1986 A
4571801 Ewing Feb 1986 A
4645419 Furuya Feb 1987 A
4649760 Wedding Mar 1987 A
4754651 Shortridge et al. Jul 1988 A
4763645 Kapp Aug 1988 A
4809742 Grau Mar 1989 A
4825904 Grau et al. May 1989 A
4909545 Hohol Mar 1990 A
4978281 Conger, IV Dec 1990 A
5064346 Atarashi et al. Nov 1991 A
5127400 DeVries et al. Jul 1992 A
5190068 Philbin Mar 1993 A
5265594 Olsson et al. Nov 1993 A
5277196 Hankinson et al. Jan 1994 A
5295397 Hall et al. Mar 1994 A
5331995 Westfall et al. Jul 1994 A
5339807 Carter Aug 1994 A
5365795 Brower, Jr. Nov 1994 A
5461932 Hall et al. Oct 1995 A
5478206 Prahst Dec 1995 A
5537992 Bjoernstijerna et al. Jul 1996 A
5572992 Kankkunen et al. Nov 1996 A
5604681 Koeninger Feb 1997 A
5606236 Tennies et al. Feb 1997 A
5771884 Yarnall et al. Jun 1998 A
5918596 Heinonen Jul 1999 A
5954051 Heinonen et al. Sep 1999 A
6017315 Starr et al. Jan 2000 A
6139262 Ravidranath Oct 2000 A
6151557 Broden et al. Nov 2000 A
6422092 Morrison et al. Jul 2002 B1
6422256 Balazy et al. Jul 2002 B1
6553923 Gatley, Jr. Apr 2003 B2
6578818 Krimmer et al. Jun 2003 B1
6609431 Tietsworth et al. Aug 2003 B1
6622724 Truitt et al. Sep 2003 B1
6820620 Rochat Nov 2004 B2
6945123 Kuehl et al. Sep 2005 B1
7107834 Meneghini et al. Sep 2006 B2
7121139 Shajii et al. Oct 2006 B2
7636640 Wang et al. Dec 2009 B2
7819022 Hope Oct 2010 B2
7826986 McDonald Nov 2010 B2
8504318 Mendelson et al. Aug 2013 B2
9003877 Qasimi et al. Apr 2015 B2
9541098 Duquette Jan 2017 B2
20020085952 Ellingboe et al. Jul 2002 A1
20020198668 Lull et al. Dec 2002 A1
20030106554 de Silva et al. Jun 2003 A1
20030220605 Bowman et al. Nov 2003 A1
20040074311 Lull et al. Apr 2004 A1
20040177703 Schumacher et al. Sep 2004 A1
20040187871 Kimmel et al. Sep 2004 A1
20050004534 Lockwood et al. Jan 2005 A1
20050241412 Tison et al. Nov 2005 A1
20060079765 Neer et al. Apr 2006 A1
20060144163 Friberg Jul 2006 A1
20060162466 Wargo et al. Jul 2006 A1
20060236781 Ohmi et al. Oct 2006 A1
20070193369 Evans et al. Aug 2007 A1
20070265877 Rice et al. Nov 2007 A1
20070277824 Aylsworth et al. Dec 2007 A1
20080059084 Wang et al. Mar 2008 A1
20080092891 Cewers Apr 2008 A1
20080105259 de Silva et al. May 2008 A1
20080283062 Esposito, Jr. Nov 2008 A1
20090038615 Bradley Feb 2009 A1
20090093774 Wang et al. Apr 2009 A1
20090095068 Redemann et al. Apr 2009 A1
20090113996 Wang et al. May 2009 A1
20090293634 Ong Dec 2009 A1
20090326839 Rogers et al. Dec 2009 A1
20100031737 Saito et al. Feb 2010 A1
20100139660 Adahan Jun 2010 A1
20100229967 Yasuda et al. Sep 2010 A1
20100236552 Kwok et al. Sep 2010 A1
20100307490 Broborg et al. Dec 2010 A1
20110100364 Faram May 2011 A1
20110126834 Winter et al. Jun 2011 A1
20110126837 Winter et al. Jun 2011 A1
20110301867 Davis et al. Dec 2011 A1
20120065533 Carrillo, Jr. et al. Mar 2012 A1
20120085349 Tobias et al. Apr 2012 A1
20120185102 Skoglund et al. Jul 2012 A1
20120204874 Sofranko Aug 2012 A1
20120226449 Delache et al. Sep 2012 A1
20120229272 Jacob et al. Sep 2012 A1
20120285454 Nibu et al. Nov 2012 A1
20120285455 Varga et al. Nov 2012 A1
20120318383 Yasuda et al. Dec 2012 A1
20130036806 Kohno Feb 2013 A1
20130079667 Berkcan et al. Mar 2013 A1
20130153040 Goto et al. Jun 2013 A1
20130220314 Bottom Aug 2013 A1
20130247905 Miller et al. Sep 2013 A1
20140054479 Shen Feb 2014 A1
20140066880 Prince et al. Mar 2014 A1
20140182590 Platt et al. Jul 2014 A1
20140251322 Miller Sep 2014 A1
20150020807 Kimmel Jan 2015 A1
20150096560 Klenner et al. Apr 2015 A1
20150143921 Postberg et al. May 2015 A1
20160256646 Vazales Sep 2016 A1
Foreign Referenced Citations (27)
Number Date Country
1041204 Apr 1990 CN
101225881 Jul 2008 CN
101687086 Mar 2010 CN
102155570 Aug 2011 CN
202366282 Aug 2012 CN
102686888 Sep 2012 CN
102927292 Feb 2013 CN
102954014 Mar 2013 CN
103041492 Apr 2013 CN
202870631 Apr 2013 CN
0072177 Feb 1983 EP
0829793 Mar 1998 EP
1127583 Aug 2001 EP
1658874 May 2006 EP
2402616 Jan 2012 EP
S5659 Jan 1981 JP
S5841299 Mar 1983 JP
H01318798 Dec 1989 JP
2004027919 Jan 2004 JP
2004308442 Nov 2004 JP
2006342690 Dec 2006 JP
4703272 Jun 2011 JP
528837 Apr 2003 TW
WO-0138832 May 2001 WO
WO-2006024532 Mar 2006 WO
WO-2011055254 May 2011 WO
WO-2013002699 Jan 2013 WO
Non-Patent Literature Citations (24)
Entry
Australian Examination Report No. 1 for Application No. 2014302307, dated Feb. 8, 2018, 3 pages.
Japanese Office Action for Application No. 2016-524219, dated May 29, 2018, 11 pages.
Chinese Office Action for Application No. 201480036971.X, dated Jun. 5, 2017, 5 pages excluding translation.
Chinese Office Action for Application No. 201480036606.9, dated Sep. 2, 2016, 6 pages excluding translation.
Chinese Office Action for Application No. 201480036971.X, dated Oct. 8, 2016, 10 pages excluding English translation.
Chinese Office Action for Application No. 201480037090.X, dated Sep. 26, 2016, 6 pages excluding English translation.
Chinese Office Action for Application No. 201480037104.8, dated Nov. 17, 2016, 5 pages excluding English translation.
International Search Report and Written Opinion for Application No. PCT/US2015/038155, dated Dec. 17, 2015, 18 pages.
International Search Report and Written Opinion for Application No. PCT/US2015/038157, dated Nov. 5, 2015, 12 pages.
International Search Report and Written Opinion for International Application No. PCT/US2014/044737, dated May 19, 2015, 18 pages.
International Search Report and Written Opinion in PCT Application No. PCT/US2014/044438 dated Oct. 28, 2014, 11 pages.
International Search Report and Written Opinion in PCT Application No. PCT/US2014/044441 dated Oct. 31, 2014, 12 pages.
International Search Report and Written Opinion in PCT Application No. PCT/US2014/044442 dated Nov. 3, 2014, 10 pages.
International Search Report and Written Opinion in PCT Application No. PCT/US2014/044724 dated Oct. 21, 2014, 12 pages.
International Search Report for International Application No. PCT/US2014/044743, dated Jan. 22, 2015, 6 pages.
Invitation to Pay Additional Fees and Partial Search Report for Application No. PCT/US2015/038155, dated Oct. 7, 2015, 7 pages.
Invitation to Pay Additional Fees in International Application No. PCT/US2014/044737 dated Oct. 28, 2014, 7 pages.
Invitation to Pay Additional Fees in PCT Application No. PCT/US2014/044743 dated Oct. 21, 2014, 7 pages.
Chinese Office Action for Application No. 201711250360.7, dated Jan. 4, 2019, 13 pages.
Chinese Office Action for Application No. 201711250360.7, dated May 30, 2019, 13 pages.
European Office Action for Application No. 14742084.8, dated May 3, 2019, 4 pages.
India Office Action for Application No. 4130/KOLNP/2015, dated Jul. 30, 2019, 6 pages.
Chinese Office Action for Application No. 201711250360.7, dated Sep. 3, 2019, 14 pages.
India Office Action for Application No. 4209/KOLNP/2015, dated Sep. 6, 2019, 7 pages.
Related Publications (1)
Number Date Country
20170114801 A1 Apr 2017 US
Continuations (1)
Number Date Country
Parent 13931465 Jun 2013 US
Child 15402126 US