This patent application incorporates by reference in its entirety nonprovisional U.S. patent application Ser. No. 13/609,349 titled “Method Of Reducing Air Compressor Noise” filed Sep. 11, 2012, which issued as U.S. Pat. No. 10,871,153 on Dec. 22, 2020. This patent application incorporates by reference in its entirety U.S. provisional patent application No. 61/533,993 titled “Air Ducting Shroud For Cooling An Air Compressor Pump And Motor” filed on Sep. 13, 2011. This patent application incorporates by reference in its entirety U.S. provisional patent application No. 61/534,001 titled “Shroud For Capturing Fan Noise” filed on Sep. 13, 2011. This patent application incorporates by reference in its entirety U.S. provisional patent application No. 61/534,009 titled “Method Of Reducing Air Compressor Noise” filed on Sep. 13, 2011. This patent application incorporates by reference in its entirety U.S. provisional patent application No. 61/534,015 titled “Tank Dampening Device” filed on Sep. 13, 2011. This patent application incorporates by reference in its entirety U.S. provisional patent application No. 61/534,046 titled “Compressor Intake Muffler And Filter” filed on Sep. 13, 2011.
The invention relates to a compressor for air, gas or gas mixtures.
Compressors are widely used in numerous applications. Existing compressors can generate a high noise output during operation. This noise can be annoying to users and can be distracting to those in the environment of compressor operation. Non-limiting examples of compressors which generate unacceptable levels of noise output include reciprocating, rotary screw and rotary centrifugal types. Compressors which are mobile or portable and not enclosed in a cabinet or compressor room can be unacceptably noisy. However, entirely encasing a compressor, for example in a cabinet or compressor room, is expensive, prevents mobility of the compressor and is often inconvenient or not feasible. Additionally, such encasement can create heat exchange and ventilation problems. There is a strong and urgent need for a quieter compressor technology.
When a power source for a compressor is electric, gas or diesel, unacceptably high levels of unwanted heat and exhaust gases can be produced. Additionally, existing compressors can be inefficient in cooling a compressor pump and motor. Existing compressors can use multiple fans, e.g. a compressor can have one fan associated with a motor and a different fan associated with a pump. The use of multiple fans adds cost manufacturing difficulty, noise and unacceptable complexity to existing compressors. Current compressors can also have improper cooling gas flow paths which can choke cooling gas flows to the compressor and its components. Thus, there is a strong and urgent need for a more efficient cooling design for compressors.
In an embodiment, the compressor assembly disclosed herein can have a tank seal which seals a tank gap between a portion of a housing of the compressor assembly and a portion of a compressed gas tank; and a sound level of the compressor assembly which is in a range of from 65 dBA to 75 dBA when the compressor assembly is in a compressing state.
The compressor assembly can have a difference in sound level between a location at a pump assembly side of the tank seal and the outside of the tank seal is in a range of from about 2 dBA to about 10 dBA. The compressor assembly can have a difference in sound level between a location at a pump assembly side of the tank seal and the outside of the tank seal is in a range of from about 2 dBA to about 8 dBA. The compressor assembly can have a difference in sound level between a location at a pump assembly side of the tank seal and the outside of the tank seal is in a range of from about 2.5 dBA to about 5 dBA. The compressor assembly can have a difference in sound level between a location at a pump assembly side of the tank seal and the outside of the tank seal is in a range of from about 5 dBA to about 8 dBA. The compressor assembly can have a difference in sound level between a location at a pump assembly side of the tank seal and the outside of the tank seal is about 2.5 dBA. The compressor assembly can have a difference in sound level between a location at a pump assembly side of the tank seal and the outside of the tank seal is about 5.0 dBA. The compressor assembly can have a difference in sound level between a location at a pump assembly side of the tank seal and the outside of the tank seal is about 8.0 dBA.
The compressor assembly can have a tank seal having a seal bulb. The compressor assembly can have a tank seal having a housing seal. The compressor assembly can have a tank seal having a seal hook. The compressor assembly can have a tank seal having a seal rib. The compressor assembly can have a tank seal having seal bulb which can be compressed.
In an aspect, the compressor assembly disclose herein can control the sound level of the compressor assembly by a method having the steps of: providing a compressor assembly having a housing; providing a compressed gas tank; configuring the housing and compressed gas tank to have tank gap between the housing and the compressed gas tank; providing a tank seal; and sealing the tank gap with the tank seal.
The method for controlling having the step of operating the compressor assembly in a compressing state at a sound level in a range of between 65 dBA and 75 dBA. The method for controlling the sound level of a compressor assembly having the steps of operating the compressor assembly in a compressing state at a sound level in a range of between 65 dBA and 75 dBA, and compressing 2.4 SCFM to 3.5 SCFM of gas.
The method for controlling the sound level of a compressor assembly according to claim 13, further having the steps of operating the compressor assembly in a compressing state at a sound level in a range of between 65 dBA and 75 dBA, and compressing gas to a pressure of 50 PSIG to 250 PSIG.
The method for controlling the sound level of a compressor assembly can have the step of transferring heat from a pump assembly at a rate of from 60 BTU/min to 200 BTU/min.
In an aspect, the compressor assembly disclosed herein can have a means for controlling the sound level of a compressor assembly, which uses a means to seal a tank gap between at least a portion of a housing and at least a portion of a compressed gas tank and by operating the compressor assembly in a range of from 65 dBA to 75 dBA when the compressor assembly is in a compressing state. The compressor assembly can have a means for controlling the sound level of a compressor assembly, wherein a means to seal a tank gap is used which has a deformable portion.
The present invention in its several aspects and embodiments solves the problems discussed above and significantly advances the technology of compressors. The present invention can become more fully understood from the detailed description and the accompanying drawings, wherein:
Herein, like reference numbers in one figure refer to like reference numbers in another figure.
The invention relates to a compressor assembly which can compress air, or gas, or gas mixtures, and which has a low noise output, effective cooling means and high heat transfer. The inventive compressor assembly achieves efficient cooling of the compressor assembly 20 (
The compressor assembly 20 can optionally be portable. The compressor assembly 20 can optionally have a handle 29, which optionally can be a portion of frame 10.
In an embodiment, the compressor assembly 20 can have a value of weight between 15 lbs and 100 lbs. In an embodiment, the compressor assembly 20 can be portable and can have a value of weight between 15 lbs and 50 lbs. In an embodiment, the compressor assembly 20 can have a value of weight between 25 lbs and 40 lbs. In an embodiment, the compressor assembly 20 can have a value of weight of, e.g. 38 lbs, or 29 lbs, or 27 lbs, or 25 lbs, or 20 lbs, or less. In an embodiment, frame 10 can have a value of weight of 10 lbs or less. In an embodiment, frame 10 can weigh 5 lbs, or less, e.g. 4 lbs, or 3 lbs, of 2 lbs, or less.
In an embodiment, the compressor assembly 20 can have a front side 12 (“front”), a rear side 13 (“rear”), a fan side 14 (“fan-side”), a pump side 15 (“pump-side”), a top side 16 (“top”) and a bottom side 17 (“bottom”).
The compressor assembly 20 can have a housing 21 which can have ends and portions which are referenced herein by orientation consistently with the descriptions set forth above. In an embodiment, the housing 21 can have a front housing 160, a rear housing 170, a fan-side housing 180 and a pump-side housing 190. The front housing 160 can have a front housing portion 161, a top front housing portion 162 and a bottom front housing portion 163. The rear housing 170 can have a rear housing portion 171, a top rear housing portion 172 and a bottom rear housing portion 173. The fan-side housing 180 can have a fan cover 181 and a plurality of intake ports 182. The compressor assembly can be cooled by air flow provided by a fan 200 (
In an embodiment, the housing 21 can be compact and can be molded. The housing 21 can have a construction at least in part of plastic, or polypropylene, acrylonitrile butadiene styrene (ABS), metal, steel, stamped steel, fiberglass, thermoset plastic, cured resin, carbon fiber, or other material. The frame 10 can be made of metal, steel, aluminum, carbon fiber, plastic or fiberglass.
Power can be supplied to the motor of the compressor assembly through a power cord 5 extending through the fan-side housing 180. In an embodiment, the compressor assembly 20 can comprise one or more of a cord holder member, e.g. first cord wrap 6 and second cord wrap 7 (
In an embodiment, power switch 11 can be used to change the operating state of the compressor assembly 20 at least from an “on” to an “off” state, and vice versa. In an “on” state, the compressor can be in a compressing state (also herein as a “pumping state”) in which it is compressing air, or a gas, or a plurality of gases, or a gas mixture.
In an embodiment, other operating modes can be engaged by power switch 11 or a compressor control system, e.g. a standby mode, or a power save mode. In an embodiment, the front housing 160 can have a dashboard 300 which provides an operator-accessible location for connections, gauges and valves which can be connected to a manifold 303 (
In an embodiment, the pressure regulator 320 employs a pressure regulating valve. The pressure regulator 320 can be used to adjust the pressure regulating valve 26 (
In an embodiment, the pump assembly 25 and the compressed gas tank 150 can be connected to frame 10. The pump assembly 25, housing 21 and compressed gas tank 150 can be connected to the frame 10 by a plurality of screws and/or one or a plurality of welds and/or a plurality of connectors and/or fasteners.
The plurality of intake ports 182 can be formed in the housing 21 adjacent the housing inlet end 23 and a plurality of exhaust ports 31 can be formed in the housing 21. In an embodiment, the plurality of the exhaust ports 31 can be placed in housing 21 in the front housing portion 161. Optionally, the exhaust ports 31 can be located adjacent to the pump end of housing 21 and/or the pump assembly 25 and/or the pump cylinder 60 and/or cylinder head 61 (
The total cross-sectional open area of the intake ports 182 (the sum of the cross-sectional areas of the individual intake ports 182) can be a value in a range of from 3.0 in{circumflex over ( )}2 to 100 in{circumflex over ( )}2. In an embodiment, the total cross-sectional open area of the intake ports 182 can be a value in a range of from 6.0 in{circumflex over ( )}2 to 38.81 in{circumflex over ( )}2. In an embodiment, the total cross-sectional open area of the intake ports 182 can be a value in a range of from 9.8 in{circumflex over ( )}2 to 25.87 in{circumflex over ( )}2. In an embodiment, the total cross-sectional open area of the intake ports 182 can be 12.936 in{circumflex over ( )}2.
In an embodiment, the cooling gas employed to cool compressor assembly 20 and its components can be air (also known herein as “cooling air”). The cooling air can be taken in from the environment in which the compressor assembly 20 is placed. The cooling air can be ambient from the natural environment, or air which has been conditioned or treated. The definition of “air” herein is intended to be very broad. The term “air” includes breathable air, ambient air, treated air, conditioned air, clean room air, cooled air, heated air, non-flammable oxygen containing gas, filtered air, purified air, contaminated air, air with particulates solids or water, air from bone dry (i.e. 0.00 humidity) air to air which is supersaturated with water, as well as any other type of air present in an environment in which a gas (e.g. air) compressor can be used. It is intended that cooling gases which are not air are encompassed by this disclosure. For non-limiting example, a cooling gas can be nitrogen, can comprise a gas mixture, can comprise nitrogen, can comprise oxygen (in a safe concentration), can comprise carbon dioxide, can comprise one inert gas or a plurality of inert gases, or comprise a mixture of gases.
In an embodiment, cooling air can be exhausted from compressor assembly 20 through a plurality of exhaust ports 31. The total cross-sectional open area of the exhaust ports 31 (the sum of the cross-sectional areas of the individual exhaust ports 31) can be a value in a range of from 3.0 in{circumflex over ( )}2 to 100 in{circumflex over ( )}2. In an embodiment, the total cross-sectional open area of the exhaust ports can be a value in a range of from 3.0 in{circumflex over ( )}2 to 77.62 in{circumflex over ( )}2. In an embodiment, the total cross-sectional open area of the exhaust ports can be a value in a range of from 4.0 in{circumflex over ( )}2 to 38.81 in{circumflex over ( )}2. In an embodiment, the total cross-sectional open area of the exhaust ports can be a value in a range of from 4.91 in{circumflex over ( )}2 to 25.87 in{circumflex over ( )}2. In an embodiment, the total cross-sectional open area of the exhaust ports can be 7.238 in{circumflex over ( )}2.
Numeric values and ranges herein, unless otherwise stated, also are intended to have associated with them a tolerance and to account for variances of design and manufacturing, and/or operational and performance fluctuations. Thus, a number disclosed herein is intended to disclose values “about” that number. For example, a value X is also intended to be understood as “about X”. Likewise, a range of Y-Z is also intended to be understood as within a range of from “about Y-about Z”. Unless otherwise stated, significant digits disclosed for a number are not intended to make the number an exact limiting value. Variance and tolerance, as well as operational or performance fluctuations, are an expected aspect of mechanical design and the numbers disclosed herein are intended to be construed to allow for such factors (in non-limiting e.g., ±10 percent of a given value). This disclosure is to be broadly construed. Likewise, the claims are to be broadly construed in their recitations of numbers and ranges.
The compressed gas tank 150 can operate at a value of pressure in a range of at least from ambient pressure, e.g. 14.7 psig to 3000 psig (“psig” is the unit lbf/in{circumflex over ( )}2 gauge), or greater. In an embodiment, compressed gas tank 150 can operate at 200 psig. In an embodiment, compressed gas tank 150 can operate at 150 psig.
In an embodiment, the compressor has a pressure regulated on/off switch which can stop the pump when a set pressure is obtained. In an embodiment, the pump is activated when the pressure of the compressed gas tank 150 falls to 70 percent of the set operating pressure, e.g. to activate at 140 psig with an operating set pressure of 200 psig (140 psig=0.70*200 psig). In an embodiment, the pump is activated when the pressure of the compressed gas tank 150 falls to 80 percent of the set operating pressure, e.g. to activate at 160 psig with an operating set pressure of 200 psig (160 psig=0.80*200 psig). Activation of the pump can occur at a value of pressure in a wide range of set operating pressure, e.g. 25 percent to 99.5 percent of set operating pressure. Set operating pressure can also be a value in a wide range of pressure, e.g. a value in a range of from 25 psig to 3000 psig. An embodiment of set pressure can be 50 psig, 75 psig, 100 psig, 150 psig, 200 psig, 250 psig, 300 psig, 500 psig, 1000 psig, 2000 psig, 3000 psig, or greater than or less than, or a value in between these example numbers.
The compressor assembly 20 disclosed herein in its various embodiments achieves a reduction in the noise created by the vibration of the air tank while the air compressor is running, in its compressing state (pumping state) e.g. to a value in a range of from 60-75 dBA, or less, as measured by ISO3744-1995. Noise values discussed herein are compliant with ISO3744-1995. ISO3744-1995 is the standard for noise data and results for noise data, or sound data, provided in this application. Herein “noise” and “sound” are used synonymously.
The pump assembly 25 can be mounted to an air tank and can be covered with a housing 21. A plurality of optional decorative shapes 141 can be formed on the front housing portion 161. The plurality of optional decorative shapes 141 can also be sound absorbing and/or vibration dampening shapes. The plurality of optional decorative shapes 141 can optionally be used with, or contain at least in part, a sound absorbing material.
The compressor assembly 20 can include a pump assembly 25. In an embodiment, pump assembly 25 which can compress a gas, air or gas mixture. In an embodiment in which the pump assembly 25 compresses air, it is also referred to herein as air compressor 25, or compressor 25. In an embodiment, the pump assembly 25 can be powered by a motor 33 (e.g.
Air ducting shroud 485 can have a shroud inlet scoop 484. As illustrated in
As shown in
The piston 63 can be formed as an integral part of the connecting rod 69. A compression seal can be attached to the piston 63 by a retaining ring and a screw. In an embodiment, the compression seal can be a sliding compression seal.
A cooling gas stream, such as cooling air stream 2000 (
In an embodiment, one fan can be used to cool both the pump and motor. A design using a single fan to provide cooling to both the pump and motor can require less air flow than a design using two or more fans, e.g. using one or more fans to cool the pump, and also using one or more fans to cool the motor. Using a single fan to provide cooling to both the pump and motor can reduce power requirements and also reduces noise production as compared to designs using a plurality of fans to cool the pump and the motor, or which use a plurality of fans to cool the pump assembly 25, or the compressor assembly 20.
In an embodiment, the fan blade 205 (e.g.
In an embodiment, the outlet pressure of cooling air from the fan can be in a range of from 1 psig to 50 psig. In an embodiment, the fan 200 can be a low flow fan with which generates an outlet pressure having a value in a range of from 1 in of water to 10 psi. In an embodiment, the fan 200 can be a low flow fan with which generates an outlet pressure having a value in a range of from 2 in of water to 5 psi.
In an embodiment, the air ducting shroud 485 can flow 100 CFM of cooling air with a pressure drop of from 0.0002 psi to 50 psi along the length of the air ducting shroud. In an embodiment, the air ducting shroud 485 can flow 75 CFM of cooling air with a pressure drop of 0.028 psi along its length as measured from the entrance to fan 200 through the exit from conduit 253 (
In an embodiment, the air ducting shroud 485 can flow 75 CFM of cooling air with a pressure drop of 0.1 psi along its length as measured from the outlet of fan 200 through the exit from conduit 253. In an embodiment, the air ducting shroud 485 can flow 100 CFM of cooling air with a pressure drop of 1.5 psi along its length as measured from the outlet of fan 200 through the exit from conduit 253. In an embodiment, the air ducting shroud 485 can flow 150 CFM of cooling air with a pressure drop of 5.0 psi along its length as measured from the outlet of fan 200 through the exit from conduit 253.
In an embodiment, the air ducting shroud 485 can flow 75 CFM of cooling air with a pressure drop in a range of from 1.0 psi to 30 psi across as measured from the outlet of fan 200 across the motor 33.
Depending upon the compressed gas (e.g. compressed air 999) output, the design rating of the motor 33 and the operating voltage, in an embodiment the motor 33 can operate at a value of rotation (motor speed) between 5,000 rpm and 20,000 rpm. In an embodiment, the motor 33 can operate at a value in a range of between 7,500 rpm and 12,000 rpm. In an embodiment, the motor 33 can operate at e.g. 11,252 rpm, or 11,000 rpm; or 10,000 rpm; or 9,000 rpm; or 7,500; or 6,000 rpm; or 5,000 rpm. The pulley 66 and the sprocket 49 can be sized to achieve reduced pump speeds (also herein as “reciprocation rates”, or “piston speed”) at which the piston 63 is reciprocated. For example, if the sprocket 49 can have a diameter of 1 in and the pulley 66 can have a diameter of 4 in, then a motor 33 speed of 14,000 rpm can achieve a reciprocation rate, or a piston speed, of 3,500 strokes per minute. In an embodiment, if the sprocket 49 can have a diameter of 1.053 in and the pulley 66 can have a diameter of 5.151 in, then a motor 33 speed of 11,252 rpm can achieve a reciprocation rate, or a piston speed (pump speed), of 2,300 strokes per minute.
The motor can have a stator 37 with an upper pole 38 around which upper stator coil 40 is wound and/or configured. The motor can have a stator 37 with a lower pole 39 around which lower stator coil 41 is wound and/or configured. A shaft 43 can be supported adjacent a first shaft end 44 by a bearing 45 and is supported adjacent to a second shaft end 46 by a bearing 47. A plurality of fan blades 205 can be secured to the fan 200 which can be secured to the first shaft end 44. When power is applied to the motor 33, the shaft 43 rotates at a high speed to in turn drive the sprocket 49 (
The compressor assembly 20 can be designed to accommodate a variety of types of motor 33. The motors 33 can come from different manufacturers and can have horsepower ratings of a value in a wide range from small to very high. In an embodiment, a motor 33 can be purchased from the existing market of commercial motors. For example, although the housing 21 is compact, in an embodiment it can accommodate a universal motor, or other motor type, rated, for example, at ½ horsepower, at ¾ horsepower or 1 horsepower by scaling and/or designing the air ducting shroud 485 to accommodate motors in a range from small to very large.
In one embodiment, the pump 59 such as “gas pump” or “air pump” can have a piston 63, a pump cylinder 60, in which a piston 63 reciprocates and a cylinder rod 69 (
A stroke having a value in a range of from 0.50 in and 12 in, or larger can be used. A stroke having a value in a range of from 1.5 in and 6 in can be used. A stroke having a value in a range of from 2 in and 4 in can be used. A stroke of 2.5 in can be used. In an embodiment, the stroke can be calculated to equal two (2) times the offset, for example, an offset 880 of 0.796 produces a stroke of 2(0.796)=1.592 in. In another example, an offset 880 of 2.25 produces a stroke of 2(2.25)=4.5 in. In yet another example, an offset 880 of 0.5 produces a stroke of 2(0.5)=1.0 in.
The compressed air passes through valve plate assembly 62 and into the cylinder head 61 having a plurality of cooling fins 89. The compressed gas, is discharged from the cylinder head 61 through the outlet line 145 which feeds compressed gas to the compressed gas tank 150.
The filter distance 1952 between an inlet centerline 1950 of the feed air port 952 and a scoop inlet 1954 of shroud inlet scoop 484 can vary widely and have a value in a range of from 0.5 in to 24 in, or even greater for larger compressor assemblies. The filter distance 1952 between inlet centerline 1950 and inlet cross-section of shroud inlet scoop 484 identified as scoop inlet 1954 can be e.g. 0.5 in, or 1.0 in, or 1.5 in, or 2.0 in, or 2.5 in, or 3.0 in, or 4.0 in, or 5.0 in or 6.0 in, or greater. In an embodiment, the filter distance 1952 between inlet centerline 1950 and inlet cross-section of shroud inlet scoop 484 identified as scoop inlet 1954 can be 1.859 in. In an embodiment, the inertia filter can have multiple inlet ports which can be located at different locations of the air ducting shroud 485. In an embodiment, the inertial filter is separate from the air ducting shroud and its feed is derived from one or more inlet ports.
In an embodiment, the rim 187 can extend past the air inlet space 184 and overlaps at least a portion of the shroud inlet scoop 484. In an embodiment, the rim 187 does not extend past and does not overlap a portion of the shroud inlet scoop 484 and the air inlet space 184 can have a width between the rim 187 and a portion of the shroud inlet scoop 484 having a value of distance in a range of from 0.1 in to 2 in, e.g. 0.25 in, or 0.5 in. In an embodiment, the air ducting shroud 485 and/or the shroud inlet scoop 484 can be used to block line of sight to the fan 200 and the pump assembly 25 in conjunction with or instead of the rim 187.
The inertia filter 949 can provide advantages over the use of a filter media which can become plugged with dirt and/or particles and which can require replacement to prevent degrading of compressor performance. Additionally, filter media, even when it is new, creates a pressure drop and can reduce compressor performance.
Air must make a substantial change in direction from the flow of cooling air to become compressed gas feed air to enter and pass through the feed air port 952 to enter the air intake path 922 from the inertia filter chamber 950 of the inertia filter 949. Any dust and other particles dispersed in the flow of cooling air have sufficient inertia that they tend to continue moving with the cooling air rather than change direction and enter the air intake path 922.
Pump assembly 25 can have a motor 33 which can drive the shaft 43 which causes a sprocket 49 to drive a drive belt 65 to rotate a pulley 66. The pulley 66 can be connected to and can drive the connecting rod 69 which has a piston 63 (
The valve plate assembly 62 of the pump assembly 25 can include air intake and air exhaust valves. The valves can be of a reed, flapper, one-way or other type. A restrictor can be attached to the valve plate adjacent the intake valve. Deflection of the exhaust valve can be restricted by the shape of the cylinder head which can minimize valve impact vibrations and corresponding valve stress.
The valve plate assembly 62 has a plurality of intake ports 103 (five shown) which can be closed by the intake valves 96 (
The compressor assembly 20 achieves efficient heat transfer. The heat transfer rate can have a value in a range of from 25 BTU/min to 1000 BTU/min. The heat transfer rate can have a value in a range of from 90 BTU/min to 500 BTU/min. In an embodiment, the compressor assembly 20 can exhibit a heat transfer rate of 200 BTU/min. The heat transfer rate can have a value in a range of from 50 BTU/min to 150 BTU/min. In an embodiment, the compressor assembly 20 can exhibit a heat transfer rate of 135 BTU/min. In an embodiment, the compressor assembly 20 exhibited a heat transfer rate of 84.1 BTU/min.
The heat transfer rate of a compressor assembly 20 can have a value in a range of 60 BTU/min to 110 BTU/min. In an embodiment of the compressor assembly 20, the heat transfer rate can have a value in a range of 66.2 BTU/min to 110 BTU/min; or 60 BTU/min to 200 BTU/min.
The compressor assembly 20 can have noise emissions reduced by e.g., slower fan and/or slower motor speeds, use of a check valve muffler, use of tank vibration dampeners, use of tank sound dampeners, use of a tank dampening ring, use of tank vibration absorbers to dampen noise to and/or from the tank walls which can reduce noise. In an embodiment, a two stage intake muffler can be used on the pump. A housing having reduced or minimized openings can reduce noise from the compressor assembly. As disclosed herein, the elimination of line of sight to the fan and other components as attempted to be viewed from outside of the compressor assembly 20 can reduce noise generated by the compressor assembly. Additionally, routing cooling air through ducts, using foam lined paths and/or routing cooling air through tortuous paths can reduce noise generation by the compressor assembly 20.
Additionally, noise can be reduced from the compressor assembly 20 and its sound level lowered by one or more of the following, employing slower motor speeds, using a check valve muffler and/or using a material to provide noise dampening of the housing 21 and its partitions and/or the compressed air tank 150 heads and shell. Other noise dampening features can include one or more of the following and be used with or apart from those listed above, using a two-stage intake muffler in the feed to a feed air port 952, elimination of line of sight to the fan and/or other noise generating parts of the compressor assembly 20, a quiet fan design and/or routing cooling air routed through a tortuous path which can optionally be lined with a sound absorbing material, such as a foam. Optionally, fan 200 can be a fan which is separate from the shaft 43 and can be driven by a power source which is not shaft 43.
In an example, an embodiment of compressor assembly 20 achieved a decibel reduction of 7.5 dBA. In this example, noise output when compared to a pancake compressor assembly was reduced from about 78.5 dBA to about 71 dBA.
The pump assembly 25 (e.g.
Parts, for example, the tank seal 600 (e.g.
The fewer openings which are present in the housing 21, the less total open area exists in the housing for noise to escape through unabated. In an embodiment, other openings, or gaps which exist in the housing 21 of the compressor assembly 20, or pieces or components thereof, can be eliminated, closed or sealed to reduce the noise emitted from the compressor assembly 20. In an embodiment, openings or gaps associated with one or a plurality of quick connections, such as the first quick connection 305 and the second quick connection 310, or with one or a plurality of a pressure regulator 320 can be eliminated, closed or sealed to reduce the noise emitted from the compressor assembly 20. In an embodiment, gaps around the dashboard 300 or the manifold 303 can be sealed or blocked by foam to reduce the noise emitted by the compressor assembly 20. In an embodiment, the sound level of a compressor assembly 20 can be reduced by reducing the amount of openings present in the housing 21, or pieces thereof.
The tank gap 599 can have a distance between the housing rim 605 and the compressed gas tank 150 which can have a value in e.g. a range of from 0.01 in to 6 in, or e.g. a range of from 0.05 in to 5 in. In an embodiment, the distance between the housing rim 605 and the compressed gas tank 150 can have a value in a range of from 1.0 in to 2.0 in. In an embodiment, the distance between the housing rim 605 and the compressed gas tank 150 can have a value in a range of from 0.15 in to 1.0 in. In an embodiment, the distance between the housing rim 605 and the compressed gas tank 150 can have a value in a range of from 0.05 in to 0.75 in. In an embodiment, the housing rim 605 can have a value of 0.250 in.
There can also be a distance between the closest portion of the pump assembly 25 components and the compressed gas tank 150 which can have a value in a range of from 0.1 in to 8 in. In an embodiment, a sound absorbing cushion can be placed between the pump assembly 25 and the compressed gas tank 150.
The use of a tank seal 600 can achieve a noise reduction having a value in a range of from 0.5 dBA to 15 dBA, or a greater. In further embodiments, the use of a tank seal 600 can achieve a noise reduction having a value in a range of from 0.5 dBA to 10 dBA; or from 0.5 dBA to 7 dBA; or from 1.4 dBA to 15 dBA; or from 5 dBA to 10 dBA; or from 0.5 dBA to 8 dBA; or from 0.5 dBA to 5 dBA; or from 5 dBA to 8 dBA.
In an embodiment, a decibel reduction of 2.5 dBA can be achieved by using a tank seal 600 to reduce the noise output of a compressor assembly 20. In this example embodiment, the noise output of a compressor assembly 20 can be reduced from 70.5 dBA to 68 dBA using a tank seal 600.
The tank gap 599 can be sealed by a tape, or a duct tape, or a foam tape, or a rubber tape, or a Gorilla Tape® (The Gorilla Glue Company, 4550 Red Bank Expressway Cincinnati, OH 45227). Alternatively, the tank gap 599 can be sealed by an expandable spray foam, a caulk or a silicone. The tank gap 599 can also be sealed by a cushion material including, but not limited to, a cloth, felt, or other type of strip or appropriately shaped material which can conform in shape, of deform, to seal tank gap 599. The rubber or rubber-like material could be over-molded onto the housing rim 605. In an embodiment, the rubber or rubber-like material could be manufactured as a separate piece for assembly as a seal. For example, the tank gap 599 can be sealed by over-molding on the shroud with low durometer material, or other material. Alternatively, the tank gap 599 can be sealed by a foam strip. For example, the tank gap 599 can be sealed by a mat, a tank blanket, a foam or other tank covering onto which the housing rim 605 can be set and which can seal the tank gap 599. In an embodiment, an ethylene propylene diene monomer (EPDM) sponge rubber can be used to seal or fill gaps or openings and/or to reduce or muffle noise.
In an embodiment, tank gap 599 can be closed and/or sealed by a rubber or foam strip which can be attached to the shroud, or the tank, or held by frictional attachment, so that the rubber or foam strip can fill the gap when the parts are assembled, thus providing a seal to prevent an amount of noise from escaping from compressor assembly 20 through tank gap 599 and/or emanating from compressor assembly 20.
In an embodiment, the tank seal 600 can be compressed under a force having a value in a range of from 0.25 lbf/in{circumflex over ( )}2 to 50 lbf/in{circumflex over ( )}2, or greater.
In an embodiment, the seal bulb 627 can have a seal bulb outer diameter 631 (also herein as “seal bulb OD 631”; see also
The seal bulb 627 can have an outer diameter, when not compressed of, e.g. 0.375 in. When compressed, the seal bulb 627 can change shape, or deform, under force to a shape which can conform to at least a portion of the compressed gas tank 150 and which can seal the tank gap 599.
The housing seal base portion 626 (
In an embodiment, the tank seal 600 can have a pump assembly side 636 and an outside 638. A difference in sound level across the tank seal 600 as measured from a location on or proximate to the pump assembly side 636 to a location on or proximate to the outside 638 can be a value in a range of from 0.25 dBA to 15 dBA. A difference in sound level across the tank seal 600 as measured from a location on or proximate to the pump assembly side 636 to a location on or proximate to the outside 638 can be a value in a range of from 0.3 dBA to 10 dBA. A difference in sound level across the tank seal 600 as measured from a location on or proximate to the pump assembly side 636 to a location on or proximate to the outside 638 can be a value in a range of from 2.0 dBA to 10 dBA. The difference in sound level across the tank seal 600 as measured at the aforementioned locations can have a value in a range of from 2.5 dBA to 8 dBA, in a range of from 5 dBA to 8 dBA.
In an embodiment, in which seal 600 is over-molded onto the housing rim 605 the height of such over-molded seal can be less than 0.3 in, an can have a range of e.g. from 0.1 in to 3.0 in, or greater.
Foam can be used to muffle the noise from the plurality of exhaust ports 31. In an embodiment, the foam can have a porosity to allow exiting exhaust air flow through the plurality of exhaust ports 31 for sufficient cooling. In an embodiment, foam can be used to muffle the noise from the intake ports 182 for the cooling air.
In an embodiment, a sound absorbing foam can be, e.g. a polyurethane foam and can have a value of density in a range from 0.8 lb/ft{circumflex over ( )}3 to 5.0 lb/ft{circumflex over ( )}3. The foam can be used as a tank seal 600 forming a noise barrier or sound absorber. In an embodiment, the foam can have a value of density in a range from 1.6 lb/ft{circumflex over ( )}3 to 2.0 lb/ft{circumflex over ( )}3, or e.g. have a value of density of 1.8 lb/ft{circumflex over ( )}3, and can be used as the tank seal 600 to form a noise barrier or sound absorber. In an embodiment, the foam can be flame retardant. In an embodiment, the foam can be used in the pump chamber 491 which can contain at least the pump and motor components to reduce noise emissions from at least the pump assembly 25. In an embodiment, a foam material can cover at least a portion of the tank surface which is present in the pump chamber 491.
The scope of this disclosure is to be broadly construed. It is intended that this disclosure disclose equivalents, means, systems and methods to achieve the devices, designs, operations, control systems, controls, activities, mechanical actions, fluid dynamics and results disclosed herein. For each mechanical element or mechanism disclosed, it is intended that this disclosure also encompasses within the scope of its disclosure and teaches equivalents, means, systems and methods for practicing the many aspects, mechanisms and devices disclosed herein. Additionally, this disclosure regards a compressor and its many aspects, features and elements. Such an apparatus can be dynamic in its use and operation. This disclosure is intended to encompass the equivalents, means, systems and methods of the use of the compressor assembly and its many aspects consistent with the description and spirit of the apparatus, means, methods, functions and operations disclosed herein. The claims of this application are likewise to be broadly construed.
The description of the inventions herein in their many embodiments is merely exemplary in nature and, thus, variations that do not depart from the gist of the invention are intended to be within the scope of the invention and the disclosure herein. Such variations are not to be regarded as a departure from the spirit and scope of the invention.
It will be appreciated that various modifications and changes can be made to the above described embodiments of a compressor assembly as disclosed herein without departing from the spirit and the scope of the following claims.
This patent application claims benefit of the filing date of nonprovisional U.S. patent application Ser. No. 13/609,349 titled “Method Of Reducing Air Compressor Noise” filed Sep. 11, 2012, which issued as U.S. Pat. No. 10,871,153 on Dec. 22, 2020, and which claims benefit of U.S. provisional patent application No. 61/533,993 titled “Air Ducting Shroud For Cooling An Air Compressor Pump And Motor” filed on Sep. 13, 2011. This patent application claims benefit of the filing date of U.S. provisional patent application No. 61/534,001 titled “Shroud For Capturing Fan Noise” filed on Sep. 13, 2011. This patent application claims benefit of the filing date of U.S. provisional patent application No. 61/534,009 titled “Method Of Reducing Air Compressor Noise” filed on Sep. 13, 2011. This patent application claims benefit of the filing date of U.S. provisional patent application No. 61/534,015 titled “Tank Dampening Device” filed on Sep. 13, 2011. This patent application claims benefit of the filing date of U.S. provisional patent application No. 61/534,046 titled “Compressor Intake Muffler And Filter” filed on Sep. 13, 2011.
Number | Name | Date | Kind |
---|---|---|---|
1381056 | Blakely | Jun 1921 | A |
1469201 | Whitted et al. | Sep 1923 | A |
1694218 | Hazard | Dec 1928 | A |
1924654 | Petersen | Aug 1933 | A |
2059894 | Newman | Nov 1936 | A |
2106488 | McCune | Jan 1938 | A |
2107644 | Ohmart | Feb 1938 | A |
2136098 | Browne | Nov 1938 | A |
2312596 | Smith | Mar 1943 | A |
2343952 | Branstrom | Mar 1944 | A |
2375442 | Sandberg | May 1945 | A |
2450468 | Cornelius | Oct 1948 | A |
2668004 | Browne | Feb 1954 | A |
2673028 | Cornelius et al. | Mar 1954 | A |
D181459 | Bullock | Nov 1957 | S |
2928491 | Crouch | Mar 1960 | A |
3370608 | Eisenbrand et al. | Feb 1968 | A |
3525606 | Bodine | Aug 1970 | A |
3537544 | King | Nov 1970 | A |
3591315 | Whelan | Jul 1971 | A |
3645651 | Bills | Feb 1972 | A |
3687019 | Wolf | Aug 1972 | A |
3710094 | Monte et al. | Jan 1973 | A |
3736074 | Kilbane et al. | May 1973 | A |
3771911 | Turci | Nov 1973 | A |
3930558 | Schnell et al. | Jan 1976 | A |
3955900 | Vinci | May 1976 | A |
3978919 | Fachbach et al. | Sep 1976 | A |
3980912 | Panza | Sep 1976 | A |
4190402 | Meece et al. | Feb 1980 | A |
4264282 | Crago | Apr 1981 | A |
4283167 | Bassan et al. | Aug 1981 | A |
4289630 | Schmidt, Jr. et al. | Sep 1981 | A |
4302224 | McCombs et al. | Nov 1981 | A |
D263216 | Maher | Mar 1982 | S |
4342573 | McCombs et al. | Aug 1982 | A |
4401418 | Fritchman | Aug 1983 | A |
4460319 | Ashikian | Jul 1984 | A |
4492533 | Tsuge | Jan 1985 | A |
4516657 | Allard | May 1985 | A |
4553903 | Ashikian | Nov 1985 | A |
4566800 | Bodine | Jan 1986 | A |
4722673 | Grime et al. | Feb 1988 | A |
4907546 | Ishii et al. | Mar 1990 | A |
4928480 | Oliver et al. | May 1990 | A |
4950133 | Sargent | Aug 1990 | A |
4988268 | Kurihara | Jan 1991 | A |
5020973 | Lammers | Jun 1991 | A |
5082019 | Tetrault | Jan 1992 | A |
5133475 | Sharp | Jul 1992 | A |
5137434 | Wheeler et al. | Aug 1992 | A |
5143772 | Iwasa | Sep 1992 | A |
5145335 | Abelen et al. | Sep 1992 | A |
D335407 | Ngian et al. | May 1993 | S |
5213484 | Hashimoto et al. | May 1993 | A |
5252035 | Lee | Oct 1993 | A |
5311090 | Ferlatte | May 1994 | A |
5311625 | Barker et al. | May 1994 | A |
5336046 | Hashimoto et al. | Aug 1994 | A |
5407330 | Rimington et al. | Apr 1995 | A |
5417258 | Privas | May 1995 | A |
5509790 | Schuderi et al. | Apr 1996 | A |
5526228 | Dickson et al. | Jun 1996 | A |
5620370 | Umai et al. | Apr 1997 | A |
5647314 | Matsumura et al. | Jul 1997 | A |
5678543 | Bower | Oct 1997 | A |
5725361 | Dantlgraber | Mar 1998 | A |
6023938 | Taras et al. | Feb 2000 | A |
6091160 | Kouchi et al. | Jul 2000 | A |
6099268 | Pressel | Aug 2000 | A |
6100599 | Kouchi et al. | Aug 2000 | A |
6145974 | Shinada et al. | Nov 2000 | A |
D437581 | Aruga et al. | Feb 2001 | S |
D437825 | Imai | Feb 2001 | S |
6206654 | Cassidy | Mar 2001 | B1 |
D444796 | Morgan | Jul 2001 | S |
D444797 | Davis et al. | Jul 2001 | S |
6257842 | Kawasaki et al. | Jul 2001 | B1 |
6331740 | Morohoshi et al. | Dec 2001 | B1 |
D454357 | Diels | Mar 2002 | S |
6357338 | Montgomery | Mar 2002 | B2 |
6362533 | Morohoshi et al. | Mar 2002 | B1 |
6364632 | Cromm et al. | Apr 2002 | B1 |
6378468 | Kouchi et al. | Apr 2002 | B1 |
6378469 | Hiranuma et al. | Apr 2002 | B1 |
6386833 | Montgomery | May 2002 | B1 |
D461196 | Buck | Aug 2002 | S |
6428283 | Bonior | Aug 2002 | B1 |
6428288 | King | Aug 2002 | B1 |
6431839 | Gruber et al. | Aug 2002 | B2 |
6435076 | Montgomery | Aug 2002 | B2 |
6447257 | Orschell | Sep 2002 | B2 |
6447264 | Lucas et al. | Sep 2002 | B1 |
6454527 | Nishiyama et al. | Sep 2002 | B2 |
6474954 | Bell et al. | Nov 2002 | B1 |
6554583 | Pressel | Apr 2003 | B1 |
6571561 | Aquino et al. | Jun 2003 | B1 |
6616415 | Renken et al. | Sep 2003 | B1 |
6682317 | Chen | Jan 2004 | B2 |
6720098 | Raiser | Apr 2004 | B2 |
6751941 | Edelman et al. | Jun 2004 | B2 |
6784560 | Sugimoto et al. | Aug 2004 | B2 |
6790012 | Sharp et al. | Sep 2004 | B2 |
6814659 | Cigelske, Jr. | Nov 2004 | B2 |
D499431 | Chen | Dec 2004 | S |
6952056 | Brandenburg et al. | Oct 2005 | B2 |
6962057 | Kurokawa et al. | Nov 2005 | B2 |
6991436 | Beckman et al. | Jan 2006 | B2 |
6998725 | Brandenburg et al. | Feb 2006 | B2 |
D517009 | Xiao | Mar 2006 | S |
D521929 | Xiao | May 2006 | S |
D531193 | Caito | Oct 2006 | S |
7147444 | Cheon | Dec 2006 | B2 |
D536348 | Bass | Feb 2007 | S |
D536708 | Bass | Feb 2007 | S |
7189068 | Thomas, Jr. et al. | Mar 2007 | B2 |
D551141 | Canitano | Sep 2007 | S |
7283359 | Bartell et al. | Oct 2007 | B2 |
7306438 | Kang et al. | Dec 2007 | B2 |
7316291 | Thomsen et al. | Jan 2008 | B2 |
D566042 | Yamasaki et al. | Apr 2008 | S |
D568797 | Elwell | May 2008 | S |
D572658 | Yamamoto et al. | Jul 2008 | S |
7392770 | Xiao | Jul 2008 | B2 |
7398747 | Onodera et al. | Jul 2008 | B2 |
7398855 | Seel | Jul 2008 | B2 |
7400501 | Bartell et al. | Jul 2008 | B2 |
D576723 | Achen | Sep 2008 | S |
7430992 | Murakami et al. | Oct 2008 | B2 |
7452256 | Kasai et al. | Nov 2008 | B2 |
7491264 | Tao et al. | Feb 2009 | B2 |
D588987 | Kato | Mar 2009 | S |
D589985 | Steinfels | Apr 2009 | S |
D593032 | Wang et al. | May 2009 | S |
7541701 | Lin et al. | Jun 2009 | B2 |
7563077 | Santa Ana | Jul 2009 | B2 |
D600205 | Imai | Sep 2009 | S |
7597340 | Hirose et al. | Oct 2009 | B2 |
7614473 | Ono et al. | Nov 2009 | B2 |
7643284 | Nakamura | Jan 2010 | B2 |
7678165 | Tingle et al. | Mar 2010 | B2 |
7707711 | Bartell et al. | May 2010 | B2 |
7743739 | Kochi et al. | Jun 2010 | B2 |
7762790 | Steinfels et al. | Jul 2010 | B2 |
7779792 | Kubo et al. | Aug 2010 | B2 |
7779793 | Ito et al. | Aug 2010 | B2 |
7811653 | Miyakawa et al. | Oct 2010 | B2 |
7854517 | Tsubura | Dec 2010 | B2 |
8215448 | Harting et al. | Jul 2012 | B2 |
8230968 | Jung et al. | Jul 2012 | B2 |
8246320 | Park et al. | Aug 2012 | B2 |
8316987 | Ishida et al. | Nov 2012 | B2 |
8327975 | Ortman et al. | Dec 2012 | B2 |
8584795 | Buckner | Nov 2013 | B1 |
8770341 | Wood et al. | Jul 2014 | B2 |
8899378 | Wood et al. | Dec 2014 | B2 |
8967324 | White et al. | Mar 2015 | B2 |
8992186 | Silveira et al. | Mar 2015 | B2 |
9309876 | Wood et al. | Apr 2016 | B2 |
9476416 | Chen | Oct 2016 | B2 |
10871153 | White | Dec 2020 | B2 |
10982664 | Wood et al. | Apr 2021 | B2 |
20020009372 | Gruber et al. | Jan 2002 | A1 |
20020134617 | Nessen et al. | Sep 2002 | A1 |
20020185333 | Svendsen | Dec 2002 | A1 |
20040103683 | Yoon | Jun 2004 | A1 |
20040191073 | Iimura | Sep 2004 | A1 |
20040202562 | Grassbaugh et al. | Oct 2004 | A1 |
20050092544 | Lee | May 2005 | A1 |
20050220640 | Finkenbinder et al. | Oct 2005 | A1 |
20050247750 | Burkholder et al. | Nov 2005 | A1 |
20060104830 | Fields | May 2006 | A1 |
20060104833 | Hueppchen | May 2006 | A1 |
20060104834 | Stilwell | May 2006 | A1 |
20060104837 | Lee et al. | May 2006 | A1 |
20060137522 | Nishimura et al. | Jun 2006 | A1 |
20060245952 | Chen | Nov 2006 | A1 |
20070236882 | Chen | Oct 2007 | A1 |
20070284954 | Lin et al. | Dec 2007 | A1 |
20080008603 | Schoegler | Jan 2008 | A1 |
20080045368 | Nishihara | Feb 2008 | A1 |
20080053746 | Albert et al. | Mar 2008 | A1 |
20080069703 | Beckman | Mar 2008 | A1 |
20080152518 | Stilwell | Jun 2008 | A1 |
20080181794 | Steinfels et al. | Jul 2008 | A1 |
20080187447 | Steinfels et al. | Aug 2008 | A1 |
20080273994 | Sadkowski et al. | Nov 2008 | A1 |
20090016902 | Lee et al. | Jan 2009 | A1 |
20090050219 | Firoenza et al. | Feb 2009 | A1 |
20090114476 | Lewis et al. | May 2009 | A1 |
20090121492 | Ito et al. | May 2009 | A1 |
20090194177 | Yokota et al. | Aug 2009 | A1 |
20100112929 | Iantorno | May 2010 | A1 |
20100192878 | Mustafa | Aug 2010 | A1 |
20100225012 | Fitton et al. | Sep 2010 | A1 |
20100226750 | Gammack | Sep 2010 | A1 |
20100226771 | Crawford et al. | Sep 2010 | A1 |
20100226787 | Gammack et al. | Sep 2010 | A1 |
20100239438 | Kinjo et al. | Sep 2010 | A1 |
20100290929 | Ohi et al. | Nov 2010 | A1 |
20100317281 | Sperandio et al. | Dec 2010 | A1 |
20110094052 | Witter | Apr 2011 | A1 |
20110095540 | Jackson et al. | Apr 2011 | A1 |
20110158828 | Nutz | Jun 2011 | A1 |
20110182754 | Gathers et al. | Jul 2011 | A1 |
20130062141 | Wood et al. | Mar 2013 | A1 |
20140294636 | Ito et al. | Oct 2014 | A1 |
20150316050 | Sharp et al. | Nov 2015 | A1 |
20150345490 | Bremeier et al. | Dec 2015 | A1 |
Number | Date | Country |
---|---|---|
101144668 | Mar 2008 | CN |
201526435 | Jul 2010 | CN |
101940589 | Jan 2011 | CN |
102162440 | Aug 2011 | CN |
2751298 | May 1979 | DE |
4416555 | Nov 1995 | DE |
10117791 | Oct 2002 | DE |
1862671 | Dec 2007 | EP |
2320085 | May 2011 | EP |
2706234 | Mar 2014 | EP |
919265 | Mar 1947 | FR |
2153920 | Aug 1985 | GB |
54041562 | Apr 1979 | JP |
1080793 | Mar 1989 | JP |
4232390 | Aug 1992 | JP |
5133330 | May 1993 | JP |
7109977 | Apr 1995 | JP |
9250456 | Sep 1997 | JP |
9250457 | Sep 1997 | JP |
10148135 | Jun 1998 | JP |
10339268 | Dec 1998 | JP |
2003065241 | Mar 2003 | JP |
2006292243 | Oct 2006 | JP |
2006062223 | Jun 2006 | WO |
2006090345 | Aug 2006 | WO |
2008021251 | Feb 2008 | WO |
2009152594 | Dec 2009 | WO |
2010092790 | Aug 2010 | WO |
2011094975 | Aug 2011 | WO |
Entry |
---|
Communication Pursuant To Article 94(3) EPC, EP Application No. 12 184 258.7-1004, EPO (Jun. 19, 2020). |
Communication Pursuant To Article 94(3) EPC, EP Application No. 12 183 996.3-1004, EPO (Feb. 3, 2020). |
Communication Pursuant To Article 94(3) EPC, EP Application No. 12 184 217.3-1004, EPO (Feb. 27, 2019). |
Communication Pursuant To Article 94(3) EPC, EP Application No. 12 184 204.1-1004, EPO (Feb. 26, 2019). |
Communication Pursuant To Article 94(3) EPC, EP Application No. 12 184 258.7-1004, EPO (Jan. 24, 2019). |
Communication Pursuant To Article 94(3) EPC, EP Application No. 12 183 996.3-1004, EPO (Jan. 24, 2019). |
Extended European Search Report, EP Application No. 12 183 992.2-1616 / 2570667, EPO (Feb. 22, 2017). |
Extended European Search Report, EP Application No. 12 184 204.1-1616 / 2570668, EPO (Feb. 7, 2017). |
Extended European Search Report, EP Application No. 12 183 978.1-1616 / 2570664, EPO (Feb. 7, 2017). |
Extended European Search Report, EP Application No. 12 183 996.3-1616 / 2570666, EPO (Feb. 7, 2017). |
Extended European Search Report, EP Application No. 12 184 217.3-1608 / 2570665, EPO (Nov. 2, 2016). |
Kiran Daware, Universal Motor—Construction, Working And Characteristics, AC Machines, Electricaleasy (Feb. 21, 2014, 9:44 PM), https://www.electricaleasy.com/2014/02/universal-motor-construction-working.html. |
Communication Pursuant To Article 94(3) EPC, Application No. 12 184 220.7-1004, EPO (Jun. 19, 2020). |
Communication Pursuant To Article 94(3) EPC, Application No. 12 184 220.7-1004, EPO (Jan. 24, 2019). |
Extended European Search Report, EP Application No. 12 184 258.7, EPO (Feb. 16, 2017). |
Extended European Search Report, Application No. 12 184 220.7-1616 / 2570669, EPO (Feb. 14, 2017). |
Extended European Search Report, EP Application No. 15 201 260.5, EPO (May 6, 2016). |
Extended European Search Report, EP Application No. 13 184 002.7-1608, EPO (Nov. 29, 2013). |
Extended European Search Report, EP Application No. 13 183 932.6-1608, EPO (Nov. 29, 2013). |
Thomas Pumps & Compressors, WOB-L Piston, Technical Document, pp. 1-2 (2002). |
LaBelle et al., Design And Development Of An Old Concept Using New Materials To Produce An Air Compressor, Thomas Industries Power Air Division, pp. 68-72 (1978), International Computer Engineering Conference, Paper 248, http://docs.lib.purdue.edu/iced/248. |
Communication Pursuant To Article 94(3) EPC, Application No. 13 183 932.6-1004, EPO (Feb. 20, 2020). |
Communication Pursuant To Article 94(3) EPC, Application No. 13 184 002.7-1004, EPO (Feb. 13, 2020). |
Communication Pursuant To Article 94(3) EPC, Application No. 15 201 260.5-1204, EPO (Jul. 11, 2018). |
Number | Date | Country | |
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20210079905 A1 | Mar 2021 | US |
Number | Date | Country | |
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61534009 | Sep 2011 | US | |
61533993 | Sep 2011 | US | |
61534001 | Sep 2011 | US | |
61534015 | Sep 2011 | US | |
61534046 | Sep 2011 | US |
Number | Date | Country | |
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Parent | 13609349 | Sep 2012 | US |
Child | 17107045 | US |