US20170089350A1 - Compressor system with grooved expansion joint - Google Patents
Compressor system with grooved expansion joint Download PDFInfo
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- US20170089350A1 US20170089350A1 US14/870,607 US201514870607A US2017089350A1 US 20170089350 A1 US20170089350 A1 US 20170089350A1 US 201514870607 A US201514870607 A US 201514870607A US 2017089350 A1 US2017089350 A1 US 2017089350A1
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- Prior art keywords
- conduits
- compressor
- conduit
- fluid
- wall thickness
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Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/60—Mounting; Assembling; Disassembling
- F04D29/62—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps
- F04D29/624—Mounting; Assembling; Disassembling of radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/02—Selection of particular materials
- F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D17/00—Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
- F04D17/08—Centrifugal pumps
- F04D17/10—Centrifugal pumps for compressing or evacuating
- F04D17/12—Multi-stage pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/04—Units comprising pumps and their driving means the pump being fluid-driven
- F04D25/045—Units comprising pumps and their driving means the pump being fluid-driven the pump wheel carrying the fluid driving means, e.g. turbine blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/06—Units comprising pumps and their driving means the pump being electrically driven
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/16—Combinations of two or more pumps ; Producing two or more separate gas flows
- F04D25/163—Combinations of two or more pumps ; Producing two or more separate gas flows driven by a common gearing arrangement
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/08—Sealings
- F04D29/083—Sealings especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/28—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps
- F04D29/284—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors
- F04D29/286—Rotors specially for elastic fluids for centrifugal or helico-centrifugal pumps for radial-flow or helico-centrifugal pumps for compressors multi-stage rotors
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/4206—Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
- F04D29/44—Fluid-guiding means, e.g. diffusers
- F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/58—Cooling; Heating; Diminishing heat transfer
- F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
- F04D29/5826—Cooling at least part of the working fluid in a heat exchanger
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L21/00—Joints with sleeve or socket
- F16L21/02—Joints with sleeve or socket with elastic sealing rings between pipe and sleeve or between pipe and socket, e.g. with rolling or other prefabricated profiled rings
- F16L21/022—Joints with sleeve or socket with elastic sealing rings between pipe and sleeve or between pipe and socket, e.g. with rolling or other prefabricated profiled rings used with sleeves or nipples for pipes of the same diameter, or with reduction pieces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L21/00—Joints with sleeve or socket
- F16L21/02—Joints with sleeve or socket with elastic sealing rings between pipe and sleeve or between pipe and socket, e.g. with rolling or other prefabricated profiled rings
- F16L21/035—Joints with sleeve or socket with elastic sealing rings between pipe and sleeve or between pipe and socket, e.g. with rolling or other prefabricated profiled rings placed around the spigot end before connection
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L23/00—Flanged joints
- F16L23/04—Flanged joints the flanges being connected by members tensioned in the radial plane
- F16L23/08—Flanged joints the flanges being connected by members tensioned in the radial plane connection by tangentially arranged pin and nut
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
- F16L25/00—Construction or details of pipe joints not provided for in, or of interest apart from, groups F16L13/00 - F16L23/00
- F16L25/14—Joints for pipes of different diameters or cross-section
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
- F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
- F25B31/00—Compressor arrangements
Definitions
- the present application generally relates to industrial air compressor systems and more particularly, but not exclusively, to coupling a thin walled conduit to the system with a grooved expansion joint.
- One embodiment of the present invention is a unique compressor system.
- Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for compressor systems with a unique coupling system for thin walled conduits. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith.
- FIG. 1 is a perspective view of a compressor system according to one embodiment of the present disclosure
- FIG. 2 is a perspective view of a portion of the compressor system of FIG. 1 with an enlarged view of a coupling mechanism
- FIG. 3 is a cross sectional view of a first conduit having a thin wall connected to a second conduit with a grooved expansion joint coupling;
- FIG. 4 is an enlarged view of a portion of FIG. 3 .
- Fluid heat exchangers as defined herein can be of any type commonly utilized in industrial applications. It should be noted that terms such as intercooler, cooler, inter-stage cooler, aftercooler or the like can be interchanged or substituted and still fall within the broad definition of a heat exchanger as defined by the present disclosure. It should be further understood that the term “fluid” includes any gas or liquid medium used in the compressor system as disclosed herein. Typically, because of the size and weight of industrial components, each of the components are transported separately and assembled on site.
- connection assemblies such as by use of thin walled conduits or pipes to connect various components of the compressor system. Limited options are available for coupling thin walled conduits when thermal expansion is an operational concern.
- the present disclosure provides means to reduce the size and complexity of the coupling mechanisms so that thin walled conduits may be used with a compressor system such as that defined herein.
- a thin walled conduit is defined as any conduit having a wall thickness that is too thin to structurally support a machined slot or groove formed in an outer surface thereof for a grooved expansion joint clamp to engage therewith. Machining a groove in a thin walled conduit deep enough to support a grooved expansion joint would result in a weakened structure or complete mechanical failure of the conduit.
- Typical wall thicknesses for thin wall conduits can be found in Nominal Pipe Size (NPS) tables for schedule 5 and schedule 10 conduits.
- Wall thickness for thin walls can range from 0.035 inches for 1 ⁇ 8 NPS to 0.083 inches for 31 ⁇ 2 NPS schedule 5 conduits and from 0.049 inches to 0.120 inches for schedule 10 conduits.
- the compressor system 10 includes a primary motive source 20 such as an electric motor, an internal combustion engine or a fluid-driven turbine and the like.
- the compressor system 10 can include a compressor 30 with multi-stage compression and in the exemplary embodiment includes a first stage compressor 32 , a second stage compressor 34 , and a third stage compressor 36 . In other embodiments a different number of compressor stages may be employed with the compressor 30 .
- the compressor 30 can include centrifugal, axial and/or positive displacement compression means.
- the primary motive source 20 is operable for driving the compressor 30 via a drive shaft 22 to compress fluids such as air or the like.
- a structural base 12 is configured to support at least portions of the compressor system 10 on a support surface 13 such as a floor or ground and the like.
- One or more cantilevered extensions or arms 14 can extend from the base 12 and is configured to hold portions of the compressor system 10 suspended above the support surface 13 .
- Portions of the compressed air discharged from the compressor 30 can be transported through more one or more conduits 40 , 50 , 60 , 70 and 80 to one or more intercoolers 100 and/or to another compressor stage.
- An inlet fluid manifold 90 and an outlet fluid manifold 92 can be fluidly connected to the intercoolers 100 to provide cooling fluid such as water or other liquid coolant to cool the compressed air after discharge from one or more of the compressor stages of the compressor 30 .
- the compressor system 10 can also include a controller 110 operable for controlling the primary motive power source and various valving and fluid control mechanisms (not shown) between the compressor 30 and intercoolers 100 .
- An intercooler fluid port 200 can be connected to an intercooler 100 proximate an intercooler connecting region 202 .
- the intercooler connecting region 202 can affix the intercooler fluid port 200 to the intercooler 100 via weld, braze, or other mechanical fastening means as known to those skilled in the art.
- the intercooler fluid port 200 can include a port coupling region 204 positioned on an opposing end of the intercooler fluid port 200 from the intercooler connecting region 202 .
- the intercooler fluid port 200 includes an elbow or bend 203 , however, in other embodiments the intercooler fluid port can substantially extend straight away from a sidewall of the intercooler 100 .
- a fluid conduit 60 can include a connecting end portion 206 extending to a coupling region 208 formed between the intercooler port 200 and the connecting end portion 206 of the fluid transfer conduit 60 .
- the fluid conduit 60 can include a thin wall 210 which defines the conduit as a thin walled conduit.
- the fluid coupling region 208 can include a grooved expansion joint clamp 209 operable for connecting the intercooler fluid port 200 with the fluid transfer conduit 60 as will be described in more detail below.
- the expansion joint claim 209 connects the fluid transfer conduit 60 to the fluid port 200 , however it should be understood that other connections of thin walled conduits are contemplated by this disclosure.
- the fluid transfer conduit 60 is formed as a thin walled structure.
- both the conduit 60 and fluid port 200 can be thin walled structures.
- a thin wall as defined herein includes a conduit or a pipe having a wall thickness that is too thin to machine grooves or the like therein for a grooved expansion clamp to engage therewith and couple a pair of conduits together.
- the thickness of the thin wall 210 is defined by the distance between an inner surface 211 and an outer surface 213 of the thin wall 210 .
- the connecting end portion 206 can include an adaptor fitting 207 that is connected to the thin wall portion of the conduit 60 .
- the adaptor fitting 207 can be attached by a weld 255 or other mechanical means known to those skilled in the art.
- the adaptor 207 provides a transition from a thin wall 210 to a second wall thickness 214 defined as the distance between an inner surface 213 and an outer surface 215 thereof.
- the second wall thickness 214 is defined as a wall that is thick enough to receive a machined groove for an expansion joint coupling and remain structurally sound.
- the connecting end portion 206 includes a tapered transition portion 212 that widens from the thin wall 210 of the conduit 60 to the second wall thickness 214 at a coupling end portion 216 .
- the coupling end portion 216 includes a second wall thickness to 214 that is structurally capable of receiving a slot or groove 200 formation therein.
- the slot or groove 220 (best seen in FIG. 4 ) can be formed in the coupling portion 216 of the adaptor 207 .
- the slot 220 can be formed in any traditional manner as known to those skilled in the art such as by way of example and not limitation a milling machine or a lathe and the like.
- the connecting end portion 206 can be attached to the thin walled portion of the conduit 60 via a weld joint 255 or a brazed joint as described previously.
- the intercooler fluid port 200 can include a wall 223 defined from an inner surface 225 to an outer surface 227 .
- the wall 223 can be a thin wall in which case an adapter such as the adapter 207 , would necessarily need to be connected thereto.
- the wall 223 can be formed with a wall having a thickness sufficient to receive a machined slot 222 (best seen in FIG. 4 ) therein.
- An expansion clamp 209 can engage the slots 220 , 222 of the fluid conduit 60 and the intercooler fluid port 200 so as to permit a releasable connection there between. The expansion clamp 209 permits the conduits to move relative to one another without binding or potentially causing material failure.
- the expansion clamp 209 can include a threaded fastener 221 on opposing sides to clamp two halves (not shown) of the clamp 209 together.
- a first o-ring seal 250 can be positioned between the clamp 209 and a portion and the outer surface 215 of the connecting end portion 206 to form a fluid tight seal therebetween.
- a second O-ring seal 252 can be positioned between the outer surface 227 of the intercooler fluid port 200 and the clamp 209 to provide a fluid type connection therebetween.
- the expansion clamp 209 can include a first leg extension 230 that is operably engageable with the slot 220 of the connecting end portion 206 of the thin walled conduit 60 and a second leg extension 232 that is operably engageable with the slot 222 formed in the end of the intercooler fluid port 200 .
- the slots 220 , 222 provide for a path for the leg extensions 230 , 232 of the clamp 209 to slide along.
- the conduits 60 , 200 can move relative to the clamp 209 and to one another along a longitudinal or axial direction defined by axis 270 (See FIG. 3 ).
- the slot 220 can include a first abutment wall 231 and a second abutment wall 233 to define the bounds for the leg extension 230 to slide therebetween.
- the slot 222 formed in the intercooler fluid port 200 can include a first abutment 235 and second abutment 237 for the leg extension 232 of the expansion clamp 209 to slide therebetween.
- the clamp 209 can include a first o-ring groove 260 on one side and a second o-ring groove 262 on the other side to receive the o-rings 250 , 252 therein so as to provide a fluid tight seal between the clamp 209 and each conduit 60 , 200 respectively.
- a single seal can be attached between the clamp and extend across the interface region of the ends of the conduit 60 , 200 respectively to form a fluid tight seal therewith.
- the conduits can include grooves to house seals such as O-rings therein as opposed to the clamp housing the O-ring seals.
- the compressor system is configured to provide compressed air at a desired temperature and pressure to external systems.
- the compressor systems can be used in any industrial application including but not limited to automobile manufacturing, textile manufacturing, process industries, refineries, power plants, mining, material handling, etc.
- the controller permits user input to define parameters such as pressure, temperature and mass flow rate.
- the controller will send command signals to the motor to rotate at a desired operating speed in order to drive the one or more compressors and control various valving to control airflow rate and coolant flow rate.
- the compressor system includes a three-stage centrifugal compressor system, however, the system can operate with other types of compressors and/or with more or less stages of compressors.
- One or more intercoolers can be fluidly coupled to each compressor stage such that after air is compressed through the first stage the air can be transported through a first intercooler and can be cooled to a desired temperature via a heat transfer mechanism such as conduction and convection in tube type heat exchangers. The compressed air can then be transported into a second stage compressor where the air further compressed and necessarily heated to a higher temperature through a thermodynamic process. The second stage compressed air can then be routed through a second intercooler to cool the air to desired temperature while remaining at or close to the compressor outlet pressure of the second stage compressor.
- a heat transfer mechanism such as conduction and convection in tube type heat exchangers.
- the compressed air can then be transported into a second stage compressor where the air further compressed and necessarily heated to a higher temperature through a thermodynamic process.
- the second stage compressed air can then be routed through a second intercooler to cool the air to desired temperature while remaining at or close to the compressor outlet pressure of the second stage compressor.
- the cooled compressed air exiting from the second intercooler can then be transported to a third stage compressor where it is compressed to a final desired pressure and then subsequently routed to a third stage intercooler to bring the temperature of the final discharged air pressure to the desired temperature for delivery to a final subsystem.
- the compressors can be centrifugal compressors, however, other forms of compression can include axial flow compressors, piston compressors or other positive displacement compressors can be used under the teachings of the present disclosure.
- the expansion groove clamp connection with at least one thin walled conduit provides means for facilitating positional variation of components due to mechanical dimensional tolerance stack-up that occurs during assembly and/or for thermal expansion growth between various components due to temperature gradients caused by variable heating and cooling of the components of the compressor system.
- the expansion groove clamp used in combination with at least one thin walled conduit also provides means for coupling of fluid conduits in the compressor system in a manner that minimizes space claim and weight which can facilitate ease of assembly and maintenance of said system.
- the conduit coupling means disclosed herein provides a system that remains structurally sound and minimizes potential for mechanical failure due to loads caused by mechanical constraints and thermal loading during operation of the compressor system.
- Material selection for the fluid conduits, coupling members and other components of the compressor system can include various forms of metal, metal alloys, composites, ceramics, or plastics as desired.
- Metals can include, but are not limited to aluminum, steel, iron, super alloys and combinations thereof.
- the metal material may further be formed from cast, wrought, or sheet stock.
- the present disclosure includes a compressor system comprising: a compressor for compressing a fluid; a component in fluid communication with the compressor for receiving compressed fluid; first and second conduits fluidly connecting the compressor to the component, wherein at least one of the conduits is a thin walled conduit; an adaptor end piece connected to an end of the at least one thin walled conduit, wherein the adaptor end piece transitions from a thin wall thickness to a predetermined second wall thickness; a circumferential groove formed in an outer surface of each of the first and second conduits at a location corresponding to the predetermined second wall thickness; and an expansion joint clamp adapted to engage the circumferential grooves and couple the first and second conduits together.
- Refining aspects include an adapter end piece having an angled inner wall extending from the thin wall of the thin walled conduit and the second wall thickness; wherein the expansion joint clamp permits relative movement between the first and second conduits; wherein the clamp includes a pair of circumferential leg extensions; wherein the leg extensions are positioned within the grooves of the first and second conduits; wherein the leg extensions are constructed to slide axially along a width of each groove; wherein each groove includes a pair of side walls to define opposing abutments; wherein one end of each conduit is permanently attached to a compressor component; wherein the component is an intercooler; and wherein the conduits are structured to receive relatively high temperature fluid flow therethrough.
- Another aspect of the present disclosure includes an apparatus comprising: a compression system configured to compress a fluid; a first conduit fluidly connectable to the compression system; a second conduit fluidly connectable to the first conduit; wherein at least one of the first and second conduits are defined by a circumferential thin walled structure; an adaptor end connected to at least one of the first and second conduits having a thin walled structure, the adaptor having a tapered inner wall that transitions from a thin wall to a second wall thickness, wherein the second wall thickness is sufficient to support a circumferential slot formed in the outer surface thereof; a circumferential slot formed in the outer surface of each of the first and second conduits at a location having a wall thickness at least equivalent to the second wall thickness; and an expansion joint coupling engageable with the slots of the first and second conduits and operable to connect the first and second conduits together.
- Refining aspects include a multi-stage centrifugal compressors driven by a motive source; further comprising: an intercooler fluidly connected to one of the first and second conduits; wherein the fluid includes air; further comprising: a fluid seal engaged with the coupling to form a fluid tight seal between the first and second conduits; wherein the expansion joint coupling permits relative movement between the first and second wherein the expansion joint coupling includes a pair of circumferential leg extensions; wherein the leg extensions are configured to engage the slots formed in the first and second conduits; wherein the leg extensions are constructed to slide between sidewall abutments along a width of each slot.
- Another aspect of the present disclosure includes a method comprising: welding an adaptor to an end of a thin walled conduit, wherein the adaptor includes a portion having a second wall thickness greater than the thin walled conduit; forming an outwardly facing groove in the adaptor proximate the portion having the second wall thickness; forming an outwardly facing groove in a second conduit; connecting the first and second conduits with an expansion groove clamp positioned within the grooves of the first and second conduits; generating heated fluid with a compressor system; transporting the heated fluid through the first and second conduit; and moving the conduits relative to the clamp in response to variable thermal loading.
- a refining aspect includes sliding a portion of the clamp along a width of the grooves formed in each of the conduits; wherein the compression system includes a centrifugal compressor fluidly connected to at least one intercooler with the first and second conduits; and further comprising: forming a fluid tight seal between the first and second conduits.
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- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
- The present application generally relates to industrial air compressor systems and more particularly, but not exclusively, to coupling a thin walled conduit to the system with a grooved expansion joint.
- Large industrial compressor systems typically have complex design and assembly procedures. Such industrial systems can be difficult to assemble and maintain due to component weight and space claim requirements. Designing conduits with coupling members to minimize size and weight can reduce assembly time as well as enable cost effective maintenance or repair of the compressor system. Some existing systems have various shortcomings relative to certain applications. Accordingly, there remains a need for further contributions in this area of technology.
- One embodiment of the present invention is a unique compressor system. Other embodiments include apparatuses, systems, devices, hardware, methods, and combinations for compressor systems with a unique coupling system for thin walled conduits. Further embodiments, forms, features, aspects, benefits, and advantages of the present application shall become apparent from the description and figures provided herewith.
-
FIG. 1 is a perspective view of a compressor system according to one embodiment of the present disclosure; -
FIG. 2 is a perspective view of a portion of the compressor system ofFIG. 1 with an enlarged view of a coupling mechanism; -
FIG. 3 is a cross sectional view of a first conduit having a thin wall connected to a second conduit with a grooved expansion joint coupling; and -
FIG. 4 is an enlarged view of a portion ofFIG. 3 . - For the purposes of promoting an understanding of the principles of the invention, reference will now be made to the embodiments illustrated in the drawings and specific language will be used to describe the same. It will nevertheless be understood that no limitation of the scope of the invention is thereby intended. Any alterations and further modifications in the described embodiments, and any further applications of the principles of the invention as described herein are contemplated as would normally occur to one skilled in the art to which the invention relates.
- Industrial compressor systems that use external fluid to fluid heat exchangers or intercoolers can be heavy, difficult to assemble and typically require a large space claim for component connection assemblies. Fluid heat exchangers as defined herein can be of any type commonly utilized in industrial applications. It should be noted that terms such as intercooler, cooler, inter-stage cooler, aftercooler or the like can be interchanged or substituted and still fall within the broad definition of a heat exchanger as defined by the present disclosure. It should be further understood that the term “fluid” includes any gas or liquid medium used in the compressor system as disclosed herein. Typically, because of the size and weight of industrial components, each of the components are transported separately and assembled on site. It is desirable to minimize the size and weight of connection assemblies such as by use of thin walled conduits or pipes to connect various components of the compressor system. Limited options are available for coupling thin walled conduits when thermal expansion is an operational concern. The present disclosure provides means to reduce the size and complexity of the coupling mechanisms so that thin walled conduits may be used with a compressor system such as that defined herein. For purposes of this disclosure a thin walled conduit is defined as any conduit having a wall thickness that is too thin to structurally support a machined slot or groove formed in an outer surface thereof for a grooved expansion joint clamp to engage therewith. Machining a groove in a thin walled conduit deep enough to support a grooved expansion joint would result in a weakened structure or complete mechanical failure of the conduit. Typical wall thicknesses for thin wall conduits can be found in Nominal Pipe Size (NPS) tables for schedule 5 and schedule 10 conduits. Wall thickness for thin walls can range from 0.035 inches for ⅛ NPS to 0.083 inches for 3½ NPS schedule 5 conduits and from 0.049 inches to 0.120 inches for
schedule 10 conduits. - Referring now to
FIG. 1 , acompressor system 10 is shown therein. Thecompressor system 10 includes aprimary motive source 20 such as an electric motor, an internal combustion engine or a fluid-driven turbine and the like. Thecompressor system 10 can include acompressor 30 with multi-stage compression and in the exemplary embodiment includes afirst stage compressor 32, asecond stage compressor 34, and athird stage compressor 36. In other embodiments a different number of compressor stages may be employed with thecompressor 30. Thecompressor 30 can include centrifugal, axial and/or positive displacement compression means. Theprimary motive source 20 is operable for driving thecompressor 30 via adrive shaft 22 to compress fluids such as air or the like. Astructural base 12 is configured to support at least portions of thecompressor system 10 on asupport surface 13 such as a floor or ground and the like. One or more cantilevered extensions orarms 14 can extend from thebase 12 and is configured to hold portions of thecompressor system 10 suspended above thesupport surface 13. Portions of the compressed air discharged from thecompressor 30 can be transported through more one or 40, 50, 60, 70 and 80 to one ormore conduits more intercoolers 100 and/or to another compressor stage. Aninlet fluid manifold 90 and anoutlet fluid manifold 92 can be fluidly connected to theintercoolers 100 to provide cooling fluid such as water or other liquid coolant to cool the compressed air after discharge from one or more of the compressor stages of thecompressor 30. Thecompressor system 10 can also include acontroller 110 operable for controlling the primary motive power source and various valving and fluid control mechanisms (not shown) between thecompressor 30 andintercoolers 100. - Referring now to
FIG. 2 , an enlarged portion of thecompressor system 10 is illustrated therein. Anintercooler fluid port 200 can be connected to anintercooler 100 proximate an intercooler connectingregion 202. Theintercooler connecting region 202 can affix theintercooler fluid port 200 to theintercooler 100 via weld, braze, or other mechanical fastening means as known to those skilled in the art. Theintercooler fluid port 200 can include aport coupling region 204 positioned on an opposing end of theintercooler fluid port 200 from theintercooler connecting region 202. In this exemplary embodiment theintercooler fluid port 200 includes an elbow orbend 203, however, in other embodiments the intercooler fluid port can substantially extend straight away from a sidewall of theintercooler 100. Afluid conduit 60 can include a connectingend portion 206 extending to acoupling region 208 formed between theintercooler port 200 and the connectingend portion 206 of thefluid transfer conduit 60. Thefluid conduit 60 can include athin wall 210 which defines the conduit as a thin walled conduit. Thefluid coupling region 208 can include a groovedexpansion joint clamp 209 operable for connecting theintercooler fluid port 200 with thefluid transfer conduit 60 as will be described in more detail below. In this this exemplary embodiment, the expansionjoint claim 209 connects thefluid transfer conduit 60 to thefluid port 200, however it should be understood that other connections of thin walled conduits are contemplated by this disclosure. - Referring now to
FIGS. 3 and 4 , an enlarged cross-sectional view of thecoupling region 208 of theconduit 60 and theintercooler fluid port 200 is illustrated. In this example, thefluid transfer conduit 60 is formed as a thin walled structure. In other embodiments both theconduit 60 andfluid port 200 can be thin walled structures. As explained above, a thin wall as defined herein includes a conduit or a pipe having a wall thickness that is too thin to machine grooves or the like therein for a grooved expansion clamp to engage therewith and couple a pair of conduits together. The thickness of thethin wall 210 is defined by the distance between aninner surface 211 and anouter surface 213 of thethin wall 210. The connectingend portion 206 can include anadaptor fitting 207 that is connected to the thin wall portion of theconduit 60. Theadaptor fitting 207 can be attached by aweld 255 or other mechanical means known to those skilled in the art. Theadaptor 207 provides a transition from athin wall 210 to a second wall thickness 214 defined as the distance between aninner surface 213 and anouter surface 215 thereof. The second wall thickness 214 is defined as a wall that is thick enough to receive a machined groove for an expansion joint coupling and remain structurally sound. The connectingend portion 206 includes atapered transition portion 212 that widens from thethin wall 210 of theconduit 60 to the second wall thickness 214 at a coupling end portion 216. The coupling end portion 216 includes a second wall thickness to 214 that is structurally capable of receiving a slot orgroove 200 formation therein. The slot or groove 220 (best seen inFIG. 4 ) can be formed in the coupling portion 216 of theadaptor 207. Theslot 220 can be formed in any traditional manner as known to those skilled in the art such as by way of example and not limitation a milling machine or a lathe and the like. The connectingend portion 206 can be attached to the thin walled portion of theconduit 60 via a weld joint 255 or a brazed joint as described previously. - The
intercooler fluid port 200 can include awall 223 defined from aninner surface 225 to anouter surface 227. Thewall 223 can be a thin wall in which case an adapter such as theadapter 207, would necessarily need to be connected thereto. Optionally thewall 223 can be formed with a wall having a thickness sufficient to receive a machined slot 222 (best seen inFIG. 4 ) therein. Anexpansion clamp 209 can engage the 220, 222 of theslots fluid conduit 60 and theintercooler fluid port 200 so as to permit a releasable connection there between. Theexpansion clamp 209 permits the conduits to move relative to one another without binding or potentially causing material failure. Theexpansion clamp 209 can include a threadedfastener 221 on opposing sides to clamp two halves (not shown) of theclamp 209 together. A first o-ring seal 250 can be positioned between theclamp 209 and a portion and theouter surface 215 of the connectingend portion 206 to form a fluid tight seal therebetween. Likewise, a second O-ring seal 252 can be positioned between theouter surface 227 of theintercooler fluid port 200 and theclamp 209 to provide a fluid type connection therebetween. - Referring now to
FIG. 4 , an enlarged exploded view of the connecting orcoupling region 208 of the 60, 200 and theconduits expansion clamp 209 is illustrated. Theexpansion clamp 209 can include afirst leg extension 230 that is operably engageable with theslot 220 of the connectingend portion 206 of the thinwalled conduit 60 and asecond leg extension 232 that is operably engageable with theslot 222 formed in the end of theintercooler fluid port 200. The 220, 222 provide for a path for theslots 230, 232 of theleg extensions clamp 209 to slide along. The 60, 200 can move relative to theconduits clamp 209 and to one another along a longitudinal or axial direction defined by axis 270 (SeeFIG. 3 ). Theslot 220 can include afirst abutment wall 231 and asecond abutment wall 233 to define the bounds for theleg extension 230 to slide therebetween. Likewise, theslot 222 formed in theintercooler fluid port 200 can include afirst abutment 235 andsecond abutment 237 for theleg extension 232 of theexpansion clamp 209 to slide therebetween. - The
clamp 209 can include a first o-ring groove 260 on one side and a second o-ring groove 262 on the other side to receive the o- 250, 252 therein so as to provide a fluid tight seal between therings clamp 209 and each 60, 200 respectively. It should be understood that other forms of fluid sealing arrangement can be used and remain within the teachings of the present application. For example, a single seal can be attached between the clamp and extend across the interface region of the ends of theconduit 60, 200 respectively to form a fluid tight seal therewith. In yet another embodiment the conduits can include grooves to house seals such as O-rings therein as opposed to the clamp housing the O-ring seals.conduit - In operation the compressor system is configured to provide compressed air at a desired temperature and pressure to external systems. The compressor systems can be used in any industrial application including but not limited to automobile manufacturing, textile manufacturing, process industries, refineries, power plants, mining, material handling, etc. The controller permits user input to define parameters such as pressure, temperature and mass flow rate. The controller will send command signals to the motor to rotate at a desired operating speed in order to drive the one or more compressors and control various valving to control airflow rate and coolant flow rate. In the illustrative example, the compressor system includes a three-stage centrifugal compressor system, however, the system can operate with other types of compressors and/or with more or less stages of compressors. One or more intercoolers can be fluidly coupled to each compressor stage such that after air is compressed through the first stage the air can be transported through a first intercooler and can be cooled to a desired temperature via a heat transfer mechanism such as conduction and convection in tube type heat exchangers. The compressed air can then be transported into a second stage compressor where the air further compressed and necessarily heated to a higher temperature through a thermodynamic process. The second stage compressed air can then be routed through a second intercooler to cool the air to desired temperature while remaining at or close to the compressor outlet pressure of the second stage compressor. The cooled compressed air exiting from the second intercooler can then be transported to a third stage compressor where it is compressed to a final desired pressure and then subsequently routed to a third stage intercooler to bring the temperature of the final discharged air pressure to the desired temperature for delivery to a final subsystem. In one form the compressors can be centrifugal compressors, however, other forms of compression can include axial flow compressors, piston compressors or other positive displacement compressors can be used under the teachings of the present disclosure.
- The expansion groove clamp connection with at least one thin walled conduit provides means for facilitating positional variation of components due to mechanical dimensional tolerance stack-up that occurs during assembly and/or for thermal expansion growth between various components due to temperature gradients caused by variable heating and cooling of the components of the compressor system. The expansion groove clamp used in combination with at least one thin walled conduit also provides means for coupling of fluid conduits in the compressor system in a manner that minimizes space claim and weight which can facilitate ease of assembly and maintenance of said system. As such, the conduit coupling means disclosed herein provides a system that remains structurally sound and minimizes potential for mechanical failure due to loads caused by mechanical constraints and thermal loading during operation of the compressor system.
- Material selection for the fluid conduits, coupling members and other components of the compressor system can include various forms of metal, metal alloys, composites, ceramics, or plastics as desired. Metals can include, but are not limited to aluminum, steel, iron, super alloys and combinations thereof. The metal material may further be formed from cast, wrought, or sheet stock.
- In one aspect the present disclosure includes a compressor system comprising: a compressor for compressing a fluid; a component in fluid communication with the compressor for receiving compressed fluid; first and second conduits fluidly connecting the compressor to the component, wherein at least one of the conduits is a thin walled conduit; an adaptor end piece connected to an end of the at least one thin walled conduit, wherein the adaptor end piece transitions from a thin wall thickness to a predetermined second wall thickness; a circumferential groove formed in an outer surface of each of the first and second conduits at a location corresponding to the predetermined second wall thickness; and an expansion joint clamp adapted to engage the circumferential grooves and couple the first and second conduits together.
- Refining aspects include an adapter end piece having an angled inner wall extending from the thin wall of the thin walled conduit and the second wall thickness; wherein the expansion joint clamp permits relative movement between the first and second conduits; wherein the clamp includes a pair of circumferential leg extensions; wherein the leg extensions are positioned within the grooves of the first and second conduits; wherein the leg extensions are constructed to slide axially along a width of each groove; wherein each groove includes a pair of side walls to define opposing abutments; wherein one end of each conduit is permanently attached to a compressor component; wherein the component is an intercooler; and wherein the conduits are structured to receive relatively high temperature fluid flow therethrough.
- Another aspect of the present disclosure includes an apparatus comprising: a compression system configured to compress a fluid; a first conduit fluidly connectable to the compression system; a second conduit fluidly connectable to the first conduit; wherein at least one of the first and second conduits are defined by a circumferential thin walled structure; an adaptor end connected to at least one of the first and second conduits having a thin walled structure, the adaptor having a tapered inner wall that transitions from a thin wall to a second wall thickness, wherein the second wall thickness is sufficient to support a circumferential slot formed in the outer surface thereof; a circumferential slot formed in the outer surface of each of the first and second conduits at a location having a wall thickness at least equivalent to the second wall thickness; and an expansion joint coupling engageable with the slots of the first and second conduits and operable to connect the first and second conduits together.
- Refining aspects include a multi-stage centrifugal compressors driven by a motive source; further comprising: an intercooler fluidly connected to one of the first and second conduits; wherein the fluid includes air; further comprising: a fluid seal engaged with the coupling to form a fluid tight seal between the first and second conduits; wherein the expansion joint coupling permits relative movement between the first and second wherein the expansion joint coupling includes a pair of circumferential leg extensions; wherein the leg extensions are configured to engage the slots formed in the first and second conduits; wherein the leg extensions are constructed to slide between sidewall abutments along a width of each slot.
- Another aspect of the present disclosure includes a method comprising: welding an adaptor to an end of a thin walled conduit, wherein the adaptor includes a portion having a second wall thickness greater than the thin walled conduit; forming an outwardly facing groove in the adaptor proximate the portion having the second wall thickness; forming an outwardly facing groove in a second conduit; connecting the first and second conduits with an expansion groove clamp positioned within the grooves of the first and second conduits; generating heated fluid with a compressor system; transporting the heated fluid through the first and second conduit; and moving the conduits relative to the clamp in response to variable thermal loading.
- A refining aspect includes sliding a portion of the clamp along a width of the grooves formed in each of the conduits; wherein the compression system includes a centrifugal compressor fluidly connected to at least one intercooler with the first and second conduits; and further comprising: forming a fluid tight seal between the first and second conduits.
- While the invention has been illustrated and described in detail in the drawings and foregoing description, the same is to be considered as illustrative and not restrictive in character, it being understood that only the preferred embodiments have been shown and described and that all changes and modifications that come within the spirit of the inventions are desired to be protected. It should be understood that while the use of words such as preferable, preferably, preferred or more preferred utilized in the description above indicate that the feature so described may be more desirable, it nonetheless may not be necessary and embodiments lacking the same may be contemplated as within the scope of the invention, the scope being defined by the claims that follow. In reading the claims, it is intended that when words such as “a,” “an,” “at least one,” or “at least one portion” are used there is no intention to limit the claim to only one item unless specifically stated to the contrary in the claim. When the language “at least a portion” and/or “a portion” is used the item can include a portion and/or the entire item unless specifically stated to the contrary.
- Unless specified or limited otherwise, the terms “mounted,” “connected,” “supported,” and “coupled” and variations thereof are used broadly and encompass both direct and indirect mountings, connections, supports, and couplings. Further, “connected” and “coupled” are not restricted to physical or mechanical connections or couplings.
Claims (23)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US14/870,607 US20170089350A1 (en) | 2015-09-30 | 2015-09-30 | Compressor system with grooved expansion joint |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US14/870,607 US20170089350A1 (en) | 2015-09-30 | 2015-09-30 | Compressor system with grooved expansion joint |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20170089350A1 true US20170089350A1 (en) | 2017-03-30 |
Family
ID=58406957
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US14/870,607 Abandoned US20170089350A1 (en) | 2015-09-30 | 2015-09-30 | Compressor system with grooved expansion joint |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US20170089350A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112935486A (en) * | 2021-03-22 | 2021-06-11 | 哈尔滨汽轮机厂有限责任公司 | MIG welding method for Z-shaped expansion groove partition plate of steam turbine |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2451587A (en) * | 1945-05-07 | 1948-10-19 | Taylor Forge & Pipe Works | Pipe end and joint |
| US2914347A (en) * | 1953-05-29 | 1959-11-24 | Materiaux De Constr Ets | Sleeve joint with resilient spacing means |
| US3695638A (en) * | 1970-03-18 | 1972-10-03 | Victaulic Co Of America | Coupling for plastic pipe |
| US4408788A (en) * | 1981-09-23 | 1983-10-11 | Grinnell Fire Protection Systems Company, Inc. | Hingeable split pipe collar |
| US4522434A (en) * | 1982-04-23 | 1985-06-11 | Victaulic Company Of America | Multiple key segmented pipe coupling |
| US4603887A (en) * | 1984-10-01 | 1986-08-05 | Halliburton Company | Rigid adjustable length assembly |
| US4662656A (en) * | 1983-09-09 | 1987-05-05 | Foster-Miller, Inc. | Pipeline coupling |
| US20090004029A1 (en) * | 2007-05-24 | 2009-01-01 | Behr Gmbh & Co. Kg | Multistage compressor unit with cooling device |
| US20120056419A1 (en) * | 2009-03-19 | 2012-03-08 | Coupling Technology Limited | Pipe coupling |
| US20120121403A1 (en) * | 2009-07-20 | 2012-05-17 | Cameron International Corporation | Removable throat mounted inlet guide vane |
-
2015
- 2015-09-30 US US14/870,607 patent/US20170089350A1/en not_active Abandoned
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2451587A (en) * | 1945-05-07 | 1948-10-19 | Taylor Forge & Pipe Works | Pipe end and joint |
| US2914347A (en) * | 1953-05-29 | 1959-11-24 | Materiaux De Constr Ets | Sleeve joint with resilient spacing means |
| US3695638A (en) * | 1970-03-18 | 1972-10-03 | Victaulic Co Of America | Coupling for plastic pipe |
| US4408788A (en) * | 1981-09-23 | 1983-10-11 | Grinnell Fire Protection Systems Company, Inc. | Hingeable split pipe collar |
| US4522434A (en) * | 1982-04-23 | 1985-06-11 | Victaulic Company Of America | Multiple key segmented pipe coupling |
| US4662656A (en) * | 1983-09-09 | 1987-05-05 | Foster-Miller, Inc. | Pipeline coupling |
| US4603887A (en) * | 1984-10-01 | 1986-08-05 | Halliburton Company | Rigid adjustable length assembly |
| US20090004029A1 (en) * | 2007-05-24 | 2009-01-01 | Behr Gmbh & Co. Kg | Multistage compressor unit with cooling device |
| US20120056419A1 (en) * | 2009-03-19 | 2012-03-08 | Coupling Technology Limited | Pipe coupling |
| US20120121403A1 (en) * | 2009-07-20 | 2012-05-17 | Cameron International Corporation | Removable throat mounted inlet guide vane |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112935486A (en) * | 2021-03-22 | 2021-06-11 | 哈尔滨汽轮机厂有限责任公司 | MIG welding method for Z-shaped expansion groove partition plate of steam turbine |
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