US20060219389A1 - Air compressor aftercooler - Google Patents
Air compressor aftercooler Download PDFInfo
- Publication number
- US20060219389A1 US20060219389A1 US11/096,728 US9672805A US2006219389A1 US 20060219389 A1 US20060219389 A1 US 20060219389A1 US 9672805 A US9672805 A US 9672805A US 2006219389 A1 US2006219389 A1 US 2006219389A1
- Authority
- US
- United States
- Prior art keywords
- aftercooler
- outlet
- inlet header
- bypass
- air
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 238000001816 cooling Methods 0.000 claims abstract description 10
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B29/00—Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
- F02B29/04—Cooling of air intake supply
- F02B29/0406—Layout of the intake air cooling or coolant circuit
- F02B29/0418—Layout of the intake air cooling or coolant circuit the intake air cooler having a bypass or multiple flow paths within the heat exchanger to vary the effective heat transfer surface
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B29/00—Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
- F02B29/04—Cooling of air intake supply
- F02B29/045—Constructional details of the heat exchangers, e.g. pipes, plates, ribs, insulation, materials, or manufacturing and assembly
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F27/00—Control arrangements or safety devices specially adapted for heat-exchange or heat-transfer apparatus
- F28F27/02—Control arrangements or safety devices specially adapted for heat-exchange or heat-transfer apparatus for controlling the distribution of heat-exchange media between different channels
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B29/00—Engines characterised by provision for charging or scavenging not provided for in groups F02B25/00, F02B27/00 or F02B33/00 - F02B39/00; Details thereof
- F02B29/04—Cooling of air intake supply
- F02B29/0493—Controlling the air charge temperature
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
- F28D21/00—Heat-exchange apparatus not covered by any of the groups F28D1/00 - F28D20/00
- F28D2021/0019—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for
- F28D2021/008—Other heat exchangers for particular applications; Heat exchange systems not otherwise provided for for vehicles
- F28D2021/0082—Charged air coolers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F28—HEAT EXCHANGE IN GENERAL
- F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
- F28F2250/00—Arrangements for modifying the flow of the heat exchange media, e.g. flow guiding means; Particular flow patterns
- F28F2250/06—Derivation channels, e.g. bypass
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T10/00—Road transport of goods or passengers
- Y02T10/10—Internal combustion engine [ICE] based vehicles
- Y02T10/12—Improving ICE efficiencies
Definitions
- the present invention relates to air compressor aftercoolers. More particularly, the present invention relates to an aftercooler assembly for providing hot or cool air from an air compressor.
- Engine driven and motor driven air compressors are frequently equipped with an aftercooler in the discharge circuit.
- the aftercooler 10 receives air from the compressor (not shown) via an inlet pipe 14 .
- the compressed air traveling in the direction A enters the aftercooler header 11 via an inlet flange 12 .
- the compressed air travels across the aftercooler as indicated by arrow C.
- the aftercooler 10 lowers the temperature of the compressed air being delivered to the equipment connected to the compressor.
- the cooled air travels from the outlet header 15 through an outlet flange 16 to a discharge pipe 18 as indicated by arrow D.
- An outlet valve 30 may be provided to control the flow to downstream components.
- the cooler air is generally required in order to precipitate moisture from the compressed air as well as protect downstream equipment from excessive temperatures.
- FIG. 2 illustrates a typical system for achieving bypass of the aftercooler 10 .
- This bypass system generally incorporates an additional piping circuit around the aftercooler 10 .
- the inlet pipe 14 includes a tee 22 with a flow path toward the inlet flange 12 and a second path through a bypass pipe 24 .
- a first control valve 23 is provided before the inlet flange 12 and a second control valve 26 is provided along the bypass pipe 24 .
- the control valves 23 and 26 are controlled to provide the desired air temperature. If cool air is desired, control valve 26 is closed while control valve 23 is opened.
- the compressed air travels through the inlet flange 12 , across the aftercooler as indicated by arrow C and out of the discharge pipe 18 , in manner similar to the standard aftercooler assembly of FIG. 1 .
- control valve 23 is closed such that the compressed air cannot enter the aftercooler 10 .
- the control valve 26 is opened such that the compressed air travels through bypass valve 24 as indicated by arrow P.
- the bypassed air reenters the discharge pipe 18 via a tee 28 .
- a check valve 29 must be provided along the discharge pipe 18 to prevent the hotter air from entering the aftercooler discharge header 15 .
- Engine and motor driven air compressors are constantly being required to be packaged in increasingly smaller enclosures.
- the inclusion of the additional piping inside of the compressor package adds complexity to the assembly and service of the compressor and also increases the cost of the unit.
- Performance of the compressor may be reduced by the additional restriction of the cooling airflow by the additional pipe work.
- the present invention provides a compressor aftercooler and an aftercooler assembly incorporating the aftercooler.
- the aftercooler has a body having an inlet header and a cooler outlet.
- the inlet header and the cooler outlet are in flow communication with a cooling area therebetween such that air passing from the inlet header to the cooler outlet is reduced in temperature.
- a bypass outlet exits directly from the inlet header such that air passing from the inlet header to the bypass outlet bypasses the cooling area.
- the aftercooler assembly further comprises a first pipe section exiting the bypass outlet and a second pipe section exiting the cooler outlet.
- the first and second pipe sections each connected with a combining tee such that flow through the first and second pipe sections flows to a common discharge.
- a first valve is positioned along the first pipe section between the bypass outlet and the common discharge and a second valve is positioned along the second pipe section between the cooler outlet and the common discharge.
- FIG. 1 is an isometric view of a standard aftercooler configuration.
- FIG. 2 is an isometric view of a standard aftercooler bypass configuration.
- FIG. 3 is an isometric view of the aftercooler of a first embodiment of the present invention.
- FIG. 4 is a top plan view of the aftercooler of FIG. 3 .
- FIG. 5 is an isometric view of an aftercooler system according to the first embodiment of the present invention.
- FIG. 6 is a top plan view of the aftercooler system of FIG. 5 with the valves positioned in a standard flow configuration.
- FIG. 7 is a top plan view of the aftercooler system of FIG. 5 with the valves positioned in a bypass flow configuration.
- the aftercooler system 50 includes an aftercooler 52 having an inlet header 57 and an outlet header 55 .
- the outlet header 55 has an outlet flange 56 similar to the outlet flange of a standard aftercooler.
- the inlet header 57 includes an inlet flange 53 entering the header 57 and an outlet flange 54 exiting the inlet header 57 , preferably directly across from the inlet flange 53 .
- Compressed air entering the inlet flange 53 can travel through the aftercooler as indicated by arrow C or may travel directly through the inlet header 57 as indicated by arrow B.
- the aftercooler assembly 50 includes a compact system of pipes 60 , 62 , 64 and valves 61 , 63 to control flow through the aftercooler 52 .
- a first pipe elbow 60 is connected to the outlet flange 54 to receive bypassed air traveling in the direction B.
- a -second pipe elbow 64 is connected to outlet flange 56 to receive air that has traveled through the aftercooler 52 as indicated by arrows C and D.
- the first and second elbows 60 , 64 are interconnected to a tee pipe 62 that provides a common discharge pipe 68 .
- the discharge pipe 68 may have a valve 30 to control flow to downstream equipment.
- a first control valve 61 is provided between the first elbow 60 and the tee 62 and a second control valve 63 is provided between the second elbow 64 and the tee 62 .
- the first control valve 61 is closed and the second control valve 63 is opened as shown in FIG. 6 .
- Air travels into the inlet flange 53 via a standard inlet pipe 14 as indicated by arrow A. Since the first control valve 61 is closed and the second control valve 63 is open, the compressed air travels across the aftercooler 52 as indicated by arrow C. The cooled air exits the outlet flange 56 as indicated by arrow D and travels through elbow 64 to the tee 62 . Since the first control valve 61 is closed, the cooled compressed air travels through the discharge pipe 68 as indicated by arrow E.
- the first control valve 61 When hot air is desired, the first control valve 61 is opened and the second control valve 63 is closed as shown in FIG. 7 . Air travels into the inlet flange 53 via a standard inlet pipe 14 as indicated by arrow A. Since the first control valve 61 is opened and the second control valve 63 is closed, the compressed air does not travel across the aftercooler 52 , but instead flows directly through the inlet header 57 and out the outlet flange 54 as indicated by arrow B. The cooled air exits the outlet flange 57 and travels through elbow 60 to the tee 62 . Since the second control valve 63 is closed, the cooled compressed air travels through the discharge pipe 68 as indicated by arrow E. The second control valve 63 prevents backflow into the outlet header 55 and therefore the check valve as in the standard bypass system is eliminated.
- valves 61 and 63 may be partially opened to provide a mixing of cool air and hot air to achieve air having a desired discharge temperature between the cool temperature and the hot temperature.
- the illustrated manual valves 61 , 63 may be replaced with automated valves, for example, solenoid valves.
- the compressor controller could than automatically control the valves to provide a desired discharge air temperature.
- the aftercooler system 50 of the present invention uses a reduced amount of piping inside the compressor enclosure.
- the reduction in piping permits greater cooling air flow, greater access for servicing of the compressor, a reduced number of components, and reduced cost of the compressor system. While the illustrated piping configuration is preferred, other piping configurations may be used.
- the outlet flange 57 may be capped and the aftercooler 52 utilized in a standard manner if such is desired. Additionally, the flow through the aftercooler 52 may be configured such that the outlet flange 56 may be provided on the inlet header 57 side of the aftercooler.
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Compressor (AREA)
Abstract
A compressor aftercooler and an aftercooler assembly incorporating the aftercooler. The aftercooler has an inlet header and a cooler outlet that are in flow communication with a cooling area therebetween such that air passing from the inlet header to the cooler outlet is reduced in temperature. A bypass outlet exits directly from the inlet header such that air passing from the inlet header to the bypass outlet bypasses the cooling area. The aftercooler assembly further comprises a valve and piping arrangement to control flow through the aftercooler.
Description
- The present invention relates to air compressor aftercoolers. More particularly, the present invention relates to an aftercooler assembly for providing hot or cool air from an air compressor.
- Engine driven and motor driven air compressors are frequently equipped with an aftercooler in the discharge circuit. As shown in
FIG. 1 , theaftercooler 10 receives air from the compressor (not shown) via aninlet pipe 14. The compressed air traveling in the direction A enters the aftercooler header 11 via aninlet flange 12. The compressed air travels across the aftercooler as indicated by arrow C. Theaftercooler 10 lowers the temperature of the compressed air being delivered to the equipment connected to the compressor. The cooled air travels from theoutlet header 15 through anoutlet flange 16 to adischarge pipe 18 as indicated by arrow D. Anoutlet valve 30 may be provided to control the flow to downstream components. The cooler air is generally required in order to precipitate moisture from the compressed air as well as protect downstream equipment from excessive temperatures. - In certain applications, such as petrochemical, steel and glass manufacturing, high temperature compressed gas is required. A method to bypass the compressor aftercooler is needed for use in these applications.
FIG. 2 illustrates a typical system for achieving bypass of theaftercooler 10. This bypass system generally incorporates an additional piping circuit around theaftercooler 10. Theinlet pipe 14 includes atee 22 with a flow path toward theinlet flange 12 and a second path through a bypass pipe 24. Afirst control valve 23 is provided before theinlet flange 12 and a second control valve 26 is provided along the bypass pipe 24. Thecontrol valves 23 and 26 are controlled to provide the desired air temperature. If cool air is desired, control valve 26 is closed whilecontrol valve 23 is opened. As such, the compressed air travels through theinlet flange 12, across the aftercooler as indicated by arrow C and out of thedischarge pipe 18, in manner similar to the standard aftercooler assembly ofFIG. 1 . If hotter air is desired,control valve 23 is closed such that the compressed air cannot enter theaftercooler 10. The control valve 26 is opened such that the compressed air travels through bypass valve 24 as indicated by arrow P. The bypassed air reenters thedischarge pipe 18 via atee 28. Acheck valve 29 must be provided along thedischarge pipe 18 to prevent the hotter air from entering theaftercooler discharge header 15. - Engine and motor driven air compressors are constantly being required to be packaged in increasingly smaller enclosures. The inclusion of the additional piping inside of the compressor package adds complexity to the assembly and service of the compressor and also increases the cost of the unit. Performance of the compressor may be reduced by the additional restriction of the cooling airflow by the additional pipe work.
- The present invention provides a compressor aftercooler and an aftercooler assembly incorporating the aftercooler. The aftercooler has a body having an inlet header and a cooler outlet. The inlet header and the cooler outlet are in flow communication with a cooling area therebetween such that air passing from the inlet header to the cooler outlet is reduced in temperature. A bypass outlet exits directly from the inlet header such that air passing from the inlet header to the bypass outlet bypasses the cooling area. The aftercooler assembly further comprises a first pipe section exiting the bypass outlet and a second pipe section exiting the cooler outlet. The first and second pipe sections each connected with a combining tee such that flow through the first and second pipe sections flows to a common discharge. A first valve is positioned along the first pipe section between the bypass outlet and the common discharge and a second valve is positioned along the second pipe section between the cooler outlet and the common discharge.
-
FIG. 1 is an isometric view of a standard aftercooler configuration. -
FIG. 2 is an isometric view of a standard aftercooler bypass configuration. -
FIG. 3 is an isometric view of the aftercooler of a first embodiment of the present invention. -
FIG. 4 is a top plan view of the aftercooler ofFIG. 3 . -
FIG. 5 is an isometric view of an aftercooler system according to the first embodiment of the present invention. -
FIG. 6 is a top plan view of the aftercooler system ofFIG. 5 with the valves positioned in a standard flow configuration. -
FIG. 7 is a top plan view of the aftercooler system ofFIG. 5 with the valves positioned in a bypass flow configuration. - The present invention will be described with reference to the accompanying drawing figures wherein like numbers represent like elements throughout. Certain terminology, for example, “top”, “bottom”, “right”, “left”, “front”, “frontward”, “forward”, “back”, “rear” and “rearward”, is used in the following description for relative descriptive clarity only and is not intended to be limiting.
- Referring to
FIGS. 3-7 , anaftercooler system 50 that is a preferred embodiment of the present invention is shown. Theaftercooler system 50 includes anaftercooler 52 having aninlet header 57 and anoutlet header 55. Theoutlet header 55 has anoutlet flange 56 similar to the outlet flange of a standard aftercooler. Theinlet header 57 includes aninlet flange 53 entering theheader 57 and anoutlet flange 54 exiting theinlet header 57, preferably directly across from theinlet flange 53. Compressed air entering theinlet flange 53 can travel through the aftercooler as indicated by arrow C or may travel directly through theinlet header 57 as indicated by arrow B. - Referring to
FIGS. 5-7 , theaftercooler assembly 50 includes a compact system ofpipes valves aftercooler 52. Afirst pipe elbow 60 is connected to theoutlet flange 54 to receive bypassed air traveling in the direction B. A -second pipe elbow 64 is connected tooutlet flange 56 to receive air that has traveled through theaftercooler 52 as indicated by arrows C and D. The first andsecond elbows tee pipe 62 that provides acommon discharge pipe 68. Thedischarge pipe 68 may have avalve 30 to control flow to downstream equipment. - To control flow through the aftercooler system 50 a
first control valve 61 is provided between thefirst elbow 60 and thetee 62 and asecond control valve 63 is provided between thesecond elbow 64 and thetee 62. When cool air is desired, thefirst control valve 61 is closed and thesecond control valve 63 is opened as shown inFIG. 6 . Air travels into theinlet flange 53 via astandard inlet pipe 14 as indicated by arrow A. Since thefirst control valve 61 is closed and thesecond control valve 63 is open, the compressed air travels across theaftercooler 52 as indicated by arrow C. The cooled air exits theoutlet flange 56 as indicated by arrow D and travels throughelbow 64 to thetee 62. Since thefirst control valve 61 is closed, the cooled compressed air travels through thedischarge pipe 68 as indicated by arrow E. - When hot air is desired, the
first control valve 61 is opened and thesecond control valve 63 is closed as shown inFIG. 7 . Air travels into theinlet flange 53 via astandard inlet pipe 14 as indicated by arrow A. Since thefirst control valve 61 is opened and thesecond control valve 63 is closed, the compressed air does not travel across theaftercooler 52, but instead flows directly through theinlet header 57 and out theoutlet flange 54 as indicated by arrow B. The cooled air exits theoutlet flange 57 and travels throughelbow 60 to thetee 62. Since thesecond control valve 63 is closed, the cooled compressed air travels through thedischarge pipe 68 as indicated by arrow E. Thesecond control valve 63 prevents backflow into theoutlet header 55 and therefore the check valve as in the standard bypass system is eliminated. - In addition to the flow described above, the
valves manual valves - The
aftercooler system 50 of the present invention uses a reduced amount of piping inside the compressor enclosure. The reduction in piping permits greater cooling air flow, greater access for servicing of the compressor, a reduced number of components, and reduced cost of the compressor system. While the illustrated piping configuration is preferred, other piping configurations may be used. Additionally, theoutlet flange 57 may be capped and theaftercooler 52 utilized in a standard manner if such is desired. Additionally, the flow through theaftercooler 52 may be configured such that theoutlet flange 56 may be provided on theinlet header 57 side of the aftercooler.
Claims (2)
1. A compressor aftercooler comprising:
a body having an inlet header and a cooler outlet, the inlet header and the cooler outlet in flow communication with a cooling area therebetween such that air passing from the inlet header to the cooler outlet is reduced in temperature; and
a bypass outlet that exits directly from the inlet header such that air passing from the inlet header to the bypass outlet bypasses the cooling area.
2. A compressor aftercooler assembly comprising:
an aftercooler having a body having
an inlet header and a cooler outlet, the inlet header and the cooler outlet in flow communication with a cooling area therebetween such that air passing from the inlet header to the cooler outlet is reduced in temperature; and
a bypass outlet that exits directly from the inlet header such that air passing from the inlet header to the bypass outlet bypasses the cooling area;
a first pipe section exiting the bypass outlet and a second pipe section exiting the cooler outlet; the first and second pipe sections each connected with a combining tee such that flow through the first and second pipe sections flows to a common discharge;
a first valve positioned along the first pipe section between the bypass outlet and the common discharge and a second valve positioned along the second pipe section between the cooler outlet and the common discharge.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/096,728 US20060219389A1 (en) | 2005-04-01 | 2005-04-01 | Air compressor aftercooler |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11/096,728 US20060219389A1 (en) | 2005-04-01 | 2005-04-01 | Air compressor aftercooler |
Publications (1)
Publication Number | Publication Date |
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US20060219389A1 true US20060219389A1 (en) | 2006-10-05 |
Family
ID=37068929
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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US11/096,728 Abandoned US20060219389A1 (en) | 2005-04-01 | 2005-04-01 | Air compressor aftercooler |
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Citations (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US267362A (en) * | 1882-11-14 | Feedeeic b | ||
US754726A (en) * | 1902-10-01 | 1904-03-15 | John Waterhouse | Air-heater. |
US1825306A (en) * | 1927-11-26 | 1931-09-29 | John M Clark | Radiator |
US2162148A (en) * | 1938-08-31 | 1939-06-13 | Wilson Engineering Corp | Air compression system of variable radiation capacity |
US2209097A (en) * | 1939-09-15 | 1940-07-23 | Westinghouse Air Brake Co | Compressed air cooling system |
US2391838A (en) * | 1945-12-25 | Air conditioning system | ||
US3227372A (en) * | 1961-09-11 | 1966-01-04 | Prokupek Stanley | Heating and cooling system and valve means therefor |
US3232340A (en) * | 1963-03-26 | 1966-02-01 | Schramm Inc | Air supply system |
US3236292A (en) * | 1962-11-15 | 1966-02-22 | Hupp Corp | High temperature heating apparatus |
US3236297A (en) * | 1961-08-23 | 1966-02-22 | Commissariat Energie Atomique | Heat removal system |
US3674980A (en) * | 1967-05-09 | 1972-07-04 | Ronson Corp | Divided flow hairdryer |
US3735809A (en) * | 1970-09-09 | 1973-05-29 | Toyota Motor Co Ltd | Fluid distribution device |
US4452301A (en) * | 1982-06-01 | 1984-06-05 | General Motors Corporation | Air conditioning and heating system air temperature control arrangement |
US4513808A (en) * | 1981-02-04 | 1985-04-30 | Hitachi, Ltd. | Automobile air conditioner |
US4604991A (en) * | 1985-09-06 | 1986-08-12 | Miller Kenneth F | Hot water preheater system |
US4798242A (en) * | 1985-05-30 | 1989-01-17 | Aisin Seiki Kabushiki Kaisha Co., Ltd. | Heat exchanger for recovering heat from exhaust gases |
US5002121A (en) * | 1988-09-13 | 1991-03-26 | Stober + Morlock Warmekraft Gesellschaft Mbh | Device at the output side of a gas turbine |
US6167956B1 (en) * | 1999-08-24 | 2001-01-02 | Westinghouse Air Brake Company | Aftercooler having bypass passage integrally formed therewith |
US6952932B2 (en) * | 1997-07-21 | 2005-10-11 | Westinghouse Air Brake Co. | Aftercooler bypass means for a locomotive compressed air system |
-
2005
- 2005-04-01 US US11/096,728 patent/US20060219389A1/en not_active Abandoned
Patent Citations (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US267362A (en) * | 1882-11-14 | Feedeeic b | ||
US2391838A (en) * | 1945-12-25 | Air conditioning system | ||
US754726A (en) * | 1902-10-01 | 1904-03-15 | John Waterhouse | Air-heater. |
US1825306A (en) * | 1927-11-26 | 1931-09-29 | John M Clark | Radiator |
US2162148A (en) * | 1938-08-31 | 1939-06-13 | Wilson Engineering Corp | Air compression system of variable radiation capacity |
US2209097A (en) * | 1939-09-15 | 1940-07-23 | Westinghouse Air Brake Co | Compressed air cooling system |
US3236297A (en) * | 1961-08-23 | 1966-02-22 | Commissariat Energie Atomique | Heat removal system |
US3227372A (en) * | 1961-09-11 | 1966-01-04 | Prokupek Stanley | Heating and cooling system and valve means therefor |
US3236292A (en) * | 1962-11-15 | 1966-02-22 | Hupp Corp | High temperature heating apparatus |
US3232340A (en) * | 1963-03-26 | 1966-02-01 | Schramm Inc | Air supply system |
US3674980A (en) * | 1967-05-09 | 1972-07-04 | Ronson Corp | Divided flow hairdryer |
US3735809A (en) * | 1970-09-09 | 1973-05-29 | Toyota Motor Co Ltd | Fluid distribution device |
US4513808A (en) * | 1981-02-04 | 1985-04-30 | Hitachi, Ltd. | Automobile air conditioner |
US4452301A (en) * | 1982-06-01 | 1984-06-05 | General Motors Corporation | Air conditioning and heating system air temperature control arrangement |
US4798242A (en) * | 1985-05-30 | 1989-01-17 | Aisin Seiki Kabushiki Kaisha Co., Ltd. | Heat exchanger for recovering heat from exhaust gases |
US4604991A (en) * | 1985-09-06 | 1986-08-12 | Miller Kenneth F | Hot water preheater system |
US5002121A (en) * | 1988-09-13 | 1991-03-26 | Stober + Morlock Warmekraft Gesellschaft Mbh | Device at the output side of a gas turbine |
US6952932B2 (en) * | 1997-07-21 | 2005-10-11 | Westinghouse Air Brake Co. | Aftercooler bypass means for a locomotive compressed air system |
US6167956B1 (en) * | 1999-08-24 | 2001-01-02 | Westinghouse Air Brake Company | Aftercooler having bypass passage integrally formed therewith |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AS | Assignment |
Owner name: INGERSOLL-RAND COMPANY, NEW JERSEY Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:HENDRIX, DEAN P.;REEL/FRAME:016215/0177 Effective date: 20050505 |
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STCB | Information on status: application discontinuation |
Free format text: ABANDONED -- FAILURE TO RESPOND TO AN OFFICE ACTION |