MULTI-PORT COMPRESSOR MANIFOLD WITH INTEGRAL BYPASS VALVE
A compressor manifold (100) includes a primary section (104) having a primary inlet port (110), a first primary outlet port (112), and a second primary outlet port (114), the primary section (104) configured to receive a fluid from a primary heat exchanger (22) through the primary inlet port (110) a...
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| creator | ARMY, Jr., Donald E |
| description | A compressor manifold (100) includes a primary section (104) having a primary inlet port (110), a first primary outlet port (112), and a second primary outlet port (114), the primary section (104) configured to receive a fluid from a primary heat exchanger (22) through the primary inlet port (110) and direct the fluid to at least one compressor (42) through the first and second primary outlet ports (112, 114). A secondary section (106) includes a first secondary inlet port (116), a second secondary inlet port (118), and a secondary outlet port (120), the secondary section (106) configured to receive the fluid from the at least one compressor (42) through the first and second secondary inlet ports (116, 118) and direct the fluid to a secondary heat exchanger (26) through the secondary outlet port (120). A bypass valve (102) is positioned between the primary section (104) and the secondary section (106) to fluidly couple the primary section (104) and the secondary section (106) to bypass the at least one compressor (42). |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2985224B1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2985224B1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2985224B13</originalsourceid><addsrcrecordid>eNrjZLD0DfUJ8dQN8A8KUXD29w0Icg0O9g9S8HX083Tz93FRCPcM8VDw9AtxdQ9y9FFwigxwDA5WCHP0CXPlYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgFGlhamRkYmTobGRCgBAGyoKMA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>MULTI-PORT COMPRESSOR MANIFOLD WITH INTEGRAL BYPASS VALVE</title><source>esp@cenet</source><creator>ARMY, Jr., Donald E</creator><creatorcontrib>ARMY, Jr., Donald E</creatorcontrib><description>A compressor manifold (100) includes a primary section (104) having a primary inlet port (110), a first primary outlet port (112), and a second primary outlet port (114), the primary section (104) configured to receive a fluid from a primary heat exchanger (22) through the primary inlet port (110) and direct the fluid to at least one compressor (42) through the first and second primary outlet ports (112, 114). A secondary section (106) includes a first secondary inlet port (116), a second secondary inlet port (118), and a secondary outlet port (120), the secondary section (106) configured to receive the fluid from the at least one compressor (42) through the first and second secondary inlet ports (116, 118) and direct the fluid to a secondary heat exchanger (26) through the secondary outlet port (120). A bypass valve (102) is positioned between the primary section (104) and the secondary section (106) to fluidly couple the primary section (104) and the secondary section (106) to bypass the at least one compressor (42).</description><language>eng ; fre ; ger</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COMBINED HEATING AND REFRIGERATION SYSTEMS ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GAS-TURBINE PLANTS ; HEAT PUMP SYSTEMS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; LIQUEFACTION SOLIDIFICATION OF GASES ; MANUFACTURE OR STORAGE OF ICE ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; RANGES ; REFRIGERATION MACHINES, PLANTS OR SYSTEMS ; REFRIGERATION OR COOLING ; TRANSPORTING ; VENTILATING ; WEAPONS</subject><creationdate>2019</creationdate><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190619&DB=EPODOC&CC=EP&NR=2985224B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190619&DB=EPODOC&CC=EP&NR=2985224B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ARMY, Jr., Donald E</creatorcontrib><title>MULTI-PORT COMPRESSOR MANIFOLD WITH INTEGRAL BYPASS VALVE</title><description>A compressor manifold (100) includes a primary section (104) having a primary inlet port (110), a first primary outlet port (112), and a second primary outlet port (114), the primary section (104) configured to receive a fluid from a primary heat exchanger (22) through the primary inlet port (110) and direct the fluid to at least one compressor (42) through the first and second primary outlet ports (112, 114). A secondary section (106) includes a first secondary inlet port (116), a second secondary inlet port (118), and a secondary outlet port (120), the secondary section (106) configured to receive the fluid from the at least one compressor (42) through the first and second secondary inlet ports (116, 118) and direct the fluid to a secondary heat exchanger (26) through the secondary outlet port (120). A bypass valve (102) is positioned between the primary section (104) and the secondary section (106) to fluidly couple the primary section (104) and the secondary section (106) to bypass the at least one compressor (42).</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COMBINED HEATING AND REFRIGERATION SYSTEMS</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEAT PUMP SYSTEMS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>LIQUEFACTION SOLIDIFICATION OF GASES</subject><subject>MANUFACTURE OR STORAGE OF ICE</subject><subject>MECHANICAL ENGINEERING</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>RANGES</subject><subject>REFRIGERATION MACHINES, PLANTS OR SYSTEMS</subject><subject>REFRIGERATION OR COOLING</subject><subject>TRANSPORTING</subject><subject>VENTILATING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZLD0DfUJ8dQN8A8KUXD29w0Icg0O9g9S8HX083Tz93FRCPcM8VDw9AtxdQ9y9FFwigxwDA5WCHP0CXPlYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgFGlhamRkYmTobGRCgBAGyoKMA</recordid><startdate>20190619</startdate><enddate>20190619</enddate><creator>ARMY, Jr., Donald E</creator><scope>EVB</scope></search><sort><creationdate>20190619</creationdate><title>MULTI-PORT COMPRESSOR MANIFOLD WITH INTEGRAL BYPASS VALVE</title><author>ARMY, Jr., Donald E</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2985224B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2019</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COMBINED HEATING AND REFRIGERATION SYSTEMS</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEAT PUMP SYSTEMS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>LIQUEFACTION SOLIDIFICATION OF GASES</topic><topic>MANUFACTURE OR STORAGE OF ICE</topic><topic>MECHANICAL ENGINEERING</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>RANGES</topic><topic>REFRIGERATION MACHINES, PLANTS OR SYSTEMS</topic><topic>REFRIGERATION OR COOLING</topic><topic>TRANSPORTING</topic><topic>VENTILATING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>ARMY, Jr., Donald E</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ARMY, Jr., Donald E</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>MULTI-PORT COMPRESSOR MANIFOLD WITH INTEGRAL BYPASS VALVE</title><date>2019-06-19</date><risdate>2019</risdate><abstract>A compressor manifold (100) includes a primary section (104) having a primary inlet port (110), a first primary outlet port (112), and a second primary outlet port (114), the primary section (104) configured to receive a fluid from a primary heat exchanger (22) through the primary inlet port (110) and direct the fluid to at least one compressor (42) through the first and second primary outlet ports (112, 114). A secondary section (106) includes a first secondary inlet port (116), a second secondary inlet port (118), and a secondary outlet port (120), the secondary section (106) configured to receive the fluid from the at least one compressor (42) through the first and second secondary inlet ports (116, 118) and direct the fluid to a secondary heat exchanger (26) through the secondary outlet port (120). A bypass valve (102) is positioned between the primary section (104) and the secondary section (106) to fluidly couple the primary section (104) and the secondary section (106) to bypass the at least one compressor (42).</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| source | esp@cenet |
| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS AIR-CONDITIONING, AIR-HUMIDIFICATION, VENTILATION, USE OF AIRCURRENTS FOR SCREENING AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBINED HEATING AND REFRIGERATION SYSTEMS COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEAT PUMP SYSTEMS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING LIQUEFACTION SOLIDIFICATION OF GASES MANUFACTURE OR STORAGE OF ICE MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS RANGES REFRIGERATION MACHINES, PLANTS OR SYSTEMS REFRIGERATION OR COOLING TRANSPORTING VENTILATING WEAPONS |
| title | MULTI-PORT COMPRESSOR MANIFOLD WITH INTEGRAL BYPASS VALVE |
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