System and method for providing air to a compresssor of an aircraft auxiliary gas turbine engine
A system (10) for providing air (12) to a compressor (16) of an auxiliary gas turbine engine (18) of an aircraft (20). A system turbine (26) has an inlet (30) adapted to receive compressed air (34) from the aircraft. A system compressor (28) is mechanically coupled to the system turbine and has an i...
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| creator | TURCO, JOHN SHELDON, KARL EDWARD |
| description | A system (10) for providing air (12) to a compressor (16) of an auxiliary gas turbine engine (18) of an aircraft (20). A system turbine (26) has an inlet (30) adapted to receive compressed air (34) from the aircraft. A system compressor (28) is mechanically coupled to the system turbine and has an inlet (36) adapted to receive atmospheric air (40). The outlets of the system turbine and the system compressor arc fluidly connectable to the inlet of the compressor of the auxiliary gas turbine engine. |
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A system turbine (26) has an inlet (30) adapted to receive compressed air (34) from the aircraft. A system compressor (28) is mechanically coupled to the system turbine and has an inlet (36) adapted to receive atmospheric air (40). The outlets of the system turbine and the system compressor arc fluidly connectable to the inlet of the compressor of the auxiliary gas turbine engine.</description><language>eng ; fre ; ger</language><subject>AIR INTAKES FOR JET-PROPULSION PLANTS ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COMBUSTION ENGINES ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; COSMONAUTICS ; ENGINE PLANTS IN GENERAL ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PARACHUTES ; PERFORMING OPERATIONS ; STEAM ENGINES ; TRANSPORTING ; WEAPONS</subject><creationdate>2007</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=20071010&DB=EPODOC&CC=EP&NR=1843022A2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20071010&DB=EPODOC&CC=EP&NR=1843022A2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>TURCO, JOHN</creatorcontrib><creatorcontrib>SHELDON, KARL EDWARD</creatorcontrib><title>System and method for providing air to a compresssor of an aircraft auxiliary gas turbine engine</title><description>A system (10) for providing air (12) to a compressor (16) of an auxiliary gas turbine engine (18) of an aircraft (20). A system turbine (26) has an inlet (30) adapted to receive compressed air (34) from the aircraft. A system compressor (28) is mechanically coupled to the system turbine and has an inlet (36) adapted to receive atmospheric air (40). The outlets of the system turbine and the system compressor arc fluidly connectable to the inlet of the compressor of the auxiliary gas turbine engine.</description><subject>AIR INTAKES FOR JET-PROPULSION PLANTS</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</subject><subject>COSMONAUTICS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GAS-TURBINE PLANTS</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>LIGHTING</subject><subject>MACHINES OR ENGINES IN GENERAL</subject><subject>MECHANICAL ENGINEERING</subject><subject>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>STEAM ENGINES</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2007</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNizEKwkAQRdNYiHqHfwFBEwtbkYiloH0ck9m4kOwsMxsxtzeCB7B6xXtvnt2voyXuQaFBz-kpDZwoosrLNz60IK9IAkItfVQ2s0mLm4avqpVcAg1v33nSES0Z0qAPHxgc2gnLbOaoM179uMhwKm_H85qjVGyRag6cqvKy3e-KTZ4f8uKP5AMyOjy9</recordid><startdate>20071010</startdate><enddate>20071010</enddate><creator>TURCO, JOHN</creator><creator>SHELDON, KARL EDWARD</creator><scope>EVB</scope></search><sort><creationdate>20071010</creationdate><title>System and method for providing air to a compresssor of an aircraft auxiliary gas turbine engine</title><author>TURCO, JOHN ; SHELDON, KARL EDWARD</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP1843022A23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2007</creationdate><topic>AIR INTAKES FOR JET-PROPULSION PLANTS</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS</topic><topic>COSMONAUTICS</topic><topic>ENGINE PLANTS IN GENERAL</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>LIGHTING</topic><topic>MACHINES OR ENGINES IN GENERAL</topic><topic>MECHANICAL ENGINEERING</topic><topic>NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>STEAM ENGINES</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>TURCO, JOHN</creatorcontrib><creatorcontrib>SHELDON, KARL EDWARD</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>TURCO, JOHN</au><au>SHELDON, KARL EDWARD</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>System and method for providing air to a compresssor of an aircraft auxiliary gas turbine engine</title><date>2007-10-10</date><risdate>2007</risdate><abstract>A system (10) for providing air (12) to a compressor (16) of an auxiliary gas turbine engine (18) of an aircraft (20). A system turbine (26) has an inlet (30) adapted to receive compressed air (34) from the aircraft. A system compressor (28) is mechanically coupled to the system turbine and has an inlet (36) adapted to receive atmospheric air (40). The outlets of the system turbine and the system compressor arc fluidly connectable to the inlet of the compressor of the auxiliary gas turbine engine.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS ENGINE PLANTS IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PARACHUTES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS |
| title | System and method for providing air to a compresssor of an aircraft auxiliary gas turbine engine |
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