METHODS OF MODIFYING TURBINE ENGINE OPERATING LIMITS
The present disclosure is directed to systems and methods of modifying turbine engine operating limits due to the intake of particulate matter. More specifically, the present disclosure is directed to the use of a sensor at the inlet of a turbine engine to measure the characteristics of particulate...
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| creator | Hodge, C. Edward |
| description | The present disclosure is directed to systems and methods of modifying turbine engine operating limits due to the intake of particulate matter. More specifically, the present disclosure is directed to the use of a sensor at the inlet of a turbine engine to measure the characteristics of particulate flow into the turbine engine such as the volume, density, flow rate, size, shape, and surface type of particulate matter. Based on these measurements, the operating limits of the turbine engine are adjusted due to known degrading effects of particulate matter intake. The adjusted operating limits may include real-time operating limits such as maximum temperature and pressure, or long-range operating limits such as engine lifespan and maintenance cycles. |
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More specifically, the present disclosure is directed to the use of a sensor at the inlet of a turbine engine to measure the characteristics of particulate flow into the turbine engine such as the volume, density, flow rate, size, shape, and surface type of particulate matter. Based on these measurements, the operating limits of the turbine engine are adjusted due to known degrading effects of particulate matter intake. The adjusted operating limits may include real-time operating limits such as maximum temperature and pressure, or long-range operating limits such as engine lifespan and maintenance cycles.</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 ; CONTROL OR REGULATING SYSTEMS IN GENERAL ; CONTROLLING ; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES ; LIGHTING ; MEASURING ; MECHANICAL ENGINEERING ; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS ; PARACHUTES ; PERFORMING OPERATIONS ; PHYSICS ; REGULATING ; TESTING ; TRANSPORTING ; WEAPONS</subject><creationdate>2018</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=20180307&DB=EPODOC&CC=EP&NR=3290342A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20180307&DB=EPODOC&CC=EP&NR=3290342A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Hodge, C. Edward</creatorcontrib><title>METHODS OF MODIFYING TURBINE ENGINE OPERATING LIMITS</title><description>The present disclosure is directed to systems and methods of modifying turbine engine operating limits due to the intake of particulate matter. More specifically, the present disclosure is directed to the use of a sensor at the inlet of a turbine engine to measure the characteristics of particulate flow into the turbine engine such as the volume, density, flow rate, size, shape, and surface type of particulate matter. Based on these measurements, the operating limits of the turbine engine are adjusted due to known degrading effects of particulate matter intake. 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Edward</creator><scope>EVB</scope></search><sort><creationdate>20180307</creationdate><title>METHODS OF MODIFYING TURBINE ENGINE OPERATING LIMITS</title><author>Hodge, C. Edward</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3290342A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2018</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>CONTROL OR REGULATING SYSTEMS IN GENERAL</topic><topic>CONTROLLING</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>FUNCTIONAL ELEMENTS OF SUCH SYSTEMS</topic><topic>GAS-TURBINE PLANTS</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES</topic><topic>LIGHTING</topic><topic>MEASURING</topic><topic>MECHANICAL ENGINEERING</topic><topic>MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>PHYSICS</topic><topic>REGULATING</topic><topic>TESTING</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Hodge, C. Edward</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Hodge, C. Edward</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>METHODS OF MODIFYING TURBINE ENGINE OPERATING LIMITS</title><date>2018-03-07</date><risdate>2018</risdate><abstract>The present disclosure is directed to systems and methods of modifying turbine engine operating limits due to the intake of particulate matter. More specifically, the present disclosure is directed to the use of a sensor at the inlet of a turbine engine to measure the characteristics of particulate flow into the turbine engine such as the volume, density, flow rate, size, shape, and surface type of particulate matter. Based on these measurements, the operating limits of the turbine engine are adjusted due to known degrading effects of particulate matter intake. The adjusted operating limits may include real-time operating limits such as maximum temperature and pressure, or long-range operating limits such as engine lifespan and maintenance cycles.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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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 CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS FUNCTIONAL ELEMENTS OF SUCH SYSTEMS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIRCHEMICAL OR PHYSICAL PROPERTIES LIGHTING MEASURING MECHANICAL ENGINEERING MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PARACHUTES PERFORMING OPERATIONS PHYSICS REGULATING TESTING TRANSPORTING WEAPONS |
| title | METHODS OF MODIFYING TURBINE ENGINE OPERATING LIMITS |
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