ROTATING DEVICES FOR MITIGATION OF ADVERSE FLOW CONDITIONS IN AN ULTRA-SHORT NACELLE INLET
A flow control system on an aircraft engine nacelle incorporates a plurality of flow control devices each having a body. A second plurality of actuators is coupled to the body of an associated one of the flow control devices. The actuator rotates the body about a leading edge of an inlet of a nacell...
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| creator | Dorsey, Andrew M Hoffman, Drew C Hoisington, Zachary C Palacios, Francisco D |
| description | A flow control system on an aircraft engine nacelle incorporates a plurality of flow control devices each having a body. A second plurality of actuators is coupled to the body of an associated one of the flow control devices. The actuator rotates the body about a leading edge of an inlet of a nacelle from a retracted position to an extended position. |
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A second plurality of actuators is coupled to the body of an associated one of the flow control devices. The actuator rotates the body about a leading edge of an inlet of a nacelle from a retracted position to an extended position.</description><language>eng</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 ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GAS-TURBINE PLANTS ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; PARACHUTES ; PERFORMING OPERATIONS ; 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=20181227&DB=EPODOC&CC=US&NR=2018371995A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,778,883,25547,76298</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20181227&DB=EPODOC&CC=US&NR=2018371995A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Dorsey, Andrew M</creatorcontrib><creatorcontrib>Hoffman, Drew C</creatorcontrib><creatorcontrib>Hoisington, Zachary C</creatorcontrib><creatorcontrib>Palacios, Francisco D</creatorcontrib><title>ROTATING DEVICES FOR MITIGATION OF ADVERSE FLOW CONDITIONS IN AN ULTRA-SHORT NACELLE INLET</title><description>A flow control system on an aircraft engine nacelle incorporates a plurality of flow control devices each having a body. A second plurality of actuators is coupled to the body of an associated one of the flow control devices. 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A second plurality of actuators is coupled to the body of an associated one of the flow control devices. The actuator rotates the body about a leading edge of an inlet of a nacelle from a retracted position to an extended position.</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 EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS |
| title | ROTATING DEVICES FOR MITIGATION OF ADVERSE FLOW CONDITIONS IN AN ULTRA-SHORT NACELLE INLET |
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