System of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans
According to one embodiment of the invention, a system for altering a fluid flow includes a nozzle having a fluid flow and including a converging portion, a diverging portion downstream of the converging portion, and a throat coupling the converging portion to the diverging portion, at least one por...
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creator | HUNTER LOUIS G HAGSETH PAUL E MILLER DANIEL N |
description | According to one embodiment of the invention, a system for altering a fluid flow includes a nozzle having a fluid flow and including a converging portion, a diverging portion downstream of the converging portion, and a throat coupling the converging portion to the diverging portion, at least one port located in a wall of the nozzle and angled with respect to the fluid flow, and at least one pulse detonation device operable to inject a plurality of detonation waves in a pulsed manner through the port and into the fluid flow. The pulsed detonation waves operate to alter the fluid flow. |
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The pulsed detonation waves operate to alter the fluid flow.</description><edition>7</edition><language>eng</language><subject>BLASTING ; COMBUSTION ENGINES ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2004</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=20040706&DB=EPODOC&CC=US&NR=6758032B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20040706&DB=EPODOC&CC=US&NR=6758032B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>HUNTER LOUIS G</creatorcontrib><creatorcontrib>HAGSETH PAUL E</creatorcontrib><creatorcontrib>MILLER DANIEL N</creatorcontrib><title>System of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans</title><description>According to one embodiment of the invention, a system for altering a fluid flow includes a nozzle having a fluid flow and including a converging portion, a diverging portion downstream of the converging portion, and a throat coupling the converging portion to the diverging portion, at least one port located in a wall of the nozzle and angled with respect to the fluid flow, and at least one pulse detonation device operable to inject a plurality of detonation waves in a pulsed manner through the port and into the fluid flow. The pulsed detonation waves operate to alter the fluid flow.</description><subject>BLASTING</subject><subject>COMBUSTION ENGINES</subject><subject>HEATING</subject><subject>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</subject><subject>JET-PROPULSION PLANTS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2004</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjE0KwjAQhbNxIeod5gAK0uLPWlHcV7eWkEwgZZwJzRSxpzeKB3Dz3rf43puae_PKig-QAGmgjB48qrDVKAyRO3RfCtJDoCH6kvIEJ6y90GcVmVDzEljGkbCAZQ8Ug0KwnOdmEmy5Xfx6ZuB8uh4vK0zSYk7WIaO2t2a72-zXdXWo6j-UN8JEPCM</recordid><startdate>20040706</startdate><enddate>20040706</enddate><creator>HUNTER LOUIS G</creator><creator>HAGSETH PAUL E</creator><creator>MILLER DANIEL N</creator><scope>EVB</scope></search><sort><creationdate>20040706</creationdate><title>System of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans</title><author>HUNTER LOUIS G ; HAGSETH PAUL E ; MILLER DANIEL N</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US6758032B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2004</creationdate><topic>BLASTING</topic><topic>COMBUSTION ENGINES</topic><topic>HEATING</topic><topic>HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS</topic><topic>JET-PROPULSION PLANTS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>HUNTER LOUIS G</creatorcontrib><creatorcontrib>HAGSETH PAUL E</creatorcontrib><creatorcontrib>MILLER DANIEL N</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>HUNTER LOUIS G</au><au>HAGSETH PAUL E</au><au>MILLER DANIEL N</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>System of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans</title><date>2004-07-06</date><risdate>2004</risdate><abstract>According to one embodiment of the invention, a system for altering a fluid flow includes a nozzle having a fluid flow and including a converging portion, a diverging portion downstream of the converging portion, and a throat coupling the converging portion to the diverging portion, at least one port located in a wall of the nozzle and angled with respect to the fluid flow, and at least one pulse detonation device operable to inject a plurality of detonation waves in a pulsed manner through the port and into the fluid flow. The pulsed detonation waves operate to alter the fluid flow.</abstract><edition>7</edition><oa>free_for_read</oa></addata></record> |
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subjects | BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS |
title | System of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans |
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