REDUCED LOSS SWEPT SUPERSONIC FAN BLADE
A swept leading edge blade (10) rotates in a stream of air (26) and experiences supersonic relative air velocities over at least a portion of the blade surface. The maximum camber points (28, 40) of adjacent blade segments (20, 18) are located to prevent intensification of the compression wave gener...
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| creator | WALTER B. HARVEY HARRIS D. WEINGOLD |
| description | A swept leading edge blade (10) rotates in a stream of air (26) and experiences supersonic relative air velocities over at least a portion of the blade surface. The maximum camber points (28, 40) of adjacent blade segments (20, 18) are located to prevent intensification of the compression wave generated by each segment (20, 18). |
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| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_AU8049987A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>AU8049987A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_AU8049987A3</originalsourceid><addsrcrecordid>eNrjZFAPcnUJdXZ1UfDxDw5WCA53DQhRCA4NcA0K9vfzdFZwc_RTcPJxdHHlYWBNS8wpTuWF0twM8m6uIc4euqkF-fGpxQWJyal5qSXxjqEWBiaWlhbmjsaEVQAAWssjFg</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>REDUCED LOSS SWEPT SUPERSONIC FAN BLADE</title><source>esp@cenet</source><creator>WALTER B. HARVEY ; HARRIS D. WEINGOLD</creator><creatorcontrib>WALTER B. HARVEY ; HARRIS D. WEINGOLD</creatorcontrib><description>A swept leading edge blade (10) rotates in a stream of air (26) and experiences supersonic relative air velocities over at least a portion of the blade surface. The maximum camber points (28, 40) of adjacent blade segments (20, 18) are located to prevent intensification of the compression wave generated by each segment (20, 18).</description><edition>4</edition><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; ENGINE PLANTS IN GENERAL ; HEATING ; HELICOPTERS ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; NON-POSITIVE DISPLACEMENT PUMPS ; PERFORMING OPERATIONS ; POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS ; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS ; STEAM ENGINES ; TRANSPORTING ; WEAPONS</subject><creationdate>1988</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=19880505&DB=EPODOC&CC=AU&NR=8049987A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19880505&DB=EPODOC&CC=AU&NR=8049987A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>WALTER B. HARVEY</creatorcontrib><creatorcontrib>HARRIS D. WEINGOLD</creatorcontrib><title>REDUCED LOSS SWEPT SUPERSONIC FAN BLADE</title><description>A swept leading edge blade (10) rotates in a stream of air (26) and experiences supersonic relative air velocities over at least a portion of the blade surface. The maximum camber points (28, 40) of adjacent blade segments (20, 18) are located to prevent intensification of the compression wave generated by each segment (20, 18).</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>ENGINE PLANTS IN GENERAL</subject><subject>HEATING</subject><subject>HELICOPTERS</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>NON-POSITIVE DISPLACEMENT PUMPS</subject><subject>PERFORMING OPERATIONS</subject><subject>POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS</subject><subject>PUMPS FOR LIQUIDS OR ELASTIC FLUIDS</subject><subject>STEAM ENGINES</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1988</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZFAPcnUJdXZ1UfDxDw5WCA53DQhRCA4NcA0K9vfzdFZwc_RTcPJxdHHlYWBNS8wpTuWF0twM8m6uIc4euqkF-fGpxQWJyal5qSXxjqEWBiaWlhbmjsaEVQAAWssjFg</recordid><startdate>19880505</startdate><enddate>19880505</enddate><creator>WALTER B. HARVEY</creator><creator>HARRIS D. WEINGOLD</creator><scope>EVB</scope></search><sort><creationdate>19880505</creationdate><title>REDUCED LOSS SWEPT SUPERSONIC FAN BLADE</title><author>WALTER B. HARVEY ; HARRIS D. 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HARVEY</creatorcontrib><creatorcontrib>HARRIS D. WEINGOLD</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>WALTER B. HARVEY</au><au>HARRIS D. WEINGOLD</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>REDUCED LOSS SWEPT SUPERSONIC FAN BLADE</title><date>1988-05-05</date><risdate>1988</risdate><abstract>A swept leading edge blade (10) rotates in a stream of air (26) and experiences supersonic relative air velocities over at least a portion of the blade surface. The maximum camber points (28, 40) of adjacent blade segments (20, 18) are located to prevent intensification of the compression wave generated by each segment (20, 18).</abstract><edition>4</edition><oa>free_for_read</oa></addata></record> |
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| language | eng |
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| subjects | AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINE PLANTS IN GENERAL HEATING HELICOPTERS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS PERFORMING OPERATIONS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES TRANSPORTING WEAPONS |
| title | REDUCED LOSS SWEPT SUPERSONIC FAN BLADE |
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