SEAL IN A GAS TURBINE ENGINE AND CORRESPONDING CREATING METHOD
A seal (200) in a gas turbine engine (100) includes a shim base (202) and a honeycomb structure having a number of cavities (204) are formed as a single unitary structure, for example by using additive manufacturing. Furthermore, a method of creating a seal (200) in a gas turbine engine (100), the m...
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| creator | KIRTLEY, Kevin Richard SEZER, Ibrahim LACY, Benjamin Paul |
| description | A seal (200) in a gas turbine engine (100) includes a shim base (202) and a honeycomb structure having a number of cavities (204) are formed as a single unitary structure, for example by using additive manufacturing. Furthermore, a method of creating a seal (200) in a gas turbine engine (100), the mehtod comprising the steps of forming a shim base (202) and forming a plurality of cavities (204) on the shim base (202) as a single unitary structure with the shim base (202). |
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Furthermore, a method of creating a seal (200) in a gas turbine engine (100), the mehtod comprising the steps of forming a shim base (202) and forming a plurality of cavities (204) on the shim base (202) as a single unitary structure with the shim base (202).</description><language>eng ; fre ; ger</language><subject>BLASTING ; CASTING ; ENGINE PLANTS IN GENERAL ; HEATING ; LIGHTING ; MACHINES OR ENGINES IN GENERAL ; MAKING METALLIC POWDER ; MANUFACTURE OF ARTICLES FROM METALLIC POWDER ; MECHANICAL ENGINEERING ; NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES ; PERFORMING OPERATIONS ; POWDER METALLURGY ; STEAM ENGINES ; TRANSPORTING ; WEAPONS ; WORKING METALLIC POWDER</subject><creationdate>2020</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=20200729&DB=EPODOC&CC=EP&NR=3299586B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20200729&DB=EPODOC&CC=EP&NR=3299586B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>KIRTLEY, Kevin Richard</creatorcontrib><creatorcontrib>SEZER, Ibrahim</creatorcontrib><creatorcontrib>LACY, Benjamin Paul</creatorcontrib><title>SEAL IN A GAS TURBINE ENGINE AND CORRESPONDING CREATING METHOD</title><description>A seal (200) in a gas turbine engine (100) includes a shim base (202) and a honeycomb structure having a number of cavities (204) are formed as a single unitary structure, for example by using additive manufacturing. 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Furthermore, a method of creating a seal (200) in a gas turbine engine (100), the mehtod comprising the steps of forming a shim base (202) and forming a plurality of cavities (204) on the shim base (202) as a single unitary structure with the shim base (202).</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | BLASTING CASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MAKING METALLIC POWDER MANUFACTURE OF ARTICLES FROM METALLIC POWDER MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS POWDER METALLURGY STEAM ENGINES TRANSPORTING WEAPONS WORKING METALLIC POWDER |
| title | SEAL IN A GAS TURBINE ENGINE AND CORRESPONDING CREATING METHOD |
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