ELECTRICAL TERMINAL DEVICE
An electrical terminal device (22) adapted to mount to a structure, and including a electrically non-conductive substructure (28), an electrically non-conductive cover (30), a heat resistant shroud (32), and an electric terminal (34). The substructure (28) is in contact with the structure. The cover...
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| creator | PATEL, Dhaval BEHLING, David S TURNER, Douglas J KASNER, Alan LEMMERS, Glenn C. Jr |
| description | An electrical terminal device (22) adapted to mount to a structure, and including a electrically non-conductive substructure (28), an electrically non-conductive cover (30), a heat resistant shroud (32), and an electric terminal (34). The substructure (28) is in contact with the structure. The cover (30) is engaged to the substructure (28). The substructure (28) and the cover (30) define a chamber, and the substructure (28) defines, at least in-part, a sealed passage in communication with the chamber. The heat resistant shroud (32) substantially covers the cover (30). The cover (30) is substantially located between the shroud (32) and the substructure (28). The electric terminal (34) is located in the chamber and is attached to the substructure (28). |
| format | Patent |
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Jr</creatorcontrib><description>An electrical terminal device (22) adapted to mount to a structure, and including a electrically non-conductive substructure (28), an electrically non-conductive cover (30), a heat resistant shroud (32), and an electric terminal (34). The substructure (28) is in contact with the structure. The cover (30) is engaged to the substructure (28). The substructure (28) and the cover (30) define a chamber, and the substructure (28) defines, at least in-part, a sealed passage in communication with the chamber. The heat resistant shroud (32) substantially covers the cover (30). The cover (30) is substantially located between the shroud (32) and the substructure (28). The electric terminal (34) is located in the chamber and is attached to the substructure (28).</description><language>eng ; fre ; ger</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BASIC ELECTRIC ELEMENTS ; COSMONAUTICS ; CURRENT COLLECTORS ; ELECTRICITY ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; LINE CONNECTORS ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2019</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=20190306&DB=EPODOC&CC=EP&NR=3451462A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20190306&DB=EPODOC&CC=EP&NR=3451462A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PATEL, Dhaval</creatorcontrib><creatorcontrib>BEHLING, David S</creatorcontrib><creatorcontrib>TURNER, Douglas J</creatorcontrib><creatorcontrib>KASNER, Alan</creatorcontrib><creatorcontrib>LEMMERS, Glenn C. Jr</creatorcontrib><title>ELECTRICAL TERMINAL DEVICE</title><description>An electrical terminal device (22) adapted to mount to a structure, and including a electrically non-conductive substructure (28), an electrically non-conductive cover (30), a heat resistant shroud (32), and an electric terminal (34). The substructure (28) is in contact with the structure. The cover (30) is engaged to the substructure (28). The substructure (28) and the cover (30) define a chamber, and the substructure (28) defines, at least in-part, a sealed passage in communication with the chamber. The heat resistant shroud (32) substantially covers the cover (30). The cover (30) is substantially located between the shroud (32) and the substructure (28). The electric terminal (34) is located in the chamber and is attached to the substructure (28).</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BASIC ELECTRIC ELEMENTS</subject><subject>COSMONAUTICS</subject><subject>CURRENT COLLECTORS</subject><subject>ELECTRICITY</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>LINE CONNECTORS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2019</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJBy9XF1DgnydHb0UQhxDfL19AMyXFzDPJ1deRhY0xJzilN5oTQ3g4Kba4izh25qQX58anFBYnJqXmpJvGuAsYmpoYmZkaOhMRFKAOyMH78</recordid><startdate>20190306</startdate><enddate>20190306</enddate><creator>PATEL, Dhaval</creator><creator>BEHLING, David S</creator><creator>TURNER, Douglas J</creator><creator>KASNER, Alan</creator><creator>LEMMERS, Glenn C. Jr</creator><scope>EVB</scope></search><sort><creationdate>20190306</creationdate><title>ELECTRICAL TERMINAL DEVICE</title><author>PATEL, Dhaval ; BEHLING, David S ; TURNER, Douglas J ; KASNER, Alan ; LEMMERS, Glenn C. 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Jr</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PATEL, Dhaval</au><au>BEHLING, David S</au><au>TURNER, Douglas J</au><au>KASNER, Alan</au><au>LEMMERS, Glenn C. Jr</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>ELECTRICAL TERMINAL DEVICE</title><date>2019-03-06</date><risdate>2019</risdate><abstract>An electrical terminal device (22) adapted to mount to a structure, and including a electrically non-conductive substructure (28), an electrically non-conductive cover (30), a heat resistant shroud (32), and an electric terminal (34). The substructure (28) is in contact with the structure. The cover (30) is engaged to the substructure (28). The substructure (28) and the cover (30) define a chamber, and the substructure (28) defines, at least in-part, a sealed passage in communication with the chamber. The heat resistant shroud (32) substantially covers the cover (30). The cover (30) is substantially located between the shroud (32) and the substructure (28). The electric terminal (34) is located in the chamber and is attached to the substructure (28).</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BASIC ELECTRIC ELEMENTS COSMONAUTICS CURRENT COLLECTORS ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS LINE CONNECTORS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | ELECTRICAL TERMINAL DEVICE |
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