Carbon-carbon stator insert for aircraft brakes

The present invention relates to annular drive inserts which are placed within an annular opening within the brake disk. Preferably the annular drive inserts comprise carbon-carbon composite which has been treated with antioxidant. In a highly preferred embodiment the treatment is accomplished by va...

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Hauptverfasser: BOOKER LAURIE A, WALKER TERENCE B, WAGHRAY AKSHAY
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Sprache:eng
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creator BOOKER LAURIE A
WALKER TERENCE B
WAGHRAY AKSHAY
description The present invention relates to annular drive inserts which are placed within an annular opening within the brake disk. Preferably the annular drive inserts comprise carbon-carbon composite which has been treated with antioxidant. In a highly preferred embodiment the treatment is accomplished by vacuum impregnation. The antioxidant generally comprises a standard phosphoric acid based solution. This invention solves a need in the art for annular drive inserts that have improved resistance to oxidation and strength.
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Preferably the annular drive inserts comprise carbon-carbon composite which has been treated with antioxidant. In a highly preferred embodiment the treatment is accomplished by vacuum impregnation. The antioxidant generally comprises a standard phosphoric acid based solution. This invention solves a need in the art for annular drive inserts that have improved resistance to oxidation and strength.</description><language>eng</language><subject>BLASTING ; BRAKES ; CLUTCHES ; COUPLINGS FOR TRANSMITTING ROTATION ; ENGINEERING ELEMENTS AND UNITS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; THERMAL INSULATION IN GENERAL ; WEAPONS</subject><creationdate>2008</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&amp;date=20080221&amp;DB=EPODOC&amp;CC=US&amp;NR=2008041674A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20080221&amp;DB=EPODOC&amp;CC=US&amp;NR=2008041674A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>BOOKER LAURIE A</creatorcontrib><creatorcontrib>WALKER TERENCE B</creatorcontrib><creatorcontrib>WAGHRAY AKSHAY</creatorcontrib><title>Carbon-carbon stator insert for aircraft brakes</title><description>The present invention relates to annular drive inserts which are placed within an annular opening within the brake disk. 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Preferably the annular drive inserts comprise carbon-carbon composite which has been treated with antioxidant. In a highly preferred embodiment the treatment is accomplished by vacuum impregnation. The antioxidant generally comprises a standard phosphoric acid based solution. This invention solves a need in the art for annular drive inserts that have improved resistance to oxidation and strength.</abstract><oa>free_for_read</oa></addata></record>
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subjects BLASTING
BRAKES
CLUTCHES
COUPLINGS FOR TRANSMITTING ROTATION
ENGINEERING ELEMENTS AND UNITS
GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS
HEATING
LIGHTING
MECHANICAL ENGINEERING
THERMAL INSULATION IN GENERAL
WEAPONS
title Carbon-carbon stator insert for aircraft brakes
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