Torque pads for aircraft brake systems and aircraft brake system including same

Torque pads for aircraft brake systems and aircraft brake system including same

An aircraft brake system ( 42 ) includes a torque tube ( 44 ), a plurality of spaced stators ( 48 ) mounted on the torque tube ( 44 ), a wheel ( 40 ) surrounding the torque tube ( 44 ) and a plurality of rotors ( 50 ) connected to the wheel ( 40 ) and projecting into the spaces between adjacent ones...

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Hauptverfasser: SARVER CHARLES F, CRESS JAMES J
Format: Patent
Sprache:eng
Schlagworte:
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
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creator SARVER CHARLES F
CRESS JAMES J
description An aircraft brake system ( 42 ) includes a torque tube ( 44 ), a plurality of spaced stators ( 48 ) mounted on the torque tube ( 44 ), a wheel ( 40 ) surrounding the torque tube ( 44 ) and a plurality of rotors ( 50 ) connected to the wheel ( 40 ) and projecting into the spaces between adjacent ones of the stators ( 48 ). A backing plate ( 52 ) mounted on the torque tube ( 44 ) has a first side ( 54 ) facing the rotors ( 50 ) and a second side ( 56 ) facing away from the rotors ( 50 ), and the second side ( 56 ) includes a plurality of keyways ( 58 ). A plurality of torque pads ( 10, 70, 100, 120 ) are connected to the torque tube ( 44 ), each having a body ( 12, 72, 102, 122 ) with a first surface ( 14, 74, 104, 124 ) contacting the second side ( 56 ) of the backing plate ( 52 ) and at least one key ( 22, 82, 112, 114, 130, 132 ) projecting from the first surface ( 14, 74, 104, 124 ) into one of the plurality of keyways ( 58 ). Also a torque pad ( 10, 70, 100, 120 ) and a method of connecting a backing plate to a torque tube.
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A backing plate ( 52 ) mounted on the torque tube ( 44 ) has a first side ( 54 ) facing the rotors ( 50 ) and a second side ( 56 ) facing away from the rotors ( 50 ), and the second side ( 56 ) includes a plurality of keyways ( 58 ). A plurality of torque pads ( 10, 70, 100, 120 ) are connected to the torque tube ( 44 ), each having a body ( 12, 72, 102, 122 ) with a first surface ( 14, 74, 104, 124 ) contacting the second side ( 56 ) of the backing plate ( 52 ) and at least one key ( 22, 82, 112, 114, 130, 132 ) projecting from the first surface ( 14, 74, 104, 124 ) into one of the plurality of keyways ( 58 ). Also a torque pad ( 10, 70, 100, 120 ) and a method of connecting a backing plate to a torque tube.</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=20080821&amp;DB=EPODOC&amp;CC=US&amp;NR=2008196982A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25562,76317</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20080821&amp;DB=EPODOC&amp;CC=US&amp;NR=2008196982A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SARVER CHARLES F</creatorcontrib><creatorcontrib>CRESS JAMES J</creatorcontrib><title>Torque pads for aircraft brake systems and aircraft brake system including same</title><description>An aircraft brake system ( 42 ) includes a torque tube ( 44 ), a plurality of spaced stators ( 48 ) mounted on the torque tube ( 44 ), a wheel ( 40 ) surrounding the torque tube ( 44 ) and a plurality of rotors ( 50 ) connected to the wheel ( 40 ) and projecting into the spaces between adjacent ones of the stators ( 48 ). A backing plate ( 52 ) mounted on the torque tube ( 44 ) has a first side ( 54 ) facing the rotors ( 50 ) and a second side ( 56 ) facing away from the rotors ( 50 ), and the second side ( 56 ) includes a plurality of keyways ( 58 ). A plurality of torque pads ( 10, 70, 100, 120 ) are connected to the torque tube ( 44 ), each having a body ( 12, 72, 102, 122 ) with a first surface ( 14, 74, 104, 124 ) contacting the second side ( 56 ) of the backing plate ( 52 ) and at least one key ( 22, 82, 112, 114, 130, 132 ) projecting from the first surface ( 14, 74, 104, 124 ) into one of the plurality of keyways ( 58 ). 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A backing plate ( 52 ) mounted on the torque tube ( 44 ) has a first side ( 54 ) facing the rotors ( 50 ) and a second side ( 56 ) facing away from the rotors ( 50 ), and the second side ( 56 ) includes a plurality of keyways ( 58 ). A plurality of torque pads ( 10, 70, 100, 120 ) are connected to the torque tube ( 44 ), each having a body ( 12, 72, 102, 122 ) with a first surface ( 14, 74, 104, 124 ) contacting the second side ( 56 ) of the backing plate ( 52 ) and at least one key ( 22, 82, 112, 114, 130, 132 ) projecting from the first surface ( 14, 74, 104, 124 ) into one of the plurality of keyways ( 58 ). Also a torque pad ( 10, 70, 100, 120 ) and a method of connecting a backing plate to a torque tube.</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 Torque pads for aircraft brake systems and aircraft brake system including same
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