SYSTEME DE FREINAGE POUR UN TRAIN D'ATTERRISSAGE D'AERONEF A ETRIER AVEC PLUSIEURS ZONE DE PINCEMENT DU DISQUE DE FREIN
La présente invention concerne un système de freinage (10) pour un train d'atterrissage d'un aéronef comportant plusieurs zones de pincement d'un disque de frein (40). Ledit système de freinage (10) comporte un actionneur (11), un étrier, une jante tournant autour d'un axe de rot...
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| creator | PRUD'HOMME LACROIX, PIERRE BISTUER, OLIVIER |
| description | La présente invention concerne un système de freinage (10) pour un train d'atterrissage d'un aéronef comportant plusieurs zones de pincement d'un disque de frein (40). Ledit système de freinage (10) comporte un actionneur (11), un étrier, une jante tournant autour d'un axe de rotation (AXROT1), et ledit disque de frein (40) monté flottant par rapport à ladite jante. Ledit étrier comporte un support interne (31) fixe, un support intermédiaire mobile et un support externe articulé par rapport audit support interne (31). Sous une action dudit actionneur (11), ledit support intermédiaire mobile se déplace et provoque un déplacement dudit disque de frein (40) afin que ledit disque de frein (40) soit pincé entre ledit support intermédiaire et ledit support externe, puis basculement dudit support externe afin que ledit disque de frein (40) soit pincé entre ledit support interne (31) et ledit support externe.
A braking system for aircraft landing gear including a plurality of clamping zones for clamping a brake disk. The braking system comprises an actuator, a caliper, a rim rotatable about an axis of rotation, and the brake disk, which is floatingly mounted relative to the rim. The caliper comprises a stationary inner support, a movable intermediate support, and an outer support that is hinged relative to the inner support. Under action of the actuator, the movable intermediate support moves and causes the brake disk to move so that the brake disk is clamped between the intermediate support and the outer support, and then causes the outer support to tilt so that the brake disk is damped between the inner support and the outer support. |
| format | Patent |
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A braking system for aircraft landing gear including a plurality of clamping zones for clamping a brake disk. The braking system comprises an actuator, a caliper, a rim rotatable about an axis of rotation, and the brake disk, which is floatingly mounted relative to the rim. The caliper comprises a stationary inner support, a movable intermediate support, and an outer support that is hinged relative to the inner support. Under action of the actuator, the movable intermediate support moves and causes the brake disk to move so that the brake disk is clamped between the intermediate support and the outer support, and then causes the outer support to tilt so that the brake disk is damped between the inner support and the outer support.</description><language>fre</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; BLASTING ; BRAKES ; CLUTCHES ; COSMONAUTICS ; COUPLINGS FOR TRANSMITTING ROTATION ; ENGINEERING ELEMENTS AND UNITS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; HELICOPTERS ; LIGHTING ; MECHANICAL ENGINEERING ; PERFORMING OPERATIONS ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; WEAPONS</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=20200529&DB=EPODOC&CC=FR&NR=3082256B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20200529&DB=EPODOC&CC=FR&NR=3082256B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>PRUD'HOMME LACROIX, PIERRE</creatorcontrib><creatorcontrib>BISTUER, OLIVIER</creatorcontrib><title>SYSTEME DE FREINAGE POUR UN TRAIN D'ATTERRISSAGE D'AERONEF A ETRIER AVEC PLUSIEURS ZONE DE PINCEMENT DU DISQUE DE FREIN</title><description>La présente invention concerne un système de freinage (10) pour un train d'atterrissage d'un aéronef comportant plusieurs zones de pincement d'un disque de frein (40). Ledit système de freinage (10) comporte un actionneur (11), un étrier, une jante tournant autour d'un axe de rotation (AXROT1), et ledit disque de frein (40) monté flottant par rapport à ladite jante. Ledit étrier comporte un support interne (31) fixe, un support intermédiaire mobile et un support externe articulé par rapport audit support interne (31). Sous une action dudit actionneur (11), ledit support intermédiaire mobile se déplace et provoque un déplacement dudit disque de frein (40) afin que ledit disque de frein (40) soit pincé entre ledit support intermédiaire et ledit support externe, puis basculement dudit support externe afin que ledit disque de frein (40) soit pincé entre ledit support interne (31) et ledit support externe.
A braking system for aircraft landing gear including a plurality of clamping zones for clamping a brake disk. The braking system comprises an actuator, a caliper, a rim rotatable about an axis of rotation, and the brake disk, which is floatingly mounted relative to the rim. The caliper comprises a stationary inner support, a movable intermediate support, and an outer support that is hinged relative to the inner support. Under action of the actuator, the movable intermediate support moves and causes the brake disk to move so that the brake disk is clamped between the intermediate support and the outer support, and then causes the outer support to tilt so that the brake disk is damped between the inner support and the outer support.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>BRAKES</subject><subject>CLUTCHES</subject><subject>COSMONAUTICS</subject><subject>COUPLINGS FOR TRANSMITTING ROTATION</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2020</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNjbEKwkAQRNNYiPoP21kJmqDYnrk9XdBL3N0TtAlBzko0EMHfNwHB1moY3vBmmLzlLIoHBIvgGMmbLUJZBIbgQdmQBzs1qshMIj3sKnLh0YEBVCZkMCfModwHIQwscOlo7yvJ553aK9gAluQYfjfjZHCr722cfHOUgEPNd7PYPKvYNvU1PuKrcpzN12m6XG0W2R-TD6ICOME</recordid><startdate>20200529</startdate><enddate>20200529</enddate><creator>PRUD'HOMME LACROIX, PIERRE</creator><creator>BISTUER, OLIVIER</creator><scope>EVB</scope></search><sort><creationdate>20200529</creationdate><title>SYSTEME DE FREINAGE POUR UN TRAIN D'ATTERRISSAGE D'AERONEF A ETRIER AVEC PLUSIEURS ZONE DE PINCEMENT DU DISQUE DE FREIN</title><author>PRUD'HOMME LACROIX, PIERRE ; BISTUER, OLIVIER</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_FR3082256B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>fre</language><creationdate>2020</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>BRAKES</topic><topic>CLUTCHES</topic><topic>COSMONAUTICS</topic><topic>COUPLINGS FOR TRANSMITTING ROTATION</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>PRUD'HOMME LACROIX, PIERRE</creatorcontrib><creatorcontrib>BISTUER, OLIVIER</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>PRUD'HOMME LACROIX, PIERRE</au><au>BISTUER, OLIVIER</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SYSTEME DE FREINAGE POUR UN TRAIN D'ATTERRISSAGE D'AERONEF A ETRIER AVEC PLUSIEURS ZONE DE PINCEMENT DU DISQUE DE FREIN</title><date>2020-05-29</date><risdate>2020</risdate><abstract>La présente invention concerne un système de freinage (10) pour un train d'atterrissage d'un aéronef comportant plusieurs zones de pincement d'un disque de frein (40). Ledit système de freinage (10) comporte un actionneur (11), un étrier, une jante tournant autour d'un axe de rotation (AXROT1), et ledit disque de frein (40) monté flottant par rapport à ladite jante. Ledit étrier comporte un support interne (31) fixe, un support intermédiaire mobile et un support externe articulé par rapport audit support interne (31). Sous une action dudit actionneur (11), ledit support intermédiaire mobile se déplace et provoque un déplacement dudit disque de frein (40) afin que ledit disque de frein (40) soit pincé entre ledit support intermédiaire et ledit support externe, puis basculement dudit support externe afin que ledit disque de frein (40) soit pincé entre ledit support interne (31) et ledit support externe.
A braking system for aircraft landing gear including a plurality of clamping zones for clamping a brake disk. The braking system comprises an actuator, a caliper, a rim rotatable about an axis of rotation, and the brake disk, which is floatingly mounted relative to the rim. The caliper comprises a stationary inner support, a movable intermediate support, and an outer support that is hinged relative to the inner support. Under action of the actuator, the movable intermediate support moves and causes the brake disk to move so that the brake disk is clamped between the intermediate support and the outer support, and then causes the outer support to tilt so that the brake disk is damped between the inner support and the outer support.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT AVIATION BLASTING BRAKES CLUTCHES COSMONAUTICS COUPLINGS FOR TRANSMITTING ROTATION ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS |
| title | SYSTEME DE FREINAGE POUR UN TRAIN D'ATTERRISSAGE D'AERONEF A ETRIER AVEC PLUSIEURS ZONE DE PINCEMENT DU DISQUE DE FREIN |
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