A landing gear drive system clutch assembly

A landing gear drive system clutch assembly

A landing gear drive system clutch assembly and method of operation 300 comprising a drive gear 320, a driven transmission 350 with an intermediate gear 340 for receiving driving torque from the drive gear and transmitting driving torque to the driven transmission. The drive gear being engageable wi...

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1. Verfasser: Robert Ian Thompson
Format: Patent
Sprache:eng
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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creator Robert Ian Thompson
description A landing gear drive system clutch assembly and method of operation 300 comprising a drive gear 320, a driven transmission 350 with an intermediate gear 340 for receiving driving torque from the drive gear and transmitting driving torque to the driven transmission. The drive gear being engageable with the intermediate gear which is engageable with the driven transmission. There is also disclosed an aircraft landing gear comprising a strut with a lever arm (130, Fig 1b) and a drive system with a drive shaft (240, fig 1b) located within an axel and a drive shaft (230, fig 1b) located in the lever arm. There is further disclosed a drive system and method of operation comprising a drive shaft located in a landing gear axel, a clutch assembly comprising a drive gear and a driven transmission, wherein the drive gear is engageable with the driven transmission. There is further disclosed a landing gear drive clutch assembly and method of operation comprising a drive gear assembly and a driven transmission, the drive gear comprising two pinion gears 323, 324 mounted either side of a rotational axis of the driven transmission which can individually engage the driven transmission via movement of a lever.
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The drive gear being engageable with the intermediate gear which is engageable with the driven transmission. There is also disclosed an aircraft landing gear comprising a strut with a lever arm (130, Fig 1b) and a drive system with a drive shaft (240, fig 1b) located within an axel and a drive shaft (230, fig 1b) located in the lever arm. There is further disclosed a drive system and method of operation comprising a drive shaft located in a landing gear axel, a clutch assembly comprising a drive gear and a driven transmission, wherein the drive gear is engageable with the driven transmission. There is further disclosed a landing gear drive clutch assembly and method of operation comprising a drive gear assembly and a driven transmission, the drive gear comprising two pinion gears 323, 324 mounted either side of a rotational axis of the driven transmission which can individually engage the driven transmission via movement of a lever.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2023</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=20230118&amp;DB=EPODOC&amp;CC=GB&amp;NR=2585823B$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20230118&amp;DB=EPODOC&amp;CC=GB&amp;NR=2585823B$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Robert Ian Thompson</creatorcontrib><title>A landing gear drive system clutch assembly</title><description>A landing gear drive system clutch assembly and method of operation 300 comprising a drive gear 320, a driven transmission 350 with an intermediate gear 340 for receiving driving torque from the drive gear and transmitting driving torque to the driven transmission. The drive gear being engageable with the intermediate gear which is engageable with the driven transmission. There is also disclosed an aircraft landing gear comprising a strut with a lever arm (130, Fig 1b) and a drive system with a drive shaft (240, fig 1b) located within an axel and a drive shaft (230, fig 1b) located in the lever arm. There is further disclosed a drive system and method of operation comprising a drive shaft located in a landing gear axel, a clutch assembly comprising a drive gear and a driven transmission, wherein the drive gear is engageable with the driven transmission. There is further disclosed a landing gear drive clutch assembly and method of operation comprising a drive gear assembly and a driven transmission, the drive gear comprising two pinion gears 323, 324 mounted either side of a rotational axis of the driven transmission which can individually engage the driven transmission via movement of a lever.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNB2VMhJzEvJzEtXSE9NLFJIKcosS1UoriwuSc1VSM4pLUnOUEgsLk7NTcqp5GFgTUvMKU7lhdLcDPJuriHOHrqpBfnxqcUFicmpeakl8e5ORqYWphZGxk7GhFUAAKI1KGE</recordid><startdate>20230118</startdate><enddate>20230118</enddate><creator>Robert Ian Thompson</creator><scope>EVB</scope></search><sort><creationdate>20230118</creationdate><title>A landing gear drive system clutch assembly</title><author>Robert Ian Thompson</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_GB2585823B3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2023</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>Robert Ian Thompson</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Robert Ian Thompson</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>A landing gear drive system clutch assembly</title><date>2023-01-18</date><risdate>2023</risdate><abstract>A landing gear drive system clutch assembly and method of operation 300 comprising a drive gear 320, a driven transmission 350 with an intermediate gear 340 for receiving driving torque from the drive gear and transmitting driving torque to the driven transmission. The drive gear being engageable with the intermediate gear which is engageable with the driven transmission. There is also disclosed an aircraft landing gear comprising a strut with a lever arm (130, Fig 1b) and a drive system with a drive shaft (240, fig 1b) located within an axel and a drive shaft (230, fig 1b) located in the lever arm. There is further disclosed a drive system and method of operation comprising a drive shaft located in a landing gear axel, a clutch assembly comprising a drive gear and a driven transmission, wherein the drive gear is engageable with the driven transmission. There is further disclosed a landing gear drive clutch assembly and method of operation comprising a drive gear assembly and a driven transmission, the drive gear comprising two pinion gears 323, 324 mounted either side of a rotational axis of the driven transmission which can individually engage the driven transmission via movement of a lever.</abstract><oa>free_for_read</oa></addata></record>
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subjects AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
title A landing gear drive system clutch assembly
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