Lock for a turbofan engine thrust reverser

Lock for a turbofan engine thrust reverser

A cascade type thrust reverser for an air duct of a turbofan engine includes a lock mechanism mounted on a track beam (14L) that supports a translating sleeve. A locking portion (42L) of a lock pin (42) of the lock mechanism is engageable with a slideway (48) by which the translating sleeve is suppo...

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Hauptverfasser: LYMONS, DENNIS E, TERREY, COLIN R
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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creator LYMONS, DENNIS E
TERREY, COLIN R
description A cascade type thrust reverser for an air duct of a turbofan engine includes a lock mechanism mounted on a track beam (14L) that supports a translating sleeve. A locking portion (42L) of a lock pin (42) of the lock mechanism is engageable with a slideway (48) by which the translating sleeve is supported by the track beam to lock the translating sleeve in the forward, closed position. The lock pin is recieved adjacent and rearward of the rearward end of the sleeve.
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A locking portion (42L) of a lock pin (42) of the lock mechanism is engageable with a slideway (48) by which the translating sleeve is supported by the track beam to lock the translating sleeve in the forward, closed position. The lock pin is recieved adjacent and rearward of the rearward end of the sleeve.</description><edition>7</edition><language>eng ; fre ; ger</language><subject>BLASTING ; COMBUSTION ENGINES ; HEATING ; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS ; JET-PROPULSION PLANTS ; LIGHTING ; MECHANICAL ENGINEERING ; WEAPONS</subject><creationdate>2003</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=20030226&amp;DB=EPODOC&amp;CC=EP&amp;NR=1286037A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76290</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20030226&amp;DB=EPODOC&amp;CC=EP&amp;NR=1286037A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>LYMONS, DENNIS E</creatorcontrib><creatorcontrib>TERREY, COLIN R</creatorcontrib><title>Lock for a turbofan engine thrust reverser</title><description>A cascade type thrust reverser for an air duct of a turbofan engine includes a lock mechanism mounted on a track beam (14L) that supports a translating sleeve. 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A locking portion (42L) of a lock pin (42) of the lock mechanism is engageable with a slideway (48) by which the translating sleeve is supported by the track beam to lock the translating sleeve in the forward, closed position. The lock pin is recieved adjacent and rearward of the rearward end of the sleeve.</abstract><edition>7</edition><oa>free_for_read</oa></addata></record>
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subjects BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title Lock for a turbofan engine thrust reverser
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