SEPARATION SYSTEM FOR MISSILE PAYLOAD FAIRINGS

SEPARATION SYSTEM FOR MISSILE PAYLOAD FAIRINGS

In detail, the system includes at least one first pulley (34A, B, C, D) mounted on the first structural member (20) and at least one-second pulley (36, A, B, C, D), mounted on the second structural member (22). A cable (40) is attached by one end (42) to the first structural member (22) and wound ab...

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1. Verfasser: NYGREN, WILLIAM, D
Format: Patent
Sprache:eng ; fre
Schlagworte:
AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
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description In detail, the system includes at least one first pulley (34A, B, C, D) mounted on the first structural member (20) and at least one-second pulley (36, A, B, C, D), mounted on the second structural member (22). A cable (40) is attached by one end (42) to the first structural member (22) and wound about the first and second pulleys and is attached by its second end (46) to the second structural member (22). Preferably there are two or more first and second pulleys with the cable alternately wound between said first and second pulleys with one end of cable attached to the first structural member and the opposite end attached to the second structural member. Thus the cable (40) holds the first and second structural members (20, 22) together. A system (52) to sever the cable (40) is included, which upon actuation will sever the cable allowing the two structural members (20, 22) to separate. L'invention concerne un système comprenant au moins une première poulie (34A, B, C, D) montée sur le premier élément de structure (20) et au moins une seconde poulie (36, A, B, C, D) montée sur un second élément de structure (22). Un câble (40) est relié par une extrémité (42) au premier élément de structure (22) et il est enroulé autour des premières et des secondes poulies; il est relié par sa seconde extrémité (46) au second élément de structure (22). De préférence, le système comprend plus de deux premières et secondes poulies, le câble susmentionné étant enroulé alternativement entre ces premières et secondes poulies, l'une des extrémité du câble est reliée au premier élément de structure et l'autre extrémité est reliée au second élément de structure. De cette manière, le câble (40) maintient ensemble les premier et second éléments de structure (20, 22). Le système décrit dans cette invention comprend également un dispositif (52) servant à disjoindre le câble (40); ce dispositif permet, lorsqu'il est actionné, de disjoindre le câble, ce qui permet de déclencher la séparation des deux éléments de structure (20, 22).
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A cable (40) is attached by one end (42) to the first structural member (22) and wound about the first and second pulleys and is attached by its second end (46) to the second structural member (22). Preferably there are two or more first and second pulleys with the cable alternately wound between said first and second pulleys with one end of cable attached to the first structural member and the opposite end attached to the second structural member. Thus the cable (40) holds the first and second structural members (20, 22) together. A system (52) to sever the cable (40) is included, which upon actuation will sever the cable allowing the two structural members (20, 22) to separate. L'invention concerne un système comprenant au moins une première poulie (34A, B, C, D) montée sur le premier élément de structure (20) et au moins une seconde poulie (36, A, B, C, D) montée sur un second élément de structure (22). 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Le système décrit dans cette invention comprend également un dispositif (52) servant à disjoindre le câble (40); ce dispositif permet, lorsqu'il est actionné, de disjoindre le câble, ce qui permet de déclencher la séparation des deux éléments de structure (20, 22).</description><edition>7</edition><language>eng ; fre</language><subject>AIRCRAFT ; AVIATION ; COSMONAUTICS ; PERFORMING OPERATIONS ; TRANSPORTING ; VEHICLES OR EQUIPMENT THEREFOR</subject><creationdate>2001</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=20010802&amp;DB=EPODOC&amp;CC=WO&amp;NR=0155663A2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76293</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&amp;date=20010802&amp;DB=EPODOC&amp;CC=WO&amp;NR=0155663A2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>NYGREN, WILLIAM, D</creatorcontrib><title>SEPARATION SYSTEM FOR MISSILE PAYLOAD FAIRINGS</title><description>In detail, the system includes at least one first pulley (34A, B, C, D) mounted on the first structural member (20) and at least one-second pulley (36, A, B, C, D), mounted on the second structural member (22). 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Un câble (40) est relié par une extrémité (42) au premier élément de structure (22) et il est enroulé autour des premières et des secondes poulies; il est relié par sa seconde extrémité (46) au second élément de structure (22). De préférence, le système comprend plus de deux premières et secondes poulies, le câble susmentionné étant enroulé alternativement entre ces premières et secondes poulies, l'une des extrémité du câble est reliée au premier élément de structure et l'autre extrémité est reliée au second élément de structure. De cette manière, le câble (40) maintient ensemble les premier et second éléments de structure (20, 22). 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A cable (40) is attached by one end (42) to the first structural member (22) and wound about the first and second pulleys and is attached by its second end (46) to the second structural member (22). Preferably there are two or more first and second pulleys with the cable alternately wound between said first and second pulleys with one end of cable attached to the first structural member and the opposite end attached to the second structural member. Thus the cable (40) holds the first and second structural members (20, 22) together. A system (52) to sever the cable (40) is included, which upon actuation will sever the cable allowing the two structural members (20, 22) to separate. L'invention concerne un système comprenant au moins une première poulie (34A, B, C, D) montée sur le premier élément de structure (20) et au moins une seconde poulie (36, A, B, C, D) montée sur un second élément de structure (22). Un câble (40) est relié par une extrémité (42) au premier élément de structure (22) et il est enroulé autour des premières et des secondes poulies; il est relié par sa seconde extrémité (46) au second élément de structure (22). De préférence, le système comprend plus de deux premières et secondes poulies, le câble susmentionné étant enroulé alternativement entre ces premières et secondes poulies, l'une des extrémité du câble est reliée au premier élément de structure et l'autre extrémité est reliée au second élément de structure. De cette manière, le câble (40) maintient ensemble les premier et second éléments de structure (20, 22). Le système décrit dans cette invention comprend également un dispositif (52) servant à disjoindre le câble (40); ce dispositif permet, lorsqu'il est actionné, de disjoindre le câble, ce qui permet de déclencher la séparation des deux éléments de structure (20, 22).</abstract><edition>7</edition><oa>free_for_read</oa></addata></record>
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subjects AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
title SEPARATION SYSTEM FOR MISSILE PAYLOAD FAIRINGS
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