DYNAMIC RETENTION SYSTEM FOR AN AIRCRAFT SEAT
The dynamic retention system may include at least one plunger assembly including a plunger base coupled to a base assembly of an aircraft seat and a spring-loaded plunger coupled to a seat frame. The spring-loaded plunger may be configured to contact the plunger base. The dynamic retention system ma...
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| creator | OLESON, Michael L PEREZ, Moises SUAREZ, Alfredo |
| description | The dynamic retention system may include at least one plunger assembly including a plunger base coupled to a base assembly of an aircraft seat and a spring-loaded plunger coupled to a seat frame. The spring-loaded plunger may be configured to contact the plunger base. The dynamic retention system may include at least one hook receptacle coupled to the base assembly, and at least one structural hook coupled to the seat frame. The at least one hook receptacle may be configured to receive the at least one structural hook responsive to the spring-loaded plunger contacting the plunger base. The seat frame may be coupled to the base assembly via an actuation assembly. The aircraft seat may be actuatable between a first position and at least a second position. |
| format | Patent |
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The spring-loaded plunger may be configured to contact the plunger base. The dynamic retention system may include at least one hook receptacle coupled to the base assembly, and at least one structural hook coupled to the seat frame. The at least one hook receptacle may be configured to receive the at least one structural hook responsive to the spring-loaded plunger contacting the plunger base. The seat frame may be coupled to the base assembly via an actuation assembly. The aircraft seat may be actuatable between a first position and at least a second position.</description><language>eng ; fre ; ger</language><subject>AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; PARACHUTES ; PERFORMING OPERATIONS ; SEATS SPECIALLY ADAPTED FOR VEHICLES ; TRANSPORTING ; VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR ; VEHICLES IN GENERAL</subject><creationdate>2022</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=20221026&DB=EPODOC&CC=EP&NR=3626618B1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20221026&DB=EPODOC&CC=EP&NR=3626618B1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>OLESON, Michael L</creatorcontrib><creatorcontrib>PEREZ, Moises</creatorcontrib><creatorcontrib>SUAREZ, Alfredo</creatorcontrib><title>DYNAMIC RETENTION SYSTEM FOR AN AIRCRAFT SEAT</title><description>The dynamic retention system may include at least one plunger assembly including a plunger base coupled to a base assembly of an aircraft seat and a spring-loaded plunger coupled to a seat frame. The spring-loaded plunger may be configured to contact the plunger base. The dynamic retention system may include at least one hook receptacle coupled to the base assembly, and at least one structural hook coupled to the seat frame. The at least one hook receptacle may be configured to receive the at least one structural hook responsive to the spring-loaded plunger contacting the plunger base. The seat frame may be coupled to the base assembly via an actuation assembly. The aircraft seat may be actuatable between a first position and at least a second position.</description><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>SEATS SPECIALLY ADAPTED FOR VEHICLES</subject><subject>TRANSPORTING</subject><subject>VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR</subject><subject>VEHICLES IN GENERAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2022</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNB1ifRz9PV0VghyDXH1C_H091MIjgwOcfVVcPMPUnD0U3D0DHIOcnQLUQh2dQzhYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxrgHGZkZmZoYWTobGRCgBAHVpJQ8</recordid><startdate>20221026</startdate><enddate>20221026</enddate><creator>OLESON, Michael L</creator><creator>PEREZ, Moises</creator><creator>SUAREZ, Alfredo</creator><scope>EVB</scope></search><sort><creationdate>20221026</creationdate><title>DYNAMIC RETENTION SYSTEM FOR AN AIRCRAFT SEAT</title><author>OLESON, Michael L ; PEREZ, Moises ; SUAREZ, Alfredo</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP3626618B13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2022</creationdate><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>SEATS SPECIALLY ADAPTED FOR VEHICLES</topic><topic>TRANSPORTING</topic><topic>VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR</topic><topic>VEHICLES IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>OLESON, Michael L</creatorcontrib><creatorcontrib>PEREZ, Moises</creatorcontrib><creatorcontrib>SUAREZ, Alfredo</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>OLESON, Michael L</au><au>PEREZ, Moises</au><au>SUAREZ, Alfredo</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>DYNAMIC RETENTION SYSTEM FOR AN AIRCRAFT SEAT</title><date>2022-10-26</date><risdate>2022</risdate><abstract>The dynamic retention system may include at least one plunger assembly including a plunger base coupled to a base assembly of an aircraft seat and a spring-loaded plunger coupled to a seat frame. The spring-loaded plunger may be configured to contact the plunger base. The dynamic retention system may include at least one hook receptacle coupled to the base assembly, and at least one structural hook coupled to the seat frame. The at least one hook receptacle may be configured to receive the at least one structural hook responsive to the spring-loaded plunger contacting the plunger base. The seat frame may be coupled to the base assembly via an actuation assembly. The aircraft seat may be actuatable between a first position and at least a second position.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; fre ; ger |
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| subjects | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS SEATS SPECIALLY ADAPTED FOR VEHICLES TRANSPORTING VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR VEHICLES IN GENERAL |
| title | DYNAMIC RETENTION SYSTEM FOR AN AIRCRAFT SEAT |
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