JP2875578B
PURPOSE:To satisfactorily absorb the inertial force by relative speed and the relative position at the time of docking by providing a spring protruding and recessing driving means for protruding and recessing a coil spring provided on the top end part of a probe fitted to a probe insert part. CONSTI...
Gespeichert in:
Hauptverfasser: | , , , |
---|---|
Format: | Patent |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
container_end_page | |
---|---|
container_issue | |
container_start_page | |
container_title | |
container_volume | |
creator | AKYAMA MASAO MITSUMA HIDEHIKO NAMEKI TOORU ENDO EIICHI |
description | PURPOSE:To satisfactorily absorb the inertial force by relative speed and the relative position at the time of docking by providing a spring protruding and recessing driving means for protruding and recessing a coil spring provided on the top end part of a probe fitted to a probe insert part. CONSTITUTION:Docking ports 3, 4 are provided in the opposite parts of a space craft and a space station are airtightly closed by hutches 5, 6, and an expansion bonding device A and a holding device B are provided in the center of each hutch 5, 6. The expansion connecting device A is formed of a coil spring 9 freely inserted into a column 7 and a spring protruding and recessing driving means 10. The expansion connecting device A is provided with a probe 19 fitted to the top end part of the coil spring 9, which can be fitted to a funnel probe inserting part 37 in the holding device B. The driving motor of the spring protruding and recessing driving means 10 is operated, and this rotation is transmitted to a drive shaft 11 through a decelerator device 12, whereby the top end of the coil spring 9 can be advanced from the hutch 5 by the action of a spiral channel 11a. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_JP2875578BB2</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>JP2875578BB2</sourcerecordid><originalsourceid>FETCH-epo_espacenet_JP2875578BB23</originalsourceid><addsrcrecordid>eNrjZODyCjCyMDc1Nbdw4mFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8QgNTkbGxKgBAC31G5c</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>JP2875578B</title><source>esp@cenet</source><creator>AKYAMA MASAO ; MITSUMA HIDEHIKO ; NAMEKI TOORU ; ENDO EIICHI</creator><creatorcontrib>AKYAMA MASAO ; MITSUMA HIDEHIKO ; NAMEKI TOORU ; ENDO EIICHI</creatorcontrib><description>PURPOSE:To satisfactorily absorb the inertial force by relative speed and the relative position at the time of docking by providing a spring protruding and recessing driving means for protruding and recessing a coil spring provided on the top end part of a probe fitted to a probe insert part. CONSTITUTION:Docking ports 3, 4 are provided in the opposite parts of a space craft and a space station are airtightly closed by hutches 5, 6, and an expansion bonding device A and a holding device B are provided in the center of each hutch 5, 6. The expansion connecting device A is formed of a coil spring 9 freely inserted into a column 7 and a spring protruding and recessing driving means 10. The expansion connecting device A is provided with a probe 19 fitted to the top end part of the coil spring 9, which can be fitted to a funnel probe inserting part 37 in the holding device B. The driving motor of the spring protruding and recessing driving means 10 is operated, and this rotation is transmitted to a drive shaft 11 through a decelerator device 12, whereby the top end of the coil spring 9 can be advanced from the hutch 5 by the action of a spiral channel 11a.</description><edition>6</edition><language>eng</language><subject>AIRCRAFT ; AVIATION ; COSMONAUTICS ; PERFORMING OPERATIONS ; TRANSPORTING ; VEHICLES OR EQUIPMENT THEREFOR</subject><creationdate>1999</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=19990331&DB=EPODOC&CC=JP&NR=2875578B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19990331&DB=EPODOC&CC=JP&NR=2875578B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>AKYAMA MASAO</creatorcontrib><creatorcontrib>MITSUMA HIDEHIKO</creatorcontrib><creatorcontrib>NAMEKI TOORU</creatorcontrib><creatorcontrib>ENDO EIICHI</creatorcontrib><title>JP2875578B</title><description>PURPOSE:To satisfactorily absorb the inertial force by relative speed and the relative position at the time of docking by providing a spring protruding and recessing driving means for protruding and recessing a coil spring provided on the top end part of a probe fitted to a probe insert part. CONSTITUTION:Docking ports 3, 4 are provided in the opposite parts of a space craft and a space station are airtightly closed by hutches 5, 6, and an expansion bonding device A and a holding device B are provided in the center of each hutch 5, 6. The expansion connecting device A is formed of a coil spring 9 freely inserted into a column 7 and a spring protruding and recessing driving means 10. The expansion connecting device A is provided with a probe 19 fitted to the top end part of the coil spring 9, which can be fitted to a funnel probe inserting part 37 in the holding device B. The driving motor of the spring protruding and recessing driving means 10 is operated, and this rotation is transmitted to a drive shaft 11 through a decelerator device 12, whereby the top end of the coil spring 9 can be advanced from the hutch 5 by the action of a spiral channel 11a.</description><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>VEHICLES OR EQUIPMENT THEREFOR</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1999</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZODyCjCyMDc1Nbdw4mFgTUvMKU7lhdLcDIpuriHOHrqpBfnxqcUFicmpeakl8QgNTkbGxKgBAC31G5c</recordid><startdate>19990331</startdate><enddate>19990331</enddate><creator>AKYAMA MASAO</creator><creator>MITSUMA HIDEHIKO</creator><creator>NAMEKI TOORU</creator><creator>ENDO EIICHI</creator><scope>EVB</scope></search><sort><creationdate>19990331</creationdate><title>JP2875578B</title><author>AKYAMA MASAO ; MITSUMA HIDEHIKO ; NAMEKI TOORU ; ENDO EIICHI</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2875578BB23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>1999</creationdate><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>VEHICLES OR EQUIPMENT THEREFOR</topic><toplevel>online_resources</toplevel><creatorcontrib>AKYAMA MASAO</creatorcontrib><creatorcontrib>MITSUMA HIDEHIKO</creatorcontrib><creatorcontrib>NAMEKI TOORU</creatorcontrib><creatorcontrib>ENDO EIICHI</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>AKYAMA MASAO</au><au>MITSUMA HIDEHIKO</au><au>NAMEKI TOORU</au><au>ENDO EIICHI</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>JP2875578B</title><date>1999-03-31</date><risdate>1999</risdate><abstract>PURPOSE:To satisfactorily absorb the inertial force by relative speed and the relative position at the time of docking by providing a spring protruding and recessing driving means for protruding and recessing a coil spring provided on the top end part of a probe fitted to a probe insert part. CONSTITUTION:Docking ports 3, 4 are provided in the opposite parts of a space craft and a space station are airtightly closed by hutches 5, 6, and an expansion bonding device A and a holding device B are provided in the center of each hutch 5, 6. The expansion connecting device A is formed of a coil spring 9 freely inserted into a column 7 and a spring protruding and recessing driving means 10. The expansion connecting device A is provided with a probe 19 fitted to the top end part of the coil spring 9, which can be fitted to a funnel probe inserting part 37 in the holding device B. The driving motor of the spring protruding and recessing driving means 10 is operated, and this rotation is transmitted to a drive shaft 11 through a decelerator device 12, whereby the top end of the coil spring 9 can be advanced from the hutch 5 by the action of a spiral channel 11a.</abstract><edition>6</edition><oa>free_for_read</oa></addata></record> |
fulltext | fulltext_linktorsrc |
identifier | |
ispartof | |
issn | |
language | eng |
recordid | cdi_epo_espacenet_JP2875578BB2 |
source | esp@cenet |
subjects | AIRCRAFT AVIATION COSMONAUTICS PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR |
title | JP2875578B |
url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-01T17%3A26%3A59IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-epo_EVB&rft_val_fmt=info:ofi/fmt:kev:mtx:patent&rft.genre=patent&rft.au=AKYAMA%20MASAO&rft.date=1999-03-31&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EJP2875578BB2%3C/epo_EVB%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_id=info:pmid/&rfr_iscdi=true |