SYSTEM, METHOD, AND TOOL ASSEMBLY FOR REMOVING COMPONENT FROM MANDREL ASSEMBLY
PROBLEM TO BE SOLVED: To provide a method of quickly, efficiently, and safely removing a component from a mandrel assembly.SOLUTION: A component-removal tool assembly is configured to remove a component from a mandrel assembly, and may include a main frame, and a plurality of rotational input device...
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Patent |
| Sprache: | eng ; jpn |
| 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 | JOHN YESTRAU |
| description | PROBLEM TO BE SOLVED: To provide a method of quickly, efficiently, and safely removing a component from a mandrel assembly.SOLUTION: A component-removal tool assembly is configured to remove a component from a mandrel assembly, and may include a main frame, and a plurality of rotational input devices extending from the main frame. Each rotational input device may be operatively coupled to a respective plunger that is configured to be actuated against a portion of the mandrel assembly. A synchronizing link synchronously couples the rotational input devices together. The synchronizing link operates to synchronize movement of the plurality of rotational input devices. Movement of one or more of the rotational input devices causes the plungers coupled thereto to exert a uniform and consistent disconnecting force against the mandrel assembly.SELECTED DRAWING: None
【課題】マンドレルアセンブリから構成要素を素早く、効率的に、且つ、安全に取り外す方法の提供。【解決手段】構成要素取り外しツールアセンブリは、マンドレルアセンブリから構成要素を取り外すように構成され、主要フレーム、及び主要フレームから延在する複数の回転入力装置を含み得る。各回転入力装置は、マンドレルアセンブリの一部分に対抗して駆動されるように構成された、それぞれのプランジャーと動作可能に連結され得る。同期リンクが、回転入力装置を共に同期させるように連結する。同期リンクは、複数の回転入力装置の動きを同期させるように動作する。回転入力装置のうちの１以上の動きは、それらと連結されたプランジャーが、マンドレルアセンブリに対して均一な調和した連結解除力を加えることをもたらす。【選択図】なし |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_JP2017185783A</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>JP2017185783A</sourcerecordid><originalsourceid>FETCH-epo_espacenet_JP2017185783A3</originalsourceid><addsrcrecordid>eNrjZPALjgwOcfXVUfB1DfHwd9FRcPRzUQjx9_dRcAwOdvV18olUcPMPUghy9fUP8_RzV3D29w3w93P1C1FwC_L3VfAFKg9yRSjmYWBNS8wpTuWF0twMSm6uIc4euqkF-fGpxQWJyal5qSXxXgFGBobmhham5hbGjsZEKQIAbY0vBA</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>SYSTEM, METHOD, AND TOOL ASSEMBLY FOR REMOVING COMPONENT FROM MANDREL ASSEMBLY</title><source>esp@cenet</source><creator>JOHN YESTRAU</creator><creatorcontrib>JOHN YESTRAU</creatorcontrib><description>PROBLEM TO BE SOLVED: To provide a method of quickly, efficiently, and safely removing a component from a mandrel assembly.SOLUTION: A component-removal tool assembly is configured to remove a component from a mandrel assembly, and may include a main frame, and a plurality of rotational input devices extending from the main frame. Each rotational input device may be operatively coupled to a respective plunger that is configured to be actuated against a portion of the mandrel assembly. A synchronizing link synchronously couples the rotational input devices together. The synchronizing link operates to synchronize movement of the plurality of rotational input devices. Movement of one or more of the rotational input devices causes the plungers coupled thereto to exert a uniform and consistent disconnecting force against the mandrel assembly.SELECTED DRAWING: None
【課題】マンドレルアセンブリから構成要素を素早く、効率的に、且つ、安全に取り外す方法の提供。【解決手段】構成要素取り外しツールアセンブリは、マンドレルアセンブリから構成要素を取り外すように構成され、主要フレーム、及び主要フレームから延在する複数の回転入力装置を含み得る。各回転入力装置は、マンドレルアセンブリの一部分に対抗して駆動されるように構成された、それぞれのプランジャーと動作可能に連結され得る。同期リンクが、回転入力装置を共に同期させるように連結する。同期リンクは、複数の回転入力装置の動きを同期させるように動作する。回転入力装置のうちの１以上の動きは、それらと連結されたプランジャーが、マンドレルアセンブリに対して均一な調和した連結解除力を加えることをもたらす。【選択図】なし</description><language>eng ; jpn</language><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING ; AIRCRAFT ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; PARACHUTES ; PERFORMING OPERATIONS ; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR ; SHAPING OR JOINING OF PLASTICS ; TRANSPORTING ; WORKING OF PLASTICS ; WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><creationdate>2017</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=20171012&DB=EPODOC&CC=JP&NR=2017185783A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76289</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20171012&DB=EPODOC&CC=JP&NR=2017185783A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>JOHN YESTRAU</creatorcontrib><title>SYSTEM, METHOD, AND TOOL ASSEMBLY FOR REMOVING COMPONENT FROM MANDREL ASSEMBLY</title><description>PROBLEM TO BE SOLVED: To provide a method of quickly, efficiently, and safely removing a component from a mandrel assembly.SOLUTION: A component-removal tool assembly is configured to remove a component from a mandrel assembly, and may include a main frame, and a plurality of rotational input devices extending from the main frame. Each rotational input device may be operatively coupled to a respective plunger that is configured to be actuated against a portion of the mandrel assembly. A synchronizing link synchronously couples the rotational input devices together. The synchronizing link operates to synchronize movement of the plurality of rotational input devices. Movement of one or more of the rotational input devices causes the plungers coupled thereto to exert a uniform and consistent disconnecting force against the mandrel assembly.SELECTED DRAWING: None
【課題】マンドレルアセンブリから構成要素を素早く、効率的に、且つ、安全に取り外す方法の提供。【解決手段】構成要素取り外しツールアセンブリは、マンドレルアセンブリから構成要素を取り外すように構成され、主要フレーム、及び主要フレームから延在する複数の回転入力装置を含み得る。各回転入力装置は、マンドレルアセンブリの一部分に対抗して駆動されるように構成された、それぞれのプランジャーと動作可能に連結され得る。同期リンクが、回転入力装置を共に同期させるように連結する。同期リンクは、複数の回転入力装置の動きを同期させるように動作する。回転入力装置のうちの１以上の動きは、それらと連結されたプランジャーが、マンドレルアセンブリに対して均一な調和した連結解除力を加えることをもたらす。【選択図】なし</description><subject>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</subject><subject>AIRCRAFT</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</subject><subject>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</subject><subject>SHAPING OR JOINING OF PLASTICS</subject><subject>TRANSPORTING</subject><subject>WORKING OF PLASTICS</subject><subject>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2017</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZPALjgwOcfXVUfB1DfHwd9FRcPRzUQjx9_dRcAwOdvV18olUcPMPUghy9fUP8_RzV3D29w3w93P1C1FwC_L3VfAFKg9yRSjmYWBNS8wpTuWF0twMSm6uIc4euqkF-fGpxQWJyal5qSXxXgFGBobmhham5hbGjsZEKQIAbY0vBA</recordid><startdate>20171012</startdate><enddate>20171012</enddate><creator>JOHN YESTRAU</creator><scope>EVB</scope></search><sort><creationdate>20171012</creationdate><title>SYSTEM, METHOD, AND TOOL ASSEMBLY FOR REMOVING COMPONENT FROM MANDREL ASSEMBLY</title><author>JOHN YESTRAU</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_JP2017185783A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; jpn</language><creationdate>2017</creationdate><topic>AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT</topic><topic>HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR</topic><topic>SHAPING OR JOINING OF PLASTICS</topic><topic>TRANSPORTING</topic><topic>WORKING OF PLASTICS</topic><topic>WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL</topic><toplevel>online_resources</toplevel><creatorcontrib>JOHN YESTRAU</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>JOHN YESTRAU</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>SYSTEM, METHOD, AND TOOL ASSEMBLY FOR REMOVING COMPONENT FROM MANDREL ASSEMBLY</title><date>2017-10-12</date><risdate>2017</risdate><abstract>PROBLEM TO BE SOLVED: To provide a method of quickly, efficiently, and safely removing a component from a mandrel assembly.SOLUTION: A component-removal tool assembly is configured to remove a component from a mandrel assembly, and may include a main frame, and a plurality of rotational input devices extending from the main frame. Each rotational input device may be operatively coupled to a respective plunger that is configured to be actuated against a portion of the mandrel assembly. A synchronizing link synchronously couples the rotational input devices together. The synchronizing link operates to synchronize movement of the plurality of rotational input devices. Movement of one or more of the rotational input devices causes the plungers coupled thereto to exert a uniform and consistent disconnecting force against the mandrel assembly.SELECTED DRAWING: None
【課題】マンドレルアセンブリから構成要素を素早く、効率的に、且つ、安全に取り外す方法の提供。【解決手段】構成要素取り外しツールアセンブリは、マンドレルアセンブリから構成要素を取り外すように構成され、主要フレーム、及び主要フレームから延在する複数の回転入力装置を含み得る。各回転入力装置は、マンドレルアセンブリの一部分に対抗して駆動されるように構成された、それぞれのプランジャーと動作可能に連結され得る。同期リンクが、回転入力装置を共に同期させるように連結する。同期リンクは、複数の回転入力装置の動きを同期させるように動作する。回転入力装置のうちの１以上の動きは、それらと連結されたプランジャーが、マンドレルアセンブリに対して均一な調和した連結解除力を加えることをもたらす。【選択図】なし</abstract><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | eng ; jpn |
| recordid | cdi_epo_espacenet_JP2017185783A |
| source | esp@cenet |
| subjects | AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL |
| title | SYSTEM, METHOD, AND TOOL ASSEMBLY FOR REMOVING COMPONENT FROM MANDREL ASSEMBLY |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-10T15%3A54%3A54IST&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=JOHN%20YESTRAU&rft.date=2017-10-12&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EJP2017185783A%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 |