Fusion type air refueling improved taper sleeve storage device and method
The invention belongs to the technical field of aircraft air refueling, and particularly relates to a fusion type air refueling improved taper sleeve storage device and method. An air refueling machine body connecting interface is arranged at one end of an air refueling hose; the aerial refueling ho...
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creator | JIANG BIAO LYU PENGFEI REN YUANCHUN |
description | The invention belongs to the technical field of aircraft air refueling, and particularly relates to a fusion type air refueling improved taper sleeve storage device and method. An air refueling machine body connecting interface is arranged at one end of an air refueling hose; the aerial refueling hose is sleeved with the machine body end butt joint connector, and the machine body end butt joint connector is located at the end, provided with the aerial refueling machine body connecting connector, of the aerial refueling hose. The air refueling hose is sleeved with the moving assembly. And the improved taper sleeve is sleeved on the aerial refueling hose. The pneumatic characteristic and the dynamic response characteristic of an existing soft air refueling system taper sleeve can be changed according to needs, the problem of collision between a plug-taper sleeve and an adjacent structure in the initial release stage and the recovery end stage is effectively solved, and the failure risk caused by impact of a ste |
format | Patent |
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An air refueling machine body connecting interface is arranged at one end of an air refueling hose; the aerial refueling hose is sleeved with the machine body end butt joint connector, and the machine body end butt joint connector is located at the end, provided with the aerial refueling machine body connecting connector, of the aerial refueling hose. The air refueling hose is sleeved with the moving assembly. And the improved taper sleeve is sleeved on the aerial refueling hose. The pneumatic characteristic and the dynamic response characteristic of an existing soft air refueling system taper sleeve can be changed according to needs, the problem of collision between a plug-taper sleeve and an adjacent structure in the initial release stage and the recovery end stage is effectively solved, and the failure risk caused by impact of a ste</description><language>chi ; eng</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 ; TRANSPORTING</subject><creationdate>2023</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=20230801&DB=EPODOC&CC=CN&NR=116513471A$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25563,76318</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20230801&DB=EPODOC&CC=CN&NR=116513471A$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>JIANG BIAO</creatorcontrib><creatorcontrib>LYU PENGFEI</creatorcontrib><creatorcontrib>REN YUANCHUN</creatorcontrib><title>Fusion type air refueling improved taper sleeve storage device and method</title><description>The invention belongs to the technical field of aircraft air refueling, and particularly relates to a fusion type air refueling improved taper sleeve storage device and method. 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The pneumatic characteristic and the dynamic response characteristic of an existing soft air refueling system taper sleeve can be changed according to needs, the problem of collision between a plug-taper sleeve and an adjacent structure in the initial release stage and the recovery end stage is effectively solved, and the failure risk caused by impact of a ste</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>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNqNyzsOwjAQRVE3FAjYw7AACit86igiCg0VfWTFL2Ekx7bsiaXsHgoWQHWbc7fq0S6ZgydZI8hwooRxgWM_Ec8xhQJLYiISZQcUUJaQzASyKDx8F29phryD3avNaFzG4dedOrb3V9OdEEOPHM0AD-mbp9bXi67ON11X_5gP8dY0vA</recordid><startdate>20230801</startdate><enddate>20230801</enddate><creator>JIANG BIAO</creator><creator>LYU PENGFEI</creator><creator>REN YUANCHUN</creator><scope>EVB</scope></search><sort><creationdate>20230801</creationdate><title>Fusion type air refueling improved taper sleeve storage device and method</title><author>JIANG BIAO ; LYU PENGFEI ; REN YUANCHUN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN116513471A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</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>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>JIANG BIAO</creatorcontrib><creatorcontrib>LYU PENGFEI</creatorcontrib><creatorcontrib>REN YUANCHUN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>JIANG BIAO</au><au>LYU PENGFEI</au><au>REN YUANCHUN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Fusion type air refueling improved taper sleeve storage device and method</title><date>2023-08-01</date><risdate>2023</risdate><abstract>The invention belongs to the technical field of aircraft air refueling, and particularly relates to a fusion type air refueling improved taper sleeve storage device and method. An air refueling machine body connecting interface is arranged at one end of an air refueling hose; the aerial refueling hose is sleeved with the machine body end butt joint connector, and the machine body end butt joint connector is located at the end, provided with the aerial refueling machine body connecting connector, of the aerial refueling hose. The air refueling hose is sleeved with the moving assembly. And the improved taper sleeve is sleeved on the aerial refueling hose. The pneumatic characteristic and the dynamic response characteristic of an existing soft air refueling system taper sleeve can be changed according to needs, the problem of collision between a plug-taper sleeve and an adjacent structure in the initial release stage and the recovery end stage is effectively solved, and the failure risk caused by impact of a ste</abstract><oa>free_for_read</oa></addata></record> |
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language | chi ; eng |
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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 TRANSPORTING |
title | Fusion type air refueling improved taper sleeve storage device and method |
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