HUBSCHRAUBER
A helicopter includes missile supporting means movable from an operational position to a stowed position in which the missiles 17 are located within the confines of the helicopter fuselage. In one embodiment the missile supporting means is pivotally attached to the fuselage about a generally horizon...
Gespeichert in:
| Hauptverfasser: | , , |
|---|---|
| Format: | Patent |
| Sprache: | ger |
| 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 | ERNEST NORTH,HORACE LEWIS COWDERY,ROY VINCENT SMITH,RONALD |
| description | A helicopter includes missile supporting means movable from an operational position to a stowed position in which the missiles 17 are located within the confines of the helicopter fuselage. In one embodiment the missile supporting means is pivotally attached to the fuselage about a generally horizontal longitudinally extending hinge for movement through an opening in the fuselage between the operational and stowed positions. A closure member 16 is provided to automatically close the opening when the missile supporting means is in the closed position and conveniently the missile supporting means may be integral with the closure member. |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_DE3532220A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>DE3532220A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_DE3532220A13</originalsourceid><addsrcrecordid>eNrjZODxCHUKdvYIcgx1cg3iYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxLq7GpsZGRkYGjobGRCgBAFy3G-M</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>HUBSCHRAUBER</title><source>esp@cenet</source><creator>ERNEST NORTH,HORACE ; LEWIS COWDERY,ROY ; VINCENT SMITH,RONALD</creator><creatorcontrib>ERNEST NORTH,HORACE ; LEWIS COWDERY,ROY ; VINCENT SMITH,RONALD</creatorcontrib><description>A helicopter includes missile supporting means movable from an operational position to a stowed position in which the missiles 17 are located within the confines of the helicopter fuselage. In one embodiment the missile supporting means is pivotally attached to the fuselage about a generally horizontal longitudinally extending hinge for movement through an opening in the fuselage between the operational and stowed positions. A closure member 16 is provided to automatically close the opening when the missile supporting means is in the closed position and conveniently the missile supporting means may be integral with the closure member.</description><edition>4</edition><language>ger</language><subject>AEROPLANES ; AIRCRAFT ; APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FLYING SUITS ; FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS ; HARPOON GUNS ; HEATING ; HELICOPTERS ; LAUNCHERS FOR ROCKETS OR TORPEDOES ; LIGHTING ; MECHANICAL ENGINEERING ; MOUNTINGS FOR SMALLARMS OR ORDNANCE ; PARACHUTES ; PERFORMING OPERATIONS ; TRANSPORTING ; WEAPONS</subject><creationdate>1987</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=19870514&DB=EPODOC&CC=DE&NR=3532220A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19870514&DB=EPODOC&CC=DE&NR=3532220A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>ERNEST NORTH,HORACE</creatorcontrib><creatorcontrib>LEWIS COWDERY,ROY</creatorcontrib><creatorcontrib>VINCENT SMITH,RONALD</creatorcontrib><title>HUBSCHRAUBER</title><description>A helicopter includes missile supporting means movable from an operational position to a stowed position in which the missiles 17 are located within the confines of the helicopter fuselage. In one embodiment the missile supporting means is pivotally attached to the fuselage about a generally horizontal longitudinally extending hinge for movement through an opening in the fuselage between the operational and stowed positions. A closure member 16 is provided to automatically close the opening when the missile supporting means is in the closed position and conveniently the missile supporting means may be integral with the closure member.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FLYING SUITS</subject><subject>FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS</subject><subject>HARPOON GUNS</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>LAUNCHERS FOR ROCKETS OR TORPEDOES</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>MOUNTINGS FOR SMALLARMS OR ORDNANCE</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1987</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZODxCHUKdvYIcgx1cg3iYWBNS8wpTuWF0twMCm6uIc4euqkF-fGpxQWJyal5qSXxLq7GpsZGRkYGjobGRCgBAFy3G-M</recordid><startdate>19870514</startdate><enddate>19870514</enddate><creator>ERNEST NORTH,HORACE</creator><creator>LEWIS COWDERY,ROY</creator><creator>VINCENT SMITH,RONALD</creator><scope>EVB</scope></search><sort><creationdate>19870514</creationdate><title>HUBSCHRAUBER</title><author>ERNEST NORTH,HORACE ; LEWIS COWDERY,ROY ; VINCENT SMITH,RONALD</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE3532220A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>ger</language><creationdate>1987</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</topic><topic>FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS</topic><topic>HARPOON GUNS</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>LAUNCHERS FOR ROCKETS OR TORPEDOES</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>MOUNTINGS FOR SMALLARMS OR ORDNANCE</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>ERNEST NORTH,HORACE</creatorcontrib><creatorcontrib>LEWIS COWDERY,ROY</creatorcontrib><creatorcontrib>VINCENT SMITH,RONALD</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>ERNEST NORTH,HORACE</au><au>LEWIS COWDERY,ROY</au><au>VINCENT SMITH,RONALD</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>HUBSCHRAUBER</title><date>1987-05-14</date><risdate>1987</risdate><abstract>A helicopter includes missile supporting means movable from an operational position to a stowed position in which the missiles 17 are located within the confines of the helicopter fuselage. In one embodiment the missile supporting means is pivotally attached to the fuselage about a generally horizontal longitudinally extending hinge for movement through an opening in the fuselage between the operational and stowed positions. A closure member 16 is provided to automatically close the opening when the missile supporting means is in the closed position and conveniently the missile supporting means may be integral with the closure member.</abstract><edition>4</edition><oa>free_for_read</oa></addata></record> |
| fulltext | fulltext_linktorsrc |
| identifier | |
| ispartof | |
| issn | |
| language | ger |
| recordid | cdi_epo_espacenet_DE3532220A1 |
| source | esp@cenet |
| subjects | AEROPLANES AIRCRAFT APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS,e.g. CANNONS ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS HARPOON GUNS HEATING HELICOPTERS LAUNCHERS FOR ROCKETS OR TORPEDOES LIGHTING MECHANICAL ENGINEERING MOUNTINGS FOR SMALLARMS OR ORDNANCE PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS |
| title | HUBSCHRAUBER |
| url | https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-02T01%3A29%3A44IST&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=ERNEST%20NORTH,HORACE&rft.date=1987-05-14&rft_id=info:doi/&rft_dat=%3Cepo_EVB%3EDE3532220A1%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 |