Light weight field howitzer
The light weight field howitzer includes a barrel (101) which is supported by a cradle constructed from hollow members (119,119A) and which is pivotally mounted about a trunnion bearing (113) secured to a chassis (117). The trunnion bearing (113) lies on the barrel axis and is positioned beyond the...
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creator | SEARLE, HAROLD LESLIE, BARROW-IN-FURNESS, CUMBRIA, GB BONE, JAMES, COLTON, CUMBRIA, GB EAGLESTONE, DAVID ANDREW, BARROW-IN-FURNESS, CUMBRIA, GB |
description | The light weight field howitzer includes a barrel (101) which is supported by a cradle constructed from hollow members (119,119A) and which is pivotally mounted about a trunnion bearing (113) secured to a chassis (117). The trunnion bearing (113) lies on the barrel axis and is positioned beyond the limit of maximum recoil of the barrel. Front stabilisers and rear trail support legs are provided to spread the load of the howitzer and spades (106) are rigidly but removably secured to the chassis. The howitzer includes a single hydraulic accumulator arrangement (136,177,185,130,189,119) constituting a combined recoil buffer and recuperator system. A barrel elevating device (Figure (7) not shown)is provided comprising a geared manual device (115,116,153,149,139) assisted by a precompressed gas system (114,119A). Hydraulically pivoted wheels and a pivotted towing lunette may be provided and the howitzer may be split easily into units which can be carried by a light helicopter. |
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fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_DE3943508A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>DE3943508A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_DE3943508A13</originalsourceid><addsrcrecordid>eNrjZJD2yUzPKFEoTwVTaZmpOSkKGfnlmSVVqUU8DKxpiTnFqbxQmptBwc01xNlDN7UgPz61uCAxOTUvtSTexdXY0sTY1MDC0dCYCCUALhoi8g</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Light weight field howitzer</title><source>esp@cenet</source><creator>SEARLE, HAROLD LESLIE, BARROW-IN-FURNESS, CUMBRIA, GB ; BONE, JAMES, COLTON, CUMBRIA, GB ; EAGLESTONE, DAVID ANDREW, BARROW-IN-FURNESS, CUMBRIA, GB</creator><creatorcontrib>SEARLE, HAROLD LESLIE, BARROW-IN-FURNESS, CUMBRIA, GB ; BONE, JAMES, COLTON, CUMBRIA, GB ; EAGLESTONE, DAVID ANDREW, BARROW-IN-FURNESS, CUMBRIA, GB</creatorcontrib><description>The light weight field howitzer includes a barrel (101) which is supported by a cradle constructed from hollow members (119,119A) and which is pivotally mounted about a trunnion bearing (113) secured to a chassis (117). The trunnion bearing (113) lies on the barrel axis and is positioned beyond the limit of maximum recoil of the barrel. Front stabilisers and rear trail support legs are provided to spread the load of the howitzer and spades (106) are rigidly but removably secured to the chassis. The howitzer includes a single hydraulic accumulator arrangement (136,177,185,130,189,119) constituting a combined recoil buffer and recuperator system. A barrel elevating device (Figure (7) not shown)is provided comprising a geared manual device (115,116,153,149,139) assisted by a precompressed gas system (114,119A). Hydraulically pivoted wheels and a pivotted towing lunette may be provided and the howitzer may be split easily into units which can be carried by a light helicopter.</description><edition>6</edition><language>eng ; ger</language><subject>BLASTING ; FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS ; HEATING ; LIGHTING ; MECHANICAL ENGINEERING ; MOUNTINGS FOR SMALLARMS OR ORDNANCE ; WEAPONS</subject><creationdate>1998</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=19980122&DB=EPODOC&CC=DE&NR=3943508A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=19980122&DB=EPODOC&CC=DE&NR=3943508A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SEARLE, HAROLD LESLIE, BARROW-IN-FURNESS, CUMBRIA, GB</creatorcontrib><creatorcontrib>BONE, JAMES, COLTON, CUMBRIA, GB</creatorcontrib><creatorcontrib>EAGLESTONE, DAVID ANDREW, BARROW-IN-FURNESS, CUMBRIA, GB</creatorcontrib><title>Light weight field howitzer</title><description>The light weight field howitzer includes a barrel (101) which is supported by a cradle constructed from hollow members (119,119A) and which is pivotally mounted about a trunnion bearing (113) secured to a chassis (117). The trunnion bearing (113) lies on the barrel axis and is positioned beyond the limit of maximum recoil of the barrel. Front stabilisers and rear trail support legs are provided to spread the load of the howitzer and spades (106) are rigidly but removably secured to the chassis. The howitzer includes a single hydraulic accumulator arrangement (136,177,185,130,189,119) constituting a combined recoil buffer and recuperator system. A barrel elevating device (Figure (7) not shown)is provided comprising a geared manual device (115,116,153,149,139) assisted by a precompressed gas system (114,119A). Hydraulically pivoted wheels and a pivotted towing lunette may be provided and the howitzer may be split easily into units which can be carried by a light helicopter.</description><subject>BLASTING</subject><subject>FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>MOUNTINGS FOR SMALLARMS OR ORDNANCE</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>1998</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJD2yUzPKFEoTwVTaZmpOSkKGfnlmSVVqUU8DKxpiTnFqbxQmptBwc01xNlDN7UgPz61uCAxOTUvtSTexdXY0sTY1MDC0dCYCCUALhoi8g</recordid><startdate>19980122</startdate><enddate>19980122</enddate><creator>SEARLE, HAROLD LESLIE, BARROW-IN-FURNESS, CUMBRIA, GB</creator><creator>BONE, JAMES, COLTON, CUMBRIA, GB</creator><creator>EAGLESTONE, DAVID ANDREW, BARROW-IN-FURNESS, CUMBRIA, GB</creator><scope>EVB</scope></search><sort><creationdate>19980122</creationdate><title>Light weight field howitzer</title><author>SEARLE, HAROLD LESLIE, BARROW-IN-FURNESS, CUMBRIA, GB ; BONE, JAMES, COLTON, CUMBRIA, GB ; EAGLESTONE, DAVID ANDREW, BARROW-IN-FURNESS, CUMBRIA, GB</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_DE3943508A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; ger</language><creationdate>1998</creationdate><topic>BLASTING</topic><topic>FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>MOUNTINGS FOR SMALLARMS OR ORDNANCE</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>SEARLE, HAROLD LESLIE, BARROW-IN-FURNESS, CUMBRIA, GB</creatorcontrib><creatorcontrib>BONE, JAMES, COLTON, CUMBRIA, GB</creatorcontrib><creatorcontrib>EAGLESTONE, DAVID ANDREW, BARROW-IN-FURNESS, CUMBRIA, GB</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SEARLE, HAROLD LESLIE, BARROW-IN-FURNESS, CUMBRIA, GB</au><au>BONE, JAMES, COLTON, CUMBRIA, GB</au><au>EAGLESTONE, DAVID ANDREW, BARROW-IN-FURNESS, CUMBRIA, GB</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Light weight field howitzer</title><date>1998-01-22</date><risdate>1998</risdate><abstract>The light weight field howitzer includes a barrel (101) which is supported by a cradle constructed from hollow members (119,119A) and which is pivotally mounted about a trunnion bearing (113) secured to a chassis (117). The trunnion bearing (113) lies on the barrel axis and is positioned beyond the limit of maximum recoil of the barrel. Front stabilisers and rear trail support legs are provided to spread the load of the howitzer and spades (106) are rigidly but removably secured to the chassis. The howitzer includes a single hydraulic accumulator arrangement (136,177,185,130,189,119) constituting a combined recoil buffer and recuperator system. A barrel elevating device (Figure (7) not shown)is provided comprising a geared manual device (115,116,153,149,139) assisted by a precompressed gas system (114,119A). Hydraulically pivoted wheels and a pivotted towing lunette may be provided and the howitzer may be split easily into units which can be carried by a light helicopter.</abstract><edition>6</edition><oa>free_for_read</oa></addata></record> |
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subjects | BLASTING FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS ANDORDNANCE, e.g. CANNONS HEATING LIGHTING MECHANICAL ENGINEERING MOUNTINGS FOR SMALLARMS OR ORDNANCE WEAPONS |
title | Light weight field howitzer |
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