Helicopter skid landing gear
A cross tube for a helicopter skid landing gear, including a monolithic metallic tube having a central portion (28) extending transversely between two end portions (30) with longitudinal central axes (A C , A E ) of the central portion (28) and of the end portions (30) being located in a plane (P),...
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creator | GUILLOT, MICHEL LEVESQUE, JULIE AQUINO, GIUSEPPE FEWS, ROBERT CLIVE GAKWAYA, AUGUSTIN BERNIER, SIMON ELIE-DIT-COSAQUE, XAVIER JEAN-GILLES BLANCHET, JOCELYN |
description | A cross tube for a helicopter skid landing gear, including a monolithic metallic tube having a central portion (28) extending transversely between two end portions (30) with longitudinal central axes (A C , A E ) of the central portion (28) and of the end portions (30) being located in a plane (P), where the central portion (28) has inner and outer heights (H ci , H co ), the end portions (30) each have inner and outer heights (H ei , H eo ), and the inner and outer heights of one of the central portion (28) and the end portion (30) are respectively greater than the inner and outer heights of the other of the central portion (28) and the end portion (30). A skid tube (22) with two portions (22b, 22d, 22a, 22c) with cross-sections having one or both of different orientations with respect to one another and different dimensions with respect to one another, and a method of forming a structural tube (22, 24, 26) for a helicopter skid landing gear (20) are also provided. |
format | Patent |
fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_EP2746155A1</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>EP2746155A1</sourcerecordid><originalsourceid>FETCH-epo_espacenet_EP2746155A13</originalsourceid><addsrcrecordid>eNrjZJDxSM3JTM4vKEktUijOzkxRyEnMS8nMS1dIT00s4mFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BRuYmZoampo6GxkQoAQBQfSM9</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Helicopter skid landing gear</title><source>esp@cenet</source><creator>GUILLOT, MICHEL ; LEVESQUE, JULIE ; AQUINO, GIUSEPPE ; FEWS, ROBERT CLIVE ; GAKWAYA, AUGUSTIN ; BERNIER, SIMON ; ELIE-DIT-COSAQUE, XAVIER JEAN-GILLES ; BLANCHET, JOCELYN</creator><creatorcontrib>GUILLOT, MICHEL ; LEVESQUE, JULIE ; AQUINO, GIUSEPPE ; FEWS, ROBERT CLIVE ; GAKWAYA, AUGUSTIN ; BERNIER, SIMON ; ELIE-DIT-COSAQUE, XAVIER JEAN-GILLES ; BLANCHET, JOCELYN</creatorcontrib><description>A cross tube for a helicopter skid landing gear, including a monolithic metallic tube having a central portion (28) extending transversely between two end portions (30) with longitudinal central axes (A C , A E ) of the central portion (28) and of the end portions (30) being located in a plane (P), where the central portion (28) has inner and outer heights (H ci , H co ), the end portions (30) each have inner and outer heights (H ei , H eo ), and the inner and outer heights of one of the central portion (28) and the end portion (30) are respectively greater than the inner and outer heights of the other of the central portion (28) and the end portion (30). A skid tube (22) with two portions (22b, 22d, 22a, 22c) with cross-sections having one or both of different orientations with respect to one another and different dimensions with respect to one another, and a method of forming a structural tube (22, 24, 26) for a helicopter skid landing gear (20) are also provided.</description><language>eng ; fre ; ger</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; BLASTING ; COSMONAUTICS ; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ; DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION ; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC ; GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS ; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT ; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR ; HEAT EXCHANGE IN GENERAL ; HEATING ; HELICOPTERS ; LIGHTING ; MECHANICAL ENGINEERING ; MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL ; PERFORMING OPERATIONS ; PUNCHING METAL ; TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION ; TECHNICAL SUBJECTS COVERED BY FORMER USPC ; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS ; TRANSPORTING ; WEAPONS ; WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS ORPROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL</subject><creationdate>2014</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=20140625&DB=EPODOC&CC=EP&NR=2746155A1$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,780,885,25564,76547</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20140625&DB=EPODOC&CC=EP&NR=2746155A1$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>GUILLOT, MICHEL</creatorcontrib><creatorcontrib>LEVESQUE, JULIE</creatorcontrib><creatorcontrib>AQUINO, GIUSEPPE</creatorcontrib><creatorcontrib>FEWS, ROBERT CLIVE</creatorcontrib><creatorcontrib>GAKWAYA, AUGUSTIN</creatorcontrib><creatorcontrib>BERNIER, SIMON</creatorcontrib><creatorcontrib>ELIE-DIT-COSAQUE, XAVIER JEAN-GILLES</creatorcontrib><creatorcontrib>BLANCHET, JOCELYN</creatorcontrib><title>Helicopter skid landing gear</title><description>A cross tube for a helicopter skid landing gear, including a monolithic metallic tube having a central portion (28) extending transversely between two end portions (30) with longitudinal central axes (A C , A E ) of the central portion (28) and of the end portions (30) being located in a plane (P), where the central portion (28) has inner and outer heights (H ci , H co ), the end portions (30) each have inner and outer heights (H ei , H eo ), and the inner and outer heights of one of the central portion (28) and the end portion (30) are respectively greater than the inner and outer heights of the other of the central portion (28) and the end portion (30). A skid tube (22) with two portions (22b, 22d, 22a, 22c) with cross-sections having one or both of different orientations with respect to one another and different dimensions with respect to one another, and a method of forming a structural tube (22, 24, 26) for a helicopter skid landing gear (20) are also provided.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</subject><subject>DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION</subject><subject>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</subject><subject>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</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>HEAT EXCHANGE IN GENERAL</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL</subject><subject>PERFORMING OPERATIONS</subject><subject>PUNCHING METAL</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER USPC</subject><subject>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</subject><subject>TRANSPORTING</subject><subject>WEAPONS</subject><subject>WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS ORPROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2014</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZJDxSM3JTM4vKEktUijOzkxRyEnMS8nMS1dIT00s4mFgTUvMKU7lhdLcDApuriHOHrqpBfnxqcUFicmpeakl8a4BRuYmZoampo6GxkQoAQBQfSM9</recordid><startdate>20140625</startdate><enddate>20140625</enddate><creator>GUILLOT, MICHEL</creator><creator>LEVESQUE, JULIE</creator><creator>AQUINO, GIUSEPPE</creator><creator>FEWS, ROBERT CLIVE</creator><creator>GAKWAYA, AUGUSTIN</creator><creator>BERNIER, SIMON</creator><creator>ELIE-DIT-COSAQUE, XAVIER JEAN-GILLES</creator><creator>BLANCHET, JOCELYN</creator><scope>EVB</scope></search><sort><creationdate>20140625</creationdate><title>Helicopter skid landing gear</title><author>GUILLOT, MICHEL ; LEVESQUE, JULIE ; AQUINO, GIUSEPPE ; FEWS, ROBERT CLIVE ; GAKWAYA, AUGUSTIN ; BERNIER, SIMON ; ELIE-DIT-COSAQUE, XAVIER JEAN-GILLES ; BLANCHET, JOCELYN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_EP2746155A13</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; fre ; ger</language><creationdate>2014</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION</topic><topic>GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC</topic><topic>GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS</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>HEAT EXCHANGE IN GENERAL</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL</topic><topic>PERFORMING OPERATIONS</topic><topic>PUNCHING METAL</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER USPC</topic><topic>TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS</topic><topic>TRANSPORTING</topic><topic>WEAPONS</topic><topic>WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS ORPROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL</topic><toplevel>online_resources</toplevel><creatorcontrib>GUILLOT, MICHEL</creatorcontrib><creatorcontrib>LEVESQUE, JULIE</creatorcontrib><creatorcontrib>AQUINO, GIUSEPPE</creatorcontrib><creatorcontrib>FEWS, ROBERT CLIVE</creatorcontrib><creatorcontrib>GAKWAYA, AUGUSTIN</creatorcontrib><creatorcontrib>BERNIER, SIMON</creatorcontrib><creatorcontrib>ELIE-DIT-COSAQUE, XAVIER JEAN-GILLES</creatorcontrib><creatorcontrib>BLANCHET, JOCELYN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>GUILLOT, MICHEL</au><au>LEVESQUE, JULIE</au><au>AQUINO, GIUSEPPE</au><au>FEWS, ROBERT CLIVE</au><au>GAKWAYA, AUGUSTIN</au><au>BERNIER, SIMON</au><au>ELIE-DIT-COSAQUE, XAVIER JEAN-GILLES</au><au>BLANCHET, JOCELYN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Helicopter skid landing gear</title><date>2014-06-25</date><risdate>2014</risdate><abstract>A cross tube for a helicopter skid landing gear, including a monolithic metallic tube having a central portion (28) extending transversely between two end portions (30) with longitudinal central axes (A C , A E ) of the central portion (28) and of the end portions (30) being located in a plane (P), where the central portion (28) has inner and outer heights (H ci , H co ), the end portions (30) each have inner and outer heights (H ei , H eo ), and the inner and outer heights of one of the central portion (28) and the end portion (30) are respectively greater than the inner and outer heights of the other of the central portion (28) and the end portion (30). A skid tube (22) with two portions (22b, 22d, 22a, 22c) with cross-sections having one or both of different orientations with respect to one another and different dimensions with respect to one another, and a method of forming a structural tube (22, 24, 26) for a helicopter skid landing gear (20) are also provided.</abstract><oa>free_for_read</oa></addata></record> |
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language | eng ; fre ; ger |
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subjects | AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OFGENERAL APPLICATION GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HEAT EXCHANGE IN GENERAL HEATING HELICOPTERS LIGHTING MECHANICAL ENGINEERING MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVINGMATERIAL PERFORMING OPERATIONS PUNCHING METAL TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION TECHNICAL SUBJECTS COVERED BY FORMER USPC TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TRANSPORTING WEAPONS WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS ORPROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL |
title | Helicopter skid landing gear |
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