Landing gear components having improved joints
The present disclosure includes landing gear components, such as an outer cylinder of a shock strut assembly. The outer cylinder includes one or more structural attachment pins configured to engage with other components of the landing gear including pintle frames, drag braces, and torque links. The...
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| creator | Haynes Noel C Manzini Marilea |
| description | The present disclosure includes landing gear components, such as an outer cylinder of a shock strut assembly. The outer cylinder includes one or more structural attachment pins configured to engage with other components of the landing gear including pintle frames, drag braces, and torque links. The pins include a cobalt alloy mated to a receptacle having a cobalt-containing coating on an inner surface, which eliminates the need for a bushing between the pin and the receptacle of the corresponding landing gear component. |
| format | Patent |
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The outer cylinder includes one or more structural attachment pins configured to engage with other components of the landing gear including pintle frames, drag braces, and torque links. The pins include a cobalt alloy mated to a receptacle having a cobalt-containing coating on an inner surface, which eliminates the need for a bushing between the pin and the receptacle of the corresponding landing gear component.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; ALLOYS ; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT ; AVIATION ; BLASTING ; CHEMISTRY ; COSMONAUTICS ; ENGINEERING ELEMENTS AND UNITS ; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT ; FERROUS OR NON-FERROUS ALLOYS ; FLYING SUITS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; HELICOPTERS ; LIGHTING ; MEANS FOR DAMPING VIBRATION ; MECHANICAL ENGINEERING ; METALLURGY ; PARACHUTES ; PERFORMING OPERATIONS ; SHOCK-ABSORBERS ; SPRINGS ; THERMAL INSULATION IN GENERAL ; TRANSPORTING ; TREATMENT OF ALLOYS OR NON-FERROUS METALS ; WEAPONS</subject><creationdate>2016</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=20160927&DB=EPODOC&CC=US&NR=9452827B2$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25543,76294</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20160927&DB=EPODOC&CC=US&NR=9452827B2$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>Haynes Noel C</creatorcontrib><creatorcontrib>Manzini Marilea</creatorcontrib><title>Landing gear components having improved joints</title><description>The present disclosure includes landing gear components, such as an outer cylinder of a shock strut assembly. The outer cylinder includes one or more structural attachment pins configured to engage with other components of the landing gear including pintle frames, drag braces, and torque links. The pins include a cobalt alloy mated to a receptacle having a cobalt-containing coating on an inner surface, which eliminates the need for a bushing between the pin and the receptacle of the corresponding landing gear component.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>ALLOYS</subject><subject>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>CHEMISTRY</subject><subject>COSMONAUTICS</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</subject><subject>FERROUS OR NON-FERROUS ALLOYS</subject><subject>FLYING SUITS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>HELICOPTERS</subject><subject>LIGHTING</subject><subject>MEANS FOR DAMPING VIBRATION</subject><subject>MECHANICAL ENGINEERING</subject><subject>METALLURGY</subject><subject>PARACHUTES</subject><subject>PERFORMING OPERATIONS</subject><subject>SHOCK-ABSORBERS</subject><subject>SPRINGS</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>TRANSPORTING</subject><subject>TREATMENT OF ALLOYS OR NON-FERROUS METALS</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2016</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZNDzScxLycxLV0hPTSxSSM7PLcjPS80rKVbISCwDCWfmFhTll6WmKGTlZwKFeRhY0xJzilN5oTQ3g4Kba4izh25qQX58anFBYnJqXmpJfGiwpYmpkYWRuZORMRFKAMhNKq0</recordid><startdate>20160927</startdate><enddate>20160927</enddate><creator>Haynes Noel C</creator><creator>Manzini Marilea</creator><scope>EVB</scope></search><sort><creationdate>20160927</creationdate><title>Landing gear components having improved joints</title><author>Haynes Noel C ; Manzini Marilea</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_US9452827B23</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2016</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ALLOYS</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>CHEMISTRY</topic><topic>COSMONAUTICS</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FERROUS OR NON-FERROUS ALLOYS</topic><topic>FLYING SUITS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>HELICOPTERS</topic><topic>LIGHTING</topic><topic>MEANS FOR DAMPING VIBRATION</topic><topic>MECHANICAL ENGINEERING</topic><topic>METALLURGY</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>SHOCK-ABSORBERS</topic><topic>SPRINGS</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>TRANSPORTING</topic><topic>TREATMENT OF ALLOYS OR NON-FERROUS METALS</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>Haynes Noel C</creatorcontrib><creatorcontrib>Manzini Marilea</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>Haynes Noel C</au><au>Manzini Marilea</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Landing gear components having improved joints</title><date>2016-09-27</date><risdate>2016</risdate><abstract>The present disclosure includes landing gear components, such as an outer cylinder of a shock strut assembly. The outer cylinder includes one or more structural attachment pins configured to engage with other components of the landing gear including pintle frames, drag braces, and torque links. The pins include a cobalt alloy mated to a receptacle having a cobalt-containing coating on an inner surface, which eliminates the need for a bushing between the pin and the receptacle of the corresponding landing gear component.</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT ALLOYS ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING CHEMISTRY COSMONAUTICS ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FERROUS OR NON-FERROUS ALLOYS FLYING SUITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MEANS FOR DAMPING VIBRATION MECHANICAL ENGINEERING METALLURGY PARACHUTES PERFORMING OPERATIONS SHOCK-ABSORBERS SPRINGS THERMAL INSULATION IN GENERAL TRANSPORTING TREATMENT OF ALLOYS OR NON-FERROUS METALS WEAPONS |
| title | Landing gear components having improved joints |
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