Pure mechanical type heavy landing indication structure
A pure mechanical type heavy landing indication structure includes a landing gear buffer supporting pillar, a bracket and a cutter; an indication wire is mounted on the bracket, the bracket is fixed on the upper end of the landing gear buffer supporting pillar, a cutter bracket is mounted on the low...
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| creator | QU HUASHAN XU HUANYU GUO WEI ZHONG XIAOHONG WANG ZHIZHU DUAN XINXING ZHANG GAIHUA WANG BIN DENG WENWEN LI CANSHAN ZHANG WEI PENG RUI ZHANG DANDAN |
| description | A pure mechanical type heavy landing indication structure includes a landing gear buffer supporting pillar, a bracket and a cutter; an indication wire is mounted on the bracket, the bracket is fixed on the upper end of the landing gear buffer supporting pillar, a cutter bracket is mounted on the lower end of the landing gear buffer supporting pillar, and the cutter used for cutting the indicationwire is mounted on the cutter bracket; the upper end of the landing gear buffer supporting pillar is a fixed end, and the lower end of the landing gear buffer supporting pillar is a movable end; whenan aircraft lands normally, the cutter cannot collide with the indication wire, and when a heavy landing occurs, the cutter crushes into the bracket equipped with the indication wire and cuts off theindication wire; the heavy landing indication structure does not require support of additional power, air supply, hydraulic pressure, and the like, as long as appropriate adjustment is performed on astructure of a connection pa |
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XU HUANYU ; GUO WEI ; ZHONG XIAOHONG ; WANG ZHIZHU ; DUAN XINXING ; ZHANG GAIHUA ; WANG BIN ; DENG WENWEN ; LI CANSHAN ; ZHANG WEI ; PENG RUI ; ZHANG DANDAN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN109606713A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2019</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR</topic><topic>EQUIPMENT FOR FITTING IN OR TO AIRCRAFT</topic><topic>FLYING SUITS</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>HELICOPTERS</topic><topic>PARACHUTES</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>QU HUASHAN</creatorcontrib><creatorcontrib>XU HUANYU</creatorcontrib><creatorcontrib>GUO WEI</creatorcontrib><creatorcontrib>ZHONG XIAOHONG</creatorcontrib><creatorcontrib>WANG ZHIZHU</creatorcontrib><creatorcontrib>DUAN XINXING</creatorcontrib><creatorcontrib>ZHANG GAIHUA</creatorcontrib><creatorcontrib>WANG BIN</creatorcontrib><creatorcontrib>DENG WENWEN</creatorcontrib><creatorcontrib>LI CANSHAN</creatorcontrib><creatorcontrib>ZHANG WEI</creatorcontrib><creatorcontrib>PENG RUI</creatorcontrib><creatorcontrib>ZHANG DANDAN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>QU HUASHAN</au><au>XU HUANYU</au><au>GUO WEI</au><au>ZHONG XIAOHONG</au><au>WANG ZHIZHU</au><au>DUAN XINXING</au><au>ZHANG GAIHUA</au><au>WANG BIN</au><au>DENG WENWEN</au><au>LI CANSHAN</au><au>ZHANG WEI</au><au>PENG RUI</au><au>ZHANG DANDAN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Pure mechanical type heavy landing indication structure</title><date>2019-04-12</date><risdate>2019</risdate><abstract>A pure mechanical type heavy landing indication structure includes a landing gear buffer supporting pillar, a bracket and a cutter; an indication wire is mounted on the bracket, the bracket is fixed on the upper end of the landing gear buffer supporting pillar, a cutter bracket is mounted on the lower end of the landing gear buffer supporting pillar, and the cutter used for cutting the indicationwire is mounted on the cutter bracket; the upper end of the landing gear buffer supporting pillar is a fixed end, and the lower end of the landing gear buffer supporting pillar is a movable end; whenan aircraft lands normally, the cutter cannot collide with the indication wire, and when a heavy landing occurs, the cutter crushes into the bracket equipped with the indication wire and cuts off theindication wire; the heavy landing indication structure does not require support of additional power, air supply, hydraulic pressure, and the like, as long as appropriate adjustment is performed on astructure of a connection pa</abstract><oa>free_for_read</oa></addata></record> |
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| subjects | AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| title | Pure mechanical type heavy landing indication structure |
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