Vibration reduction mechanism and flight equipment
The embodiment of the utility model discloses a vibration reduction mechanism and flight equipment. The vibration reduction mechanism comprises a containing unit, a mandrel and a first vibration reduction part. The interior of the containing unit is hollow to form a containing chamber, the first vib...
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| creator | SHEN ZONGZHANG WU TONGGANG DUAN BOYANG |
| description | The embodiment of the utility model discloses a vibration reduction mechanism and flight equipment. The vibration reduction mechanism comprises a containing unit, a mandrel and a first vibration reduction part. The interior of the containing unit is hollow to form a containing chamber, the first vibration reduction part and at least part of the mandrel are arranged in the containing chamber, the mandrel and the first vibration reduction part are sequentially arranged in the vertical direction, and the mandrel is fixedly connected with the first vibration reduction part; wherein the first vibration reduction part is made of a rubber element, the first vibration reduction part is provided with a corner angle, at least two first vibration reduction grooves are formed in the corner angle of the first vibration reduction part, and a vibration reduction space is formed between each first vibration reduction groove and the containing unit. According to the damping device, it is guaranteed that deformation spaces are |
| format | Patent |
| fullrecord | <record><control><sourceid>epo_EVB</sourceid><recordid>TN_cdi_epo_espacenet_CN219911597UU</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>CN219911597UU</sourcerecordid><originalsourceid>FETCH-epo_espacenet_CN219911597UU3</originalsourceid><addsrcrecordid>eNrjZDAKy0wqSizJzM9TKEpNKU0Gs3JTkzMS8zKLcxUS81IU0nIy0zNKFFILSzMLclPzSngYWNMSc4pTeaE0N4OSm2uIs4duakF-fGpxQWJyal5qSbyzn5GhpaWhoamleWioMVGKAFjiLV4</addsrcrecordid><sourcetype>Open Access Repository</sourcetype><iscdi>true</iscdi><recordtype>patent</recordtype></control><display><type>patent</type><title>Vibration reduction mechanism and flight equipment</title><source>esp@cenet</source><creator>SHEN ZONGZHANG ; WU TONGGANG ; DUAN BOYANG</creator><creatorcontrib>SHEN ZONGZHANG ; WU TONGGANG ; DUAN BOYANG</creatorcontrib><description>The embodiment of the utility model discloses a vibration reduction mechanism and flight equipment. The vibration reduction mechanism comprises a containing unit, a mandrel and a first vibration reduction part. The interior of the containing unit is hollow to form a containing chamber, the first vibration reduction part and at least part of the mandrel are arranged in the containing chamber, the mandrel and the first vibration reduction part are sequentially arranged in the vertical direction, and the mandrel is fixedly connected with the first vibration reduction part; wherein the first vibration reduction part is made of a rubber element, the first vibration reduction part is provided with a corner angle, at least two first vibration reduction grooves are formed in the corner angle of the first vibration reduction part, and a vibration reduction space is formed between each first vibration reduction groove and the containing unit. According to the damping device, it is guaranteed that deformation spaces are</description><language>chi ; eng</language><subject>BLASTING ; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR ; ENGINEERING ELEMENTS AND UNITS ; FLUID-PRESSURE ACTUATORS ; FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS ; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS ; HEATING ; HYDRAULICS OR PNEUMATICS IN GENERAL ; LIGHTING ; MEANS FOR DAMPING VIBRATION ; MECHANICAL ENGINEERING ; SHOCK-ABSORBERS ; SPRINGS ; SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL ; THERMAL INSULATION IN GENERAL ; WEAPONS</subject><creationdate>2023</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=20231027&DB=EPODOC&CC=CN&NR=219911597U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,777,882,25545,76296</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20231027&DB=EPODOC&CC=CN&NR=219911597U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SHEN ZONGZHANG</creatorcontrib><creatorcontrib>WU TONGGANG</creatorcontrib><creatorcontrib>DUAN BOYANG</creatorcontrib><title>Vibration reduction mechanism and flight equipment</title><description>The embodiment of the utility model discloses a vibration reduction mechanism and flight equipment. The vibration reduction mechanism comprises a containing unit, a mandrel and a first vibration reduction part. The interior of the containing unit is hollow to form a containing chamber, the first vibration reduction part and at least part of the mandrel are arranged in the containing chamber, the mandrel and the first vibration reduction part are sequentially arranged in the vertical direction, and the mandrel is fixedly connected with the first vibration reduction part; wherein the first vibration reduction part is made of a rubber element, the first vibration reduction part is provided with a corner angle, at least two first vibration reduction grooves are formed in the corner angle of the first vibration reduction part, and a vibration reduction space is formed between each first vibration reduction groove and the containing unit. According to the damping device, it is guaranteed that deformation spaces are</description><subject>BLASTING</subject><subject>DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR</subject><subject>ENGINEERING ELEMENTS AND UNITS</subject><subject>FLUID-PRESSURE ACTUATORS</subject><subject>FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS</subject><subject>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</subject><subject>HEATING</subject><subject>HYDRAULICS OR PNEUMATICS IN GENERAL</subject><subject>LIGHTING</subject><subject>MEANS FOR DAMPING VIBRATION</subject><subject>MECHANICAL ENGINEERING</subject><subject>SHOCK-ABSORBERS</subject><subject>SPRINGS</subject><subject>SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL</subject><subject>THERMAL INSULATION IN GENERAL</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2023</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAKy0wqSizJzM9TKEpNKU0Gs3JTkzMS8zKLcxUS81IU0nIy0zNKFFILSzMLclPzSngYWNMSc4pTeaE0N4OSm2uIs4duakF-fGpxQWJyal5qSbyzn5GhpaWhoamleWioMVGKAFjiLV4</recordid><startdate>20231027</startdate><enddate>20231027</enddate><creator>SHEN ZONGZHANG</creator><creator>WU TONGGANG</creator><creator>DUAN BOYANG</creator><scope>EVB</scope></search><sort><creationdate>20231027</creationdate><title>Vibration reduction mechanism and flight equipment</title><author>SHEN ZONGZHANG ; WU TONGGANG ; DUAN BOYANG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN219911597UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>chi ; eng</language><creationdate>2023</creationdate><topic>BLASTING</topic><topic>DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR</topic><topic>ENGINEERING ELEMENTS AND UNITS</topic><topic>FLUID-PRESSURE ACTUATORS</topic><topic>FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS</topic><topic>GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS</topic><topic>HEATING</topic><topic>HYDRAULICS OR PNEUMATICS IN GENERAL</topic><topic>LIGHTING</topic><topic>MEANS FOR DAMPING VIBRATION</topic><topic>MECHANICAL ENGINEERING</topic><topic>SHOCK-ABSORBERS</topic><topic>SPRINGS</topic><topic>SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL</topic><topic>THERMAL INSULATION IN GENERAL</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>SHEN ZONGZHANG</creatorcontrib><creatorcontrib>WU TONGGANG</creatorcontrib><creatorcontrib>DUAN BOYANG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SHEN ZONGZHANG</au><au>WU TONGGANG</au><au>DUAN BOYANG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Vibration reduction mechanism and flight equipment</title><date>2023-10-27</date><risdate>2023</risdate><abstract>The embodiment of the utility model discloses a vibration reduction mechanism and flight equipment. The vibration reduction mechanism comprises a containing unit, a mandrel and a first vibration reduction part. The interior of the containing unit is hollow to form a containing chamber, the first vibration reduction part and at least part of the mandrel are arranged in the containing chamber, the mandrel and the first vibration reduction part are sequentially arranged in the vertical direction, and the mandrel is fixedly connected with the first vibration reduction part; wherein the first vibration reduction part is made of a rubber element, the first vibration reduction part is provided with a corner angle, at least two first vibration reduction grooves are formed in the corner angle of the first vibration reduction part, and a vibration reduction space is formed between each first vibration reduction groove and the containing unit. According to the damping device, it is guaranteed that deformation spaces are</abstract><oa>free_for_read</oa></addata></record> |
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| language | chi ; eng |
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| subjects | BLASTING DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR ENGINEERING ELEMENTS AND UNITS FLUID-PRESSURE ACTUATORS FLUID-PRESSURE ACTUATORS, e.g. SERVO-MOTORS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HYDRAULICS OR PNEUMATICS IN GENERAL LIGHTING MEANS FOR DAMPING VIBRATION MECHANICAL ENGINEERING SHOCK-ABSORBERS SPRINGS SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL THERMAL INSULATION IN GENERAL WEAPONS |
| title | Vibration reduction mechanism and flight equipment |
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