Autorotation rotorcraft
The utility model relates to an autorotation rotorcraft. The autorotation rotorcraft comprises a frame, a body, an engine, a rotor, a propeller, a tail vane, an operating rod, an instrument and an undercarriage, wherein the upper end of the frame is connected with the rotor; the engine is positioned...
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| description | The utility model relates to an autorotation rotorcraft. The autorotation rotorcraft comprises a frame, a body, an engine, a rotor, a propeller, a tail vane, an operating rod, an instrument and an undercarriage, wherein the upper end of the frame is connected with the rotor; the engine is positioned between the tail vane and a cockpit; the instrument and the operating rod are arranged in the cockpit; the engine is connected with the propeller; the undercarriage is arranged below the frame; the rotor consists of two blades which are fixed at the upper end of the frame through a blade shaft. The autorotation rotorcraft has the benefits of high safety, short take-off and landing distance, high stability, high wind resistance and higher cost performance. |
| format | Patent |
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The autorotation rotorcraft comprises a frame, a body, an engine, a rotor, a propeller, a tail vane, an operating rod, an instrument and an undercarriage, wherein the upper end of the frame is connected with the rotor; the engine is positioned between the tail vane and a cockpit; the instrument and the operating rod are arranged in the cockpit; the engine is connected with the propeller; the undercarriage is arranged below the frame; the rotor consists of two blades which are fixed at the upper end of the frame through a blade shaft. The autorotation rotorcraft has the benefits of high safety, short take-off and landing distance, high stability, high wind resistance and higher cost performance.</description><language>eng</language><subject>AEROPLANES ; AIRCRAFT ; AVIATION ; COSMONAUTICS ; HELICOPTERS ; PERFORMING OPERATIONS ; TRANSPORTING</subject><creationdate>2015</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=20150318&DB=EPODOC&CC=CN&NR=204210731U$$EHTML$$P50$$Gepo$$Hfree_for_read</linktohtml><link.rule.ids>230,308,776,881,25542,76516</link.rule.ids><linktorsrc>$$Uhttps://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20150318&DB=EPODOC&CC=CN&NR=204210731U$$EView_record_in_European_Patent_Office$$FView_record_in_$$GEuropean_Patent_Office$$Hfree_for_read</linktorsrc></links><search><creatorcontrib>SU GUIBIN</creatorcontrib><title>Autorotation rotorcraft</title><description>The utility model relates to an autorotation rotorcraft. The autorotation rotorcraft comprises a frame, a body, an engine, a rotor, a propeller, a tail vane, an operating rod, an instrument and an undercarriage, wherein the upper end of the frame is connected with the rotor; the engine is positioned between the tail vane and a cockpit; the instrument and the operating rod are arranged in the cockpit; the engine is connected with the propeller; the undercarriage is arranged below the frame; the rotor consists of two blades which are fixed at the upper end of the frame through a blade shaft. The autorotation rotorcraft has the benefits of high safety, short take-off and landing distance, high stability, high wind resistance and higher cost performance.</description><subject>AEROPLANES</subject><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>COSMONAUTICS</subject><subject>HELICOPTERS</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2015</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZBB3LC3JL8ovSSzJzM9TADLyi5KLEtNKeBhY0xJzilN5oTQ3g5Kba4izh25qQX58anFBYnJqXmpJvLOfkYGJkaGBubFhaKgxUYoASa4jKQ</recordid><startdate>20150318</startdate><enddate>20150318</enddate><creator>SU GUIBIN</creator><scope>EVB</scope></search><sort><creationdate>20150318</creationdate><title>Autorotation rotorcraft</title><author>SU GUIBIN</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_CN204210731UU3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng</language><creationdate>2015</creationdate><topic>AEROPLANES</topic><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>COSMONAUTICS</topic><topic>HELICOPTERS</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><toplevel>online_resources</toplevel><creatorcontrib>SU GUIBIN</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>SU GUIBIN</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>Autorotation rotorcraft</title><date>2015-03-18</date><risdate>2015</risdate><abstract>The utility model relates to an autorotation rotorcraft. The autorotation rotorcraft comprises a frame, a body, an engine, a rotor, a propeller, a tail vane, an operating rod, an instrument and an undercarriage, wherein the upper end of the frame is connected with the rotor; the engine is positioned between the tail vane and a cockpit; the instrument and the operating rod are arranged in the cockpit; the engine is connected with the propeller; the undercarriage is arranged below the frame; the rotor consists of two blades which are fixed at the upper end of the frame through a blade shaft. The autorotation rotorcraft has the benefits of high safety, short take-off and landing distance, high stability, high wind resistance and higher cost performance.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng |
| recordid | cdi_epo_espacenet_CN204210731UU |
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| subjects | AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING |
| title | Autorotation rotorcraft |
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