http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-112943253-A
Outgoing Links
Predicate | Object |
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assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_e89c206df73c7928c3fa05f87f1287de |
classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/E21C50-00 |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/E21C50-00 |
filingDate | 2021-02-02^^<http://www.w3.org/2001/XMLSchema#date> |
inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_c4e5055bbe84606376212c8f5ca6e335 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_bcdef05d9cc721ee33694a2d4a0e83fa http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6d6139c612bf42b1990289df156777a0 |
publicationDate | 2021-06-11^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber | CN-112943253-A |
titleOfInvention | A double-wing type submarine polymetallic nodule collection device |
abstract | The invention discloses a double-wing type submarine polymetallic nodule collecting device, comprising a fuselage and two wing bodies, the two wing bodies are respectively located on both sides of the fuselage, one end of the wing body is movably connected with the fuselage, and the two wing bodies are movably connected between the two wing bodies. Connected by an adjusting device; a ski board is arranged at the bottom of the fuselage; the wing body includes a wing tip baffle, a collection rake, a jet device, a baffle shell, a slide plate, and a conveyor belt. The conveyor belt is located behind the collection rake, and the wing tip baffle is located in the collection On the outside of the rake, the baffle shell is located behind the collecting rake and the conveyor belt, and the jet device is located on the baffle shell; a sliding plate is arranged at the bottom of the wing body, the distance between the sliding plate and the wing body is adjustable, and the height of the wing body from the ground can be adjusted; The body and the fuselage are connected by rotating parts, and a locking device is also arranged between the wing body and the fuselage. The invention can achieve technical effects such as wide application range, reducing forward resistance, and improving the field of view of the seabed mining vehicle. |
isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-115387792-A |
priorityDate | 2021-02-02^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
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