http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-111731465-A

Outgoing Links

Predicate Object
assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_cf2fab8425eeb6c70b1535bb1c580859
classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64U10-25
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C1-061
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C1-06
filingDate 2020-06-30^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_18faa3fdb536aed250d800b4e0e41038
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_b5e87432da0d631cf9bc77fa30388baf
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f00e5340421ba234752ba122993877bb
publicationDate 2020-10-02^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-111731465-A
titleOfInvention A fuselage frame structure for unmanned aerial vehicle and unmanned aerial vehicle
abstract The invention discloses a fuselage frame structure for an unmanned aerial vehicle and an unmanned aerial vehicle, comprising a fuselage frame and a wing connecting frame, wherein the fuselage frame comprises a fourth frame, a second frame, a fifth frame, a third frame The frame and the two first frames, the fifth frame is further provided with a sixth frame in parallel on the side away from the fourth frame, the integrated circuit frame is vertically installed on the side of the sixth frame close to the fifth frame, and the side away from the fifth frame is fixedly installed with an integrated circuit frame. The engine mount; the wing connecting frame includes a first wing connecting carbon tube and a second wing connecting carbon tube. The invention optimizes the design of the traditional UAV using the skin as the main load-bearing structure of the fuselage, divides the fuselage into multiple areas, and each load has its fixed installation position, which is convenient for space allocation and ensures that each component is in the space When the load is installed, the accuracy of the center of gravity of the whole machine is ensured; different equipment spaces are divided according to different equipment functions, which can be quickly disassembled and assembled, which is convenient for inspection and maintenance.
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-114228418-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-114228418-B
priorityDate 2020-06-30^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

Incoming Links

Predicate Subject
isCitedBy http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-109353513-A
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-110466750-A
isDiscussedBy http://rdf.ncbi.nlm.nih.gov/pubchem/anatomy/ANATOMYID14
http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID297
http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID419559581

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