http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-111204464-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_58286784ceb94b973e74a24c9993f2a1 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-24 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D29-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D33-08 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-26 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D29-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D29-04 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D29-04 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D29-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-24 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D29-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-26 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D33-08 |
| filingDate | 2020-03-13^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_17d62a40c59b54741d55c189e0654e82 |
| publicationDate | 2020-05-29^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-111204464-A |
| titleOfInvention | Fairing, aircraft and aircraft heat dissipation method |
| abstract | The invention discloses a fairing, an aircraft and an aircraft heat dissipation method. The fairing comprises an air inlet and a flow guide structure, wherein the flow guide structure is used for dredging air entering from the air inlet; during assembly, the fairing is fixedly arranged in front of the blades of the aircraft and rotates along with the blades when the blades rotate, so that air enters from the air inlet and is exhausted by the flow guide structure in an accelerating manner, and the air fluidity in the fairing is increased, so that the heat of the motor behind the blades is dissipated. Because this application radome fairing includes air intake and water conservancy diversion structure, install the paddle the place ahead at the aircraft during assembly and rotate along with the paddle, the air intake can make the air get into the radome fairing, and the water conservancy diversion structure can make the air that gets into discharge with higher speed to increase the gas mobility in the radome fairing, reach the radiating effect of motor for the paddle rear, consequently solved the heat dissipation problem of motor, improved the life of motor, also strengthened the security performance of aircraft flight. |
| isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-114194403-A |
| priorityDate | 2020-03-13^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
| Predicate | Subject |
|---|---|
| isDiscussedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID962 http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID419512635 |
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