http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-111272877-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_71dbd3952f2600e4fc0bafe7902188fb |
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01N2291-0232 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01N29-04 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01N29-04 |
| filingDate | 2020-03-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_2945d7bf8f758416d1e859bd45a3d5f4 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a3e1eef6564496cd9f1ab2766e25c02f |
| publicationDate | 2020-06-12-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-111272877-A |
| titleOfInvention | A kind of non-cold area airport runway structure health monitoring system and control evaluation method |
| abstract | A non-cold region airport runway structure health monitoring system and control evaluation method. The system includes a plurality of acceleration sensors, a Wifi communication module, a data storage module, a power supply, an industrial computer and a background server; the non-cold area airport runway structure health monitoring system and control evaluation method provided by the present invention have the following advantages: (1) easy to implement. The acceleration sensor can be placed directly inside the lamp housing of the airport runway center line lamp, and the power cable and data cable are routed from the lamp power cable, which is convenient for construction and later management. (2) The calculation is convenient. Using the airport runway surface theory and the measured acceleration value combined with the aircraft mass information can be quickly solved, greatly improving the calculation speed. (3) High security. The system layout does not cause any damage to the runway structure, and the actual safety performance of the runway is instantly evaluated by using the aircraft's actual load model safety evaluation. |
| priorityDate | 2020-03-15-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 17.