http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-105958597-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_01ea580ae0fb1a70e9aceb43f74bdeca |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H02J7-0026 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H02H11-002 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/H02J7-0034 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H02H11-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/H02J7-00 |
| filingDate | 2016-06-23-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d40f3bd858454cceab9aecbfc173b4e7 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_09779a04eeeeb3e319b24a96608a23be http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_cdf13efa8a76f27648ca42995bddec7e |
| publicationDate | 2016-09-21-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-105958597-A |
| titleOfInvention | Ground starting power supply for aircraft |
| abstract | The invention discloses a ground starting power supply for an aircraft. The ground starting power supply comprises a module combined type frame, three cell modules, a control module and an output cable, wherein the cell modules and the control module are connected with the module combined type frame; and the output cable is connected with the control module. The ground starting power supply has the advantages as follows: a lithium iron phosphate battery pack is initially adopted in the cell part to replace the 7-HK-182 lead-acid storage battery in China, so that high reliability is realized; the appearance of the power supply is optimized to be small in size, and the power supply can be charged in a fully automatic manner, so that the service life of the equipment can be greatly prolonged; meanwhile, the starting power supply adopts the modular design, so that the starting power supply is particularly suitable for airplane starting and electrification check operations in occasions of complex landforms, emergency rescuing and the like; the capacity of the battery is the maximum of the same type equipment at home and abroad, and the requirement of long-term continuous operation task can be met; and in addition, the ground starting power supply can satisfy the requirements of ground starting and electrification check operations of small and medium size fixed wing aircrafts and helicopters. |
| priorityDate | 2016-06-23-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 27.