http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-214741728-U

Outgoing Links

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assignee http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_06e4573b06d20bba3e9810dd0ee54880
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K9-58
filingDate 2020-12-29-04:00^^<http://www.w3.org/2001/XMLSchema#date>
grantDate 2021-11-16-04:00^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_4edc3a4c625930e6403c755f414fd487
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_26a110f597ce271b57f7ac82a69ad736
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publicationDate 2021-11-16-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber CN-214741728-U
titleOfInvention Isolation control device suitable for attitude and orbit control power system
abstract The utility model provides an isolation control device suitable for attitude and orbit control driving system, which comprises a gas generating device, a gas storage shell, a capillary guide pipe and a gas explosion valve. During storage of the attitude and orbit control power system, the gas explosion valve is in a closed state to play an isolation role; when the attitude and orbit control power system is ready to work and needs to be isolated, the gas generating device is ignited to generate gas, the gas storage shell is used for equalizing the pressure of the generated gas, the gas is conveyed to each gas explosion valve through the capillary guide pipe, and the gas explosion valves are cut open to remove the isolation. The gas storage shell is designed with a certain volume, which not only plays a role of reducing the pressure peak of gas production of the gas production device, but also plays a role of ensuring that the pressure is not too low to influence the opening of other gas explosion valves after the individual gas explosion valve is opened; the capillary guide tube adopts a stainless steel seamless tube or a titanium capillary tube with smaller outer diameter, has better flexibility and is convenient to arrange in an attitude and orbit control power system, and has smaller weight and stronger bearing capacity.
priorityDate 2020-12-29-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

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Total number of triples: 29.