http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-109670232-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_06e4573b06d20bba3e9810dd0ee54880 |
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T90-00 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G06F30-20 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G06F17-50 |
| filingDate | 2018-12-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_4cddd9b3eb5c043dd95cec4223a6509d http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5d14e9e55764a88f95e118b4c4606c39 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_965ea1040c734f1ae7ef2550fac5e88e http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f6bc8b593098ecde61d4c4dab4ac9638 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d37bab535f8095620dfa39b58a472437 http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_b956eee0a7fa6053af238c5f5e1d0bac http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_f65e601cd471e63821c07c1ae0a4b4d2 |
| publicationDate | 2019-04-23-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-109670232-A |
| titleOfInvention | A method for quickly estimating the size and weight of the attitude control two-component thrust chamber |
| abstract | The invention provides a method for quickly estimating the size and weight of the attitude control double-component thrust chamber, which divides the attitude control double-component thrust chamber into three main parts, and quantitatively describes the key design dimensions and performance parameters in the design process , obtain the geometric outline of the thrust chamber through parameter driving, use the strength check formula to determine the wall thickness of the thrust chamber according to the selected safety factor, and obtain the thrust chamber weight by statistical calculation combined with the selected material density. Help researchers to quickly and efficiently design thrust chambers and predict performance. This method realizes the rapid design and performance prediction of the attitude control two-component thrust chamber product in the demonstration stage of the power system system, greatly improves the design demonstration efficiency of the product, and shortens the demonstration period. greater application prospects. |
| priorityDate | 2018-12-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 21.