| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c72d118f5664072de841f9c5c34b9d99 |
| classificationCPCAdditional |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2240-12
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-208
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-207
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2260-205 |
| classificationCPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D9-041
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D9-023
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F01D5-185
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-16 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-12 |
| filingDate |
2010-10-19-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_064c64fa886f8b21c8da8fd1b81e2226
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_d6b7788cc01ae7433e2051fa5b925e94 |
| publicationDate |
2011-05-12-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
DE-102010038274-A1 |
| titleOfInvention |
Apparatus and method for cooling gas turbines |
| abstract |
A gas turbine engine (10) includes a turbine housing (40), a turbine (16) configured to receive hot combustion gas, thermal energy from the hot combustion gas subjected turbine component (22), and a turbine housing disposed outside the turbine housing and a cooling system (92) having cooling medium (99) therein. A heat pipe (72, 74) has a high temperature end in communication with the turbine component and a low temperature end extending from the turbine housing in communication with the cooling medium in the cooling system to transfer the heat energy from the component to the cooling medium. |
| priorityDate |
2009-10-30-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |