http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-3902325-A1
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_fd4735dbc2bd2bb60a1673344a4a95c1 |
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D2027-268 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-26 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-18 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-18 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-26 |
| filingDate | 1989-01-26^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_9cc88cc41eee82d1901d8a6df2d8930a |
| publicationDate | 1989-09-21^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | DE-3902325-A1 |
| titleOfInvention | METHOD FOR SUSPENDING A MANIFOLD FAN GAS TURBINE ENGINE FROM AN AIRPLANE |
| abstract | A bypass fan gas-turbine engine (12) on a supporting pylon (14) is rigidly connected via guide rods (18 and 20) and bolted flanges with metallic mutual contact, such that no relative movement can take place between them as a result of vibration. In contrast, the pylon (14) is mounted on the aircraft load-bearing structure (38 and 40) via connections which have elastic sleeves. The arrangement ensures greater robustness of the structure, consisting of the fan structure and the core gas generator. <IMAGE> |
| priorityDate | 1988-03-08^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
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