http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-110341968-A
Outgoing Links
| Predicate | Object |
|---|---|
| assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_4e3c804fb60c8285b549597da004115a |
| classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2230-72 |
| classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D27-18 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K1-70 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D29-08 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D29-06 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K1-72 |
| classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64D27-18 |
| filingDate | 2019-04-03^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_1405ce68d3312e421de6b3b19c81da9a http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_389bf15abc4052d6d43e9fd972c111bd http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_a2ae36371b2a3a55c27c6db726e572a3 |
| publicationDate | 2019-10-18^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber | CN-110341968-A |
| titleOfInvention | Ducted fan turbojets and aircraft |
| abstract | The present invention relates to a ducted fan turbojet engine (100) and an aircraft, the ducted fan turbojet engine comprising a nacelle (102), the nacelle comprising a fixed structure (207), a thrust reverser system ( 250), the thrust reverser system has a frame (208b), a movable structure (208a) fastened to the frame, and an inner door (208c) and an outer door (208d) hinged to the frame. The frame is movable in translation between a forward position and a rear position on the fixed structure to define a window (210) between the fixed structure and the movable structure, the window between the bypass duct and the short Open between the outside of the cabin. Each door (208c-d) is movable between a stowed position and a deployed position, and the movable structure is assembled to be hinged to the frame by at least one hinge (402), the axis of rotation of which is generally is parallel to the longitudinal axis X of the ducted fan turbojet engine (100). |
| priorityDate | 2018-04-05^^<http://www.w3.org/2001/XMLSchema#date> |
| type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
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