http://rdf.ncbi.nlm.nih.gov/pubchem/patent/DE-102012005642-A1
Outgoing Links
Predicate | Object |
---|---|
assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_3f4358c6db4647ada8d761bbe05cf55a http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_5c0b0cbaae4d1618ecb89864d2c3020a |
classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C1-12 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64C1-1461 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64F5-10 |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64F5-00 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C1-00 |
filingDate | 2012-03-22-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationDate | 2013-09-26-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber | DE-102012005642-A1 |
titleOfInvention | Method for producing an aircraft fuselage section |
abstract | The invention relates to a method for producing an aircraft fuselage section (1) having an exit opening (2), wherein in the finished state an outer skin segment (3), a Doubler segment (4) reinforcing at least the edge of the exit opening (2) and a frame segment (5) are rented together, wherein in a first process step, the three segments (3, 4, 5) are made at least as a semi-finished separately, wherein in a second process step, the three segments (3, 4, 5) are aligned with each other in a third method step, the three aligned segments (3, 4, 5) are stapled together and wherein in a fourth method step, the three segments (3, 4, 5) are finally riveted together. |
isCitedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/patent/CN-105667831-A |
priorityDate | 2012-03-22-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 121.