| Predicate |
Object |
| assignee |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_41bd05f41941dcc8a5f485ce83681d9a
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_b5feca2b5ecb229b3f4f3eea6bc25a54
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_10b682b6151873459771fc6ca55a80b1
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_10efc646a4dd605c2f09c493718f5b81
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_b46b6eb983e3f0b927fb6cbc35eee979
http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_c6c2e9aab8e4e160be6b096126471cc8 |
| classificationIPCInventive |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C39-08
http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/B64C31-00 |
| filingDate |
2009-01-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| grantDate |
2010-06-20-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| inventor |
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5f115823c269435f180bc53ef853b7f0
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_adf9733dcc7b8d87d67d19785b237ba7
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_cc16904cb280e0577bf45e9138650ba1
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_98f53988c4a6afe0afb99378e78ee815
http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_73024d6517e982866761e9ff8b5e33d2 |
| publicationDate |
2010-06-20-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| publicationNumber |
RU-2392188-C1 |
| titleOfInvention |
Method of deployment and altitude suspension of data system and carrier aircraft to this end |
| abstract |
FIELD: transport. ^ SUBSTANCE: proposed is the method of deployment and altitude suspension of data system comprising carrier aircraft (CA) with data acquisition, processing and transmission hardware and base servicing module connected therewith by steel rope system. Carrier aircraft is placed in stable wind flow of atmosphere tropo pause zone and kept therein by means of aircraft control surfaces and steel rope relative to earth surface. Placing aircraft to operating altitude is performed by midair towing exploiting aerodynamic properties of aircraft while descent and landing after completed flight program (or in the case of failures) is effected by controlled gliding after unlatching the towing rope. Carrier aircraft represents hydride airplane "glider - kite" that features "duck" aerodynamic profile with high aerodynamic characteristics and low specific load onto wing. ^ EFFECT: longer continuous flight and higher stability, reduced costs. ^ 6 cl, 6 dwg |
| isCitedBy |
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2715420-C1
http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2749249-C2 |
| priorityDate |
2009-01-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
| type |
http://data.epo.org/linked-data/def/patent/Publication |