http://rdf.ncbi.nlm.nih.gov/pubchem/patent/FR-2658248-A1
Outgoing Links
Predicate | Object |
---|---|
assignee | http://rdf.ncbi.nlm.nih.gov/pubchem/patentassignee/MD5_ee75c11ff8c42daff3db154886acbaba |
classificationCPCAdditional | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y10T137-0536 http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/Y02T50-60 |
classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02C7-042 |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02C7-042 http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K7-16 |
filingDate | 1991-01-29-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
inventor | http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_5debd8f344e344eca3a9eb031d2ee709 |
publicationDate | 1991-08-16-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber | FR-2658248-A1 |
titleOfInvention | GAS-STATOREACTOR TURBINE ENGINE ASSEMBLY HAVING A VARIABLE AIR INLET |
abstract | a) Gas turbine engine-ramjet assembly comprising a variable air inlet, b) characterized by: - an air duct (2) communicating with the air inlet, which widens in the form of a tubular channel directed axially towards the base turbojet, widening towards an annular supply (4) of the air channel at dynamic pressure (5), - the closure means are provided at least on the inlet side to quadrangular segments (3, 8) of the tubular channel, - the means for closing off the supply (4) are constituted by an annular slide (16) movable axially and capable of being traversed by the flow, and at at least one flap (17) capable of tilting against a partial entry (T1) of the power supply (4), and among these the drawer (16) closes like a cover, in the power supply in the common position , released. c) The invention relates to a gas turbine engine-ramjet assembly comprising a variable air inlet. |
priorityDate | 1990-02-13-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Total number of triples: 193.