http://rdf.ncbi.nlm.nih.gov/pubchem/patent/RU-2009139325-A

Outgoing Links

Predicate Object
classificationCPCAdditional http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2250-42
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F05D2230-80
classificationCPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/F02K1-72
http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/B64D29-08
classificationIPCInventive http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/F02K1-72
filingDate 2008-02-20-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationDate 2011-05-10-04:00^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber RU-2009139325-A
titleOfInvention TURBLE REVERSE FOR TURBOJET ENGINE
abstract 1. Reverser (9) thrust for the nacelle (1) aircraft engine, containing:! a frontal frame (11) designed to be installed downstream of the casing (15) of the compressor of a bypass turbojet engine (3) placed in the nacelle (1); ! a hood (21) movable between a closed position, in which it hides the frontal frame (11), an open position, in which it exposes the frontal frame (11), and a preliminary maintenance position, in which it is located downstream of the frontal frame (eleven); ! means (26) for moving the hood (21) between the specified closed and open positions; ! internal structure (23), installed with the ability to move between the working position, in which it is partially hidden by the frontal frame (11) and, in turn, itself hides part of the turbojet engine (3), forming an annular path (25) of cold air together with the hood (21) and the preliminary maintenance position in which it is located downstream of the frontal frame (11),! characterized in that the hood (21) consists of two flaps (21a, 21b), and the inner structure (23) consists of two inner flaps (23a, 23b), moreover, the flaps (21a, 21b) and the inner flaps (23a, 23b) are made with the possibility of opening outward when the hood (21) and the inner structure (23) are in a preliminary maintenance position. ! 2. Reversing device (9) according to claim 1, characterized in that the flaps (21a, 21b) are movable between open and closed positions along the first rails (29) attached to the inner flaps (23a, 23b). ! 3. Reverse device (9) according to claim 1, characterized in that the inner flaps (23a, 23b) have aprons (27) allowing the inner flaps (23a, 23b) to open
priorityDate 2007-04-04-04:00^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

Incoming Links

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Total number of triples: 16.