http://rdf.ncbi.nlm.nih.gov/pubchem/patent/BE-1025263-A1

Outgoing Links

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filingDate 2017-05-31^^<http://www.w3.org/2001/XMLSchema#date>
inventor http://rdf.ncbi.nlm.nih.gov/pubchem/patentinventor/MD5_6b80f8e73391ffbb8832d4f7e85a93a6
publicationDate 2019-01-03^^<http://www.w3.org/2001/XMLSchema#date>
publicationNumber BE-1025263-A1
titleOfInvention TURBOMACHINE DEGIVER COMPRESSOR AND DEFROSTING METHOD
abstract The invention proposes a low-pressure compressor of an aircraft turbojet engine. The compressor, also known as a booster, comprises an inlet structure defrosted by a circulation of hot pressurized fluid from the high-pressure compressor. The deicing structure (28) comprises a deformable membrane (30) traversed by the circulation of pressurized fluid (50). In the event of deposition of frost (44) on the membrane (30), the circulation of pressurized fluid (50) is blocked so that its pressure deforms the membrane so as to fracture said deposition of frost (44). The invention also relates to a compressor deicing process.
priorityDate 2017-05-31^^<http://www.w3.org/2001/XMLSchema#date>
type http://data.epo.org/linked-data/def/patent/Publication

Incoming Links

Predicate Subject
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