9 Patents
- 0 cites
- US119134052024Turbine Engine with a Flow Splitter Having a Profile with Inclined Serrations
Safran Aircraft Engines
0 cites - 0 cites
- 0 cites
- US117325882023Profiled Structure for an Aircraft or Turbomachine for an Aircraft
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
0 cites - US116681962023Profiled Structure for an Aircraft or Turbomachine
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
0 cites - US116296642023Turbine Engine with a Flow Splitter Having a Profile with Inclined Serrations
Safran Aircraft Engines
0 cites - 0 cites
- US115607962023Profiled Structure for an Aircraft or Turbomachine for an Aircraft
OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES
0 cites