| 8959926 |
Gas turbine high pressure compressor fluid return and reinjection including an annular air bleeding manifold |
Michel Gilbert Roland Brault |
2015-02-24 |
| 8800291 |
Bleeding of air via the diffuser of a centrifugal compressor of a turbine engine |
Jean-Francois Rios, Delphine Roussin-Leroux |
2014-08-12 |
| 7785066 |
Bleed system for a low-pressure compressor of a turbomachine |
Gilles Alain Charier, Philippe Jacques Pierre Fessou, Patrick Morel |
2010-08-31 |
| 7618232 |
Compressor comprising a plurality of cells reconstituting an annular volume of separation of flows in a turbine engine |
Gilles Alain Charier |
2009-11-17 |
| 7399163 |
Rotor blade for a compressor or a gas turbine |
Chantal Giot, Thomas Schlesinger |
2008-07-15 |
| 7214034 |
Control of leak zone under blade platform |
Chantal Giot, Marc Marchi, Christian Gosselin |
2007-05-08 |
| 6457935 |
System for ventilating a pair of juxtaposed vane platforms |
Serge Louis Antunes, Isabelle Bourriaud, Maurice Guy Judet |
2002-10-01 |
| 6328531 |
Cooled turbine blade |
Christian Bariaud |
2001-12-11 |
| 6163959 |
Method of reducing the gap between a liner and a turbine distributor of a turbojet engine |
Anne-Marie Arraitz, Michel Gerard Paul Hacault, Laurent Philippe Yves Leray, Michel Jean Loubet, Marc Marchi +4 more |
2000-12-26 |
| 5997247 |
Seal of stacked thin slabs that slide within reception slots |
Anne-Marie Arraitz, Michel Gerard Paul Hacault, Laurent Philippe Yves Leray, Marc Marchi, Didier Mortgat |
1999-12-07 |