Issued Patents All Time
Showing 1–25 of 30 patents
| Patent # | Title | Co-Inventors | Date |
|---|---|---|---|
| 6276126 | Axisymmetric, directable and adjustable turbojet-engine exhaust nozzle | Philippe Pierre Vincent Bouiller, Gilles Alain Charier, Daniel Germain Alexis Kettler, Gerard M. F. Mandet, Jackie Raymond Julien Prouteau | 2001-08-21 |
| 6185926 | Turbojet engine thrust reverser and exhaust nozzle assembly | Michel David Ah-fa, Xavier Guyonnet | 2001-02-13 |
| 6082669 | System for the admission of air into a working section of a gas turbine engine | Thierry Bardagi | 2000-07-04 |
| 5934564 | Variable geometry turbojet engine exhaust nozzle | Philippe Pierre Vincent Bouiller, Pierre Bourquin, Jean-Pierre Ruis | 1999-08-10 |
| 5623821 | Turbojet equipped with a deicing system on the intake case | Philippe Pierre Vincent Bouiller, Claude Corbin, Michel Franchet | 1997-04-29 |
| 5593278 | Gas turbine engine rotor blading sealing device | Jean-Paul Lagrange, Gerard M. F. Mandet, Jacques H. Mouchel, Jean-Philippe Richard, Marcel R. Soligny | 1997-01-14 |
| 5566884 | Supersonic nozzle for a turbojet engine | Jean Hardy, Marcel R. Soligny | 1996-10-22 |
| 5542607 | Supersonic nozzle, in particular for a turbojet engine | Marcel R. Soligny | 1996-08-06 |
| 5520336 | Nozzle for a jet engine containing an adjustable convergent-divergent portion | Marcel R. Soligny | 1996-05-28 |
| 5421704 | Inter-blade platform for a bladed disc of a turbomachine rotor | Ollivier Carletti, Gerard F. Inizan, Francois M. P. Marlin, Philippe Pabion, Thierry Pancou +3 more | 1995-06-06 |
| 5367874 | Integral composite gas turbine afterburner structure | Didier L. C. Auffret, Gerard C. L. Berger, Eric Conete, Frederic Delage, Christophe Thorel | 1994-11-29 |
| 5359849 | Afterburner assembly for a gas turbine engine | Didier L. C. Auffret, Gerard C. L. Berger, Eric Conete, Frederic Delage, Christophe Thorel | 1994-11-01 |
| 5269138 | Variable geometry flame trap device for use in an after-burner device of a gas turbine | Eric Conete, Frédéric Paul Eichstadt | 1993-12-14 |
| 5263823 | Gas turbine engine impeller having an annular collar platform | Maurice Jean Cabaret, Christophe Jean Roger Champenois, Christophe G. J. Gourio, Gilles A. Le Rumeur, Didier Merville +2 more | 1993-11-23 |
| 5193982 | Separate inter-blade platform for a bladed rotor disk | Gerard F. Inizan, Philippe Pabion, Jean-Michel Payen, Christine J. G. Ruffier | 1993-03-16 |
| 5116218 | Segmented hot molding apparatus | Regis Raynal | 1992-05-26 |
| 5069034 | Heat protective lining for an afterburner or transition duct of a turbojet engine | Marc G. Loubet | 1991-12-03 |
| 4974638 | Transition pipe for a jet pipe assembly of a turbojet engine | Philippe M. D. Gastebois, Marc G. Loubet | 1990-12-04 |
| 4955541 | Two dimensional nozzle for a turbojet engine | Olivier Carteron | 1990-09-11 |
| 4907743 | Assembly of two bodies having distinctly different coefficients of expansion | Jean G. Bouiller, Marc G. Loubet | 1990-03-13 |
| 4817871 | Control system for turbojet engine nozzle flaps | Yves R. J. Berneuil | 1989-04-04 |
| 4805398 | Turbo-machine with device for automatically controlling the rate of flow of turbine ventilation air | Jean-Mac Payen, Georges Mazeaud | 1989-02-21 |
| 4778109 | Adjustable two dimensional nozzle for aircraft jet engines | Marc G. Loubet, Jean-Michel Payen | 1988-10-18 |
| 4716640 | Method for manufacturing a burner ring for a turbojet engine | Francois, M. B. Marlin | 1988-01-05 |
| 4679982 | Compressor blow-off arrangement | Jean G. Bouiller | 1987-07-14 |