Inventors list |
Assignees list |
Classification tree browser |
Top 100 Inventors |
Top 100 Assignees |
Patrice Andre Commaret, Rubelles FR
Patrice Andre Commaret, Rubelles FR
| Patent application number | Description | Published |
|---|---|---|
| 20080245053 | GAS TURBINE ENGINE DIFFUSER AND COMBUSTION CHAMBER AND GAS TURBINE ENGINE COMPRISING SAME - The present invention relates to a gas turbine engine diffuser ( | 10-09-2008 |
| 20090019856 | CHAMBER-BOTTOM BAFFLE, COMBUSTION CHAMBER COMPRISING SAME AND GAS TURBINE ENGINE FITTED THEREWITH - The present invention relates to a baffle ( | 01-22-2009 |
| 20090047127 | TURBOMACHINE DIFFUSER - A turbomachine comprising: | 02-19-2009 |
| 20090056337 | TURBOMACHINE WITH ANNULAR COMBUSTION CHAMBER - Turbomachine with an annular combustion chamber ( | 03-05-2009 |
| 20090100839 | COMBUSTION CHAMBER WALL WITH OPTIMIZED DILUTION AND COOLING, AND COMBUSTION CHAMBER AND TURBOMACHINE BOTH PROVIDED THEREWITH - The invention applies to the field of turbomachines and relates to a combustion chamber in which the supply of dilution air and cooling air is optimized. The invention is concerned more particularly with optimizing the position of the dilution holes present on the walls of the combustion chamber. | 04-23-2009 |
| 20090100840 | COMBUSTION CHAMBER WITH OPTIMISED DILUTION AND TURBOMACHINE PROVIDED WITH SAME - The invention relates to the field of turbomachines and concerns a combustion chamber ( | 04-23-2009 |
| 20100043449 | DEVICE FOR ATTACHING A COMBUSTION CHAMBER - Turbomachine comprising an annular combustion chamber ( | 02-25-2010 |
| 20110056207 | DIFFUSER FOR TURBINE ENGINE INCLUDING INDENTED ANNULAR WEBS - A diffuser for a turbine engine that includes two annular webs extending inside one another and connected between them by substantially radial vanes, wherein the downstream peripheral edge of at least one of the webs includes indentions evenly distributed about the longitudinal axis of the diffuser. | 03-10-2011 |
| 20110088402 | ANNULAR COMBUSTION CHAMBER FOR A GAS TURBINE ENGINE - An annular combustion chamber for a gas turbine engine includes radially inner and outer walls connected together by a chamber end wall including openings, each of which receives a fuel injection system. Heat protection deflectors are fastened to the chamber end wall. Holes are formed through the chamber end wall to pass cooling air onto an upstream face of each deflector. The inner or outer edge of a deflector presents a sealing rim engaging the respective inner or outer wall of the chamber. | 04-21-2011 |