| Patent Number |
Title Of Patent |
Date Issued |
| 4280324 |
Fuel distribution device |
July 28, 1981 |
| The invention concerns a fuel distribution device in a high velocity gase flow. The device consists of two coaxial, toric injection manifolds placed in close proximity with respect to each other, pierced by small diameter uniformly distributed orifices and arranged to introduce fuel |
| 4246758 |
Antipollution combustion chamber |
January 27, 1981 |
| The invention concerns a combustion chamber for turbojet engines. The comtion chamber is of the annular type and consists of two coaxial flame tubes opening into a common dilution and mixing zone. The inner tube is designed for low operating ratings of the engine, the outer tube for hig |
| 4162611 |
Combustion chamber for turbo engines |
July 31, 1979 |
| A fuel injection nozzle for a turbo engine is mounted at the base of a costion chamber, either tubular or annular, by means of an intermediate inwardly flared member having openings through its sides for admitting cooling air. An annular flange structure around the intermediate member |
| 4125998 |
Device for igniting fuel injected into a rapidly flowing gaseous medium |
November 21, 1978 |
| An auxiliary chamber or ignition "prechamber" for afterburners of aeronautical turbine engines draws in, through a perforated plate, a carbureted mixture produced by fuel projected against an anvil by an injection manifold, and the injection manifold also issues a jet of fuel into a |
| 4104874 |
Double-walled combustion chamber shell having combined convective wall cooling and film cooling |
August 8, 1978 |
| A combustion chamber shell, particularly for aircraft turbojet engines, cisting of an assembly of sleeves each of which comprises two parallel facings connected and braced to each other by multiple longitudinal ribs which form an equal number of channels for the passage of the cooling a |
