Casing made of organic matrix composite material that facilitates the discharge of smoke
A gas turbine casing made of organic matrix composite material includes reinforcement densified by an organic matrix defines an inside volume. On its inside face the casing has a structural part with a first face facing the inside face of the casing, and an opposite second face defining a flow passage portion. Recesses opening out into the inside volume of the casing are present between the inside face of the casing and the first face of the structural part facing the inside face of the casing. In the event of a fire, the recesses allow gas coming from degradation of the resin of the casing to be discharged into the flow passage.
1. A gas turbine casing made of organic matrix composite material comprising reinforcement densified by an organic matrix, said casing defining an inside volume having on its inside face a structural part having a first face facing the inside face of the casing and an opposite second face defining a portion of a flow passage, wherein the first face of the structural part facing the inside face of the casing includes grooves defining a flow path between the inside face of the casing and the first face of the structural part, the flow path extending directly or indirectly into the inside volume of the casing, and wherein said grooves extend at least in an axial direction of the casing and extend to at least at one axial end of the structural part.
2. A casing according to claim 1 wherein the grooves stop before axial ends of the structural part, the grooves including perforations in the second face of the structural part.
3. A casing according to claim 1 , wherein first grooves extend in the axial direction of the casing, and wherein second grooves extend perpendicularly to the first grooves.
4. A casing according to claim 1 wherein the inside face of the casing includes grooves that extend beyond the structural part.
5. A gas turbine aeroengine having a gas turbine casing according to claim 1 .
6. An aircraft including one or more engines, each engine having a gas turbine casing according to claim 1 .
7. A gas turbine casing made of organic matrix composite material comprising reinforcement densified by an organic matrix, said casing defining an inside volume having on its inside face a structural part having a first face facing the inside face of the casing and an opposite second face defining a portion of a flow passage, wherein the first face of the structural part facing the inside face of the casing includes grooves defining a flow path between the inside face of the casing and the first face of the structural part, the flow path extending directly or indirectly into the inside volume of the casing, and wherein said grooves extend at least in an axial direction of the casing wherein the structural part comprises a cellular structure facing the inside face of the casing.
8. A casing according to claim 7 , wherein the grooves comprise gutters.
9. A casing according to claim 7 wherein the structural part further includes an abradable coating layer.