Device for injecting cooling air into a turbine rotor
AssigneeSnecma Moteurs
InventorDidier Mortgat
Life of this patent
Estimating the term…
Abstract
A device for injecting cooling air into a turbo-machine turbine rotor includes a plurality of injectors distributed regularly around a longitudinal axis of the turbomachine and mounted between an inner shroud and an outer shroud. Each injector has a bimetallic structure with a first metal material forming a major portion of the structure of the injector and having a first coefficient of thermal expansion, and a second metal material forming a complementary portion of the structure in the vicinity of the suction side wall meeting the trailing edge of the injector, and having a second coefficient of thermal expansion that is smaller than the first.
Claims20
A device for injecting cooling air into a turbomachine turbine rotor, the device comprising a plurality of injectors distributed regularly around a longitudinal axis of the turbomachine and mounted between an inner shroud and an outer shroud, each injector of aerodynamic profile comprising, between a leading edge and a trailing edge, a suction side wall and a pressure side wall, the cooling air passing through the injectors being ejected towards through orifices in the turbine rotor via a flow section forming an aerodynamic throat between the trailing edge of one injector and the suction side wall of an immediately adjacent injector, wherein, in order to modify the section of the aerodynamic throat as a function of the temperature of the cooling air passing through the injectors, each injector comprises a bimetallic structure with a first metal material forming a major portion of the structure of the injector and having a first coefficient of thermal expansion, and a second metal material forming a complementary portion of the structure in the vicinity of the suction side wall meeting the trailing edge of the injector, and having a second coefficient of thermal expansion that is smaller than the first wherein a leading edge portion of the bimetallic structure is free of said second material.
A device for injecting cooling air into a turbomachine turbine rotor comprising:
- a plurality of injectors distributed regularly around a longitudinal axis of the turbomachine and mounted between an inner shroud and an outer shroud, each injector of aerodynamic profile including, between a leading edge and a trailing edge,
- a suction side wall, and
- a pressure side wall,
- the cooling air passing through the injectors being ejected towards through orifices in the turbine rotor via a flow section forming an aerodynamic throat between the trailing edge of one injector and the suction side wall of an immediately adjacent injector,
- wherein each injector comprises,
- a leading edge portion including a first metal material having a first coefficient of thermal expansion, and
- a trailing edge portion including the first material and a second metal material forming a complementary portion on a suction side of the injector, said second material having a second coefficient of thermal expansion that is smaller than the first,
- wherein said leading edge portion is free of said second metal material.
A method for making an injector for a cooling injection device comprising:
- joining a first material with a second material to form a bimetallic structure, said first material having a first second coefficient of thermal expansion, said second material having a second coefficient of thermal expansion that is smaller than the first;
- forming an injector from the bimetallic structure, said injector having,
- a leading edge portion including the first metal material, and
- a trailing edge portion including the first material and the second metal material, the second material forming a complementary portion on a suction side of the injector,
- wherein said leading edge portion is free of said second metal material.
Dependencies are inferred from the claim text.