초록 ▼

The invention relates to a device for ventilating a high pressure turbine rotor which comprises a turbine disk and an upstream end plate. A first circuit for cooling blades delivers a first air flow via main injectors and holes formed in the end plate. A second cooling circuit delivers a second air

The invention relates to a device for ventilating a high pressure turbine rotor which comprises a turbine disk and an upstream end plate. A first circuit for cooling blades delivers a first air flow via main injectors and holes formed in the end plate. A second cooling circuit delivers a second air flow through a discharge baffle situated downstream from the compressor, a fraction of this second flow serving to cool the upstream top face of the end plate through a second baffle situated beneath the main injectors. A branch connection is provided between the first circuit and the enclosure situated downstream from the second baffle and it delivers a third flow which is set into pre-rotation by additional injector means formed in the form of inclined bores.

대표청구항 ▼

1. A ventilation device for a high pressure turbine rotor of a turbomachine, said turbine being disposed downstream from the combustion chamber and comprising firstly a turbine disk presenting an internal aperture and an upstream flange for fixing to the downstream cone of a high pressure compressor

1. A ventilation device for a high pressure turbine rotor of a turbomachine, said turbine being disposed downstream from the combustion chamber and comprising firstly a turbine disk presenting an internal aperture and an upstream flange for fixing to the downstream cone of a high pressure compressor, and secondly an end plate disposed upstream from said disk and separated therefrom by a cavity, said end plate comprising a solid radially inner portion likewise having an internal aperture, through which the upstream flange of said disk extends, and an upstream flange for being fixed to said downstream cone, said device comprising a first circuit for cooling blades fed with a first flow of air taken from the end of the combustion chamber and delivering said first flow of air into said cavity via main injectors disposed upstream from said end plate, and ventilation holes formed through said end plate, and a second circuit for cooling the end plate fed with a second flow of air through a discharge baffle situated downstream from the high pressure compressor, at least a fraction of said second air flow serving to ventilate the upstream top face of said end plate through a second baffle situated beneath the injectors,the device further comprising a branch connection between the first circuit and the enclosure situated downstream from the second baffle, said branch connection delivering a third flow of air for cooling the upstream top face of the radially inner portion of said end plate, said third flow of air being entrained into pre-rotation by means of additional injectors. 2. A device according to claim 1, wherein the additional injectors are implemented in the form of bores that are inclined tangentially in the direction of rotation of the rotor. 3. A device according to claim 2, wherein said bores take air from inside the main injectors. 4. A device according to claim 3, wherein said bores deliver air immediately downstream from the second baffle. 5. A device according to claim 2, wherein the second baffle is disposed between the main injectors and the upstream flange of the end plate. 6. A device according to claim 5, wherein the upstream flange of the end plate is radial.