Cooling circuits for a turbomachine moving blade
View Patent ↗A moving blade for a turbomachine, the central portion of the blade including a pressure-side cooling circuit and a suction-side cooling circuit. The pressure-side circuit comprises at least first and second pressure-side cavities extending from the pressure side of the blade to a central wall, a central cavity extending from the pressure side to the suction side of the blade, and outlet orifices opening out from the central cavity and into the pressure-side face of the blade. The suction-side circuit comprises at least first and second suction-side cavities extending radially from the suction side of the blade to the central wall, a central cavity extending across the blade from the pressure side to the suction side, and outlet orifices opening out from the central cavity and into the pressure-side face of the blade.
1. A moving blade for a turbomachine, the blade being characterized in that its central portion (C) includes a pressure-side cooling circuit and a suction-side cooling circuit,
said pressure-side cooling circuit comprising:
at least first and second pressure-side cavities extending radially and in the thickness direction of the blade from the pressure side of the blade to a central wall extending radially and along the skeleton direction of the blade;
a central cavity extending radially and in the thickness direction of the blade from the pressure side to the suction side of the blade;
an air admission opening at one radial end of the first pressure-side cavity for feeding the pressure-side circuit with air;
a first passage causing the other radial end of the first pressure-side cavity to communicate with a neighboring radial end of the second pressure-side cavity;
a second passage causing the other radial end of the second pressure-side cavity to communicate with a neighboring radial end of the central cavity; and
outlet orifices opening out from the central cavity and into a pressure-side face of the blade;
the suction-side cooling circuit comprising:
at least first and second suction-side cavities extending radially and in the thickness direction of the blade from the suction side of the blade to said central wall;
a central cavity extending radially and in the thickness direction of the blade from the pressure side to the suction side of the blade;
an air admission opening at one radial end of the first suction-side cavity to feed the suction-side circuit with air;
a first passage causing the other radial end of the first suction-side cavity to communicate with a neighboring radial end of the second suction-side cavity;
a second passage causing the other radial end of the second suction-side cavity to communicate with a neighboring radial end of the central cavity; and
outlet orifices opening out from the central cavity and into the pressure-side face of the blade.
2. A blade according to claim 1 , further including a leading edge cooling circuit comprising at least one cavity extending radially in the vicinity of the leading edge of the blade, at least one air admission orifice opening out into the leading edge cavity, and outlet orifices opening out from said leading edge cavity and into the leading edge of the blade.
3. A blade according to claim 2 , in which the air admission orifice is an opening situated at the radial end of the leading edge cavity.
4. A blade according to claim 2 , in which the leading edge cooling circuit includes a plurality of air admission orifices opening out from the central cavity of the pressure-side cooling circuit and into the leading edge cavity.
5. A blade according to claim 2 , in which the leading edge cooling circuit further includes a central cavity extending radially and in the thickness direction of the blade from the pressure side to the suction side of the blade, an opening at one radial end of the central cavity for feeding the circuit with air, and a plurality of air admission orifices opening out from the central cavity and into the leading edge cavity.
6. A blade according to any one of claims 1 to 5 , further including a trailing edge cooling circuit comprising at least one cavity extending radially in the vicinity of the trailing edge of the blade, at least one air admission orifice opening out into the trailing edge cavity, and air outlet orifices opening out from the trailing edge cavity and into the pressure-side face of the blade.
7. A blade according to claim 6 , in which the air admission orifice is a opening situated at the radial end of the trailing edge cavity.
8. A blade according to claim 6 , in which the trailing edge cooling circuit includes a plurality of air admission orifices opening out from the central cavity of the suction-side cooling circuit and into the trailing edge cavity.
9. A blade according to claim 6 , in which the trailing edge cooling circuit further includes a central cavity extending radially and across the blade from the pressure side to the suction side of the blade, an opening at a radial end of the central cavity for feeding the circuit with air, and a plurality of air admission orifices opening out from said central cavity and into the trailing edge cavity.
10. A blade according to claim 1 , in which the internal walls of the cavities of the pressure-side and suction-side cooling circuits are provided with flow disturbers for increasing heat transfer along said walls.