Cooling arrangement
First Claim
1. An aerofoil for a gas turbine engine comprising:
- a pressure wall and a suction wall, together defining leading and trailing edges and a passage into which is supplied a cooling fluid, at least one wall of the pressure wall and suction wall having an interior surface and exterior surface, and defining an array of cooling holes to allow the cooling fluid to flow from the interior surface to the exterior surface, the array of holes defining a first group and a second group, the holes of the first group are angled to intersect the holes of the second group, wherein the holes of at least one of the groups include two or more holes positioned at different angles to one another to vary a porosity of the at least one wall dependent on a varying temperature profile.
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Accused Products
Abstract
An aerofoil for a gas turbine engine comprising a pressure wall and a suction wall and defining leading and trailing edges, the walls define a passage into which is supplied a cooling fluid, an array of cooling holes is provided through at least one of the walls to allow the cooling fluid to flow from an interior surface to an exterior surface. The array of holes comprise two groups, the holes of each group are angled to intersect the holes of the other group and are characterized in that the holes of at least one of the groups comprises two or more holes at different angles to one another to vary the porosity of the wall to account for otherwise varying wall temperatures. This arrangement also allows either less coolant mass flow to maintain a constant metal temperature, or a lower metal temperature for a given coolant mass flow.
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Citations
11 Claims
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1. An aerofoil for a gas turbine engine comprising:
a pressure wall and a suction wall, together defining leading and trailing edges and a passage into which is supplied a cooling fluid, at least one wall of the pressure wall and suction wall having an interior surface and exterior surface, and defining an array of cooling holes to allow the cooling fluid to flow from the interior surface to the exterior surface, the array of holes defining a first group and a second group, the holes of the first group are angled to intersect the holes of the second group, wherein the holes of at least one of the groups include two or more holes positioned at different angles to one another to vary a porosity of the at least one wall dependent on a varying temperature profile. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11)
Specification