Enhanced impingement cooled components
First Claim
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1. An improved component heat transfer assembly for use in a gas turbine engine, the assembly comprising:
- a. a component including a textured surface; and
b. impingement means spaced from the textured surface for directing an impinging fluid to directly impinge upon the textured surface; and
c. wherein the textured surface comprises an array of protuberances extending from a first surface and wherein the impingement means is spaced from the protuberances for directing an impinging fluid to directly impinge upon a plurality of the protuberances;
d. wherein the protuberances are generally semi-spherical in shape.
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Abstract
An improved heat transfer assembly includes a textured impingement surface and means for impinging cooling air directly upon the textured surface. A component includes a surface textured to increase convective heat transfer with minimal increase in resistance to conductive heat transfer through the component. The textured surface can comprise an array of closely spaced hemispherically shaped protuberances. A method is disclosed for texturing a surface with discrete laser welds.
165 Citations
5 Claims
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1. An improved component heat transfer assembly for use in a gas turbine engine, the assembly comprising:
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a. a component including a textured surface; and b. impingement means spaced from the textured surface for directing an impinging fluid to directly impinge upon the textured surface; and c. wherein the textured surface comprises an array of protuberances extending from a first surface and wherein the impingement means is spaced from the protuberances for directing an impinging fluid to directly impinge upon a plurality of the protuberances; d. wherein the protuberances are generally semi-spherical in shape.
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2. An improved component heat transfer assembly for use in a gas turbine engine, the assembly comprising:
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a. a component including a textured surface; and b. impingement means spaced from the textured surface for directing an impinging fluid to directly impinge upon the textured surface; and c. wherein the textured surface comprises an array of protuberances extending from a first surface and wherein the impingement means is spaced from the protuberance for directing an impinging fluid to directly impinge upon a plurality of the protuberances; d. wherein the protuberances are generally hemispherical in shape.
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3. An improved component heat transfer assembly for use in a gas turbine engine, the assembly comprising:
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a. a component including a textured surface; and b. impingement means spaced from the textured surface for directing an impinging fluid to directly impinge upon the textured surface; and c. wherein the textured surface comprises an array of protuberances extending from a first surface and wherein the impingement means is spaced from the protuberances for directing an impinging fluid to directly impinge upon a plurality of the protuberances; d. wherein the protuberances are generally hemispherical in shape and wherein the protuberances extend above the first surface with a height less than or equal to 0.020 inch. - View Dependent Claims (4)
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5. An improved component heat transfer assembly for use in a gas turbine engine, the assembly comprising:
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a. a component including a textured surface; and b. impingement means spaced from the textured surface for directing an impinging fluid to directly impinge upon the textured surface; and c. wherein the textured surface comprises an array of protuberances extending from a first surface and wherein the impingement means is spaced from the protuberances for directing an impinging fluid to directly impinge upon a plurality of the protuberances; d. wherein the protuberances are discrete hemispherical weld beads disposed on the first surface.
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Specification