US2013052036A1PendingUtilityA1
Pin-fin array
Est. expiryAug 30, 2031(~5.1 yrs left)· nominal 20-yr term from priority
Inventors:Aaron Ezekiel Smith
F05D 2240/304F01D 5/188F05D 2260/2214F05D 2260/2212
37
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Claims
Abstract
The present application provides an airfoil with a cooling flow therein. The airfoil may include an internal cooling passage, a number of cooling holes in communication with the internal cooling passage, and a number of pin-fins positioned within the internal cooling passage. The pin-fins are arranged with one or more turning openings and one or more guiding openings so as to direct the cooling flow towards the cooling holes.
Claims
exact text as granted — not AI-modified1 . An airfoil with a cooling flow therein, comprising:
an internal cooling passage; a plurality of cooling holes in communication with the internal cooling passage; and a plurality of pin-fins positioned within the internal cooling passage; the plurality of pin-fins comprising one or more turning openings and one or more guiding openings so as to direct the cooling flow towards the plurality of cooling holes.
2 . The airfoil of claim 1 , wherein the plurality of pin-fins comprises a non-uniform array.
3 . The airfoil of claim 1 , further comprising a plurality of internal cooling passages.
4 . The airfoil of claim 1 , wherein the plurality of pin-fins comprises a staggered positioning across a pair of columns.
5 . The airfoil of claim 4 , wherein the plurality of pin-fins comprises a staggered positioning across a plurality of columns.
6 . The airfoil of claim 1 , wherein the one or more turning openings comprise a first distance between a first pair of the plurality of pin-fins, the one or more guiding openings comprise a second distance between a second pair of the plurality of pin-fins, and wherein the first distance is greater than the second distance.
7 . The airfoil of claim 1 , wherein the one or more turning openings turn the cooling flow about ninety (90) degrees.
8 . The airfoil of claim 1 , wherein the plurality of cooling holes comprises a plurality of trailing edge cooling holes.
9 . The airfoil of claim 1 , further comprising a plurality of turning openings over a plurality of columns.
10 . The air foil of claim 1 , further comprising a plurality of guiding openings over a plurality of columns.
11 . An airfoil with a cooling flow therein, comprising:
an internal cooling passage; a plurality of cooling holes in communication with the internal cooling passage; and a plurality of pin-fins positioned within the internal cooling passage in a non-uniform array; the plurality of pin-fins comprising one or more turning openings and one or more guiding openings in a staggered positioning so as to direct the cooling flow towards the plurality of cooling holes.
12 . The airfoil of claim 11 , wherein the one or more turning openings comprise a first distance between a first pair of the plurality of pin-fins, the one or more guiding openings comprise a second distance between a second pair of the plurality of pin-fins, and wherein the first distance is greater than the second distance.
13 . The airfoil of claim 11 , wherein the one or more turning openings turn the cooling flow about ninety (90) degrees.
14 . The airfoil of claim 11 , wherein the plurality of cooling holes comprises a plurality of trailing edge cooling holes.
15 . The airfoil of claim 11 , further comprising a plurality of turning openings over a plurality of columns.
16 . The air foil of claim 11 , further comprising a plurality of guiding openings over a plurality of columns.
17 . An internal cooling passage with a cooling flow therein, comprising:
a plurality of cooling holes; and a plurality of pin-fins positioned within the internal cooling passage; the plurality of pin-fins comprising one or more turning openings with a first distance between a first pair of the plurality of pin-fins, one or more guiding openings with a second distance between a second pair of the plurality of pin-fins, and wherein the first distance is greater than the second distance.
18 . The internal cooling passage of claim 17 , wherein the plurality of pin-fins comprises a non-uniform array.
19 . The internal cooling passage of claim 17 , wherein the one or more turning openings turn the cooling flow about ninety (90) degrees.
20 . The internal cooling passage of claim 17 , further comprising a plurality of turning openings over a plurality of columns.Join the waitlist — get patent alerts
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