Gas turbine moving blade steam cooling system

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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Details

F01D 25/12 (2006.01) F01D 5/18 (2006.01) F01D 11/00 (2006.01)

Patent

CA 2242650

A gas turbine moving blade steam cooling system is disclosed wherein leakage of steam for cooling a moving blade is prevented and thermal stress at a blade root end portion is mitigated. Each end portion of a blade root portion 3 of a moving blade 1 is projected to form a projection portion 4a, 4b. A steam passage 5 is provided between the projection portions 4a, 4b and a steam supply port 5a and a steam recovery port 5b are provided downwardly to the steam passage 5. The steam supply port 5a connects to a steam supply passage 20 and the steam recovery port 5b connects to a steam recovery passage 21. Steam is supplied from the steam supply port 5a into a blade interior and is recovered through the steam recovery port 5b. Side surface seal plates 6, 7 and 8 are provided for a secure prevention of steam leakage. The steam cools the moving blade 1 and can be recovered without leakage and stress concentration due to heat at the projection portions 4a, 4b of the blade root end portion is mitigated.

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