Turbine nozzle segment

Details Turbine nozzle segment Turbine nozzle segment

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 25/12 (2006.01) F01D 9/02 (2006.01)

Patent

CA 2647754

A turbine nozzle segment (118) includes a band (120,122) having a flowpath side (124,128) and a non-flowpath side (126,130) and an enclosure (142) disposed on the non-flowpath side (126,130) of the band (120,122). A plenum (144) may be defined between the band (120,122) and the enclosure (142) and a discourager (166) may extend from the enclosure (142).

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