TY  - JOUR
AB  - Materials have been developed in recent years which are particularly well‐suited for use in fabricated gas turbine hot section components. Among these are HAYNES® alloy No. 230 and HASTELLOY® alloy S. These alloys combine very good performance characteristics with capability for fabrication into such complex components as combustion chambers, afterburner flame‐holders, seal rings, and thermocouple/probe assemblies. The properties and fabrication characteristics of these two materials are reviewed and compared with other well‐known gas turbine alloys.
VL  - 62
IS  - 5
SN  - 0002-2667
DO  - 10.1108/eb036935
UR  - https://doi.org/10.1108/eb036935
AU  - Rothman M.F.
AU  - Patriarca C.R.
PY  - 1990
Y1  - 1990/01/01
TI  - New Materials for Fabricated Gas Turbine Hot Section Components
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 2
EP  - 7
Y2  - 2024/09/23
ER  -