New Alloys for Automotive Turbines

560052

01/01/1956

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
THIS paper reports on progress to date in the development of high-temperature alloys for automotive gas turbines.
Strict limitations have been set on the alloying elements in order to keep costs down — the cost factor being the main reason for this alloy search.
The materials discussed here, which meet the alloy limitations and the temperature and stress requirements, fall into three classes:
  1. 1.
    Iron-base chromium - manganese - nitrogen austenitic alloys.
  2. 2.
    Iron-aluminum ferritic alloys.
  3. 3.
    Cast ferritic alloys with up to 12% chromium and some titanium, vanadium, molybdenum, and tungsten.
Meta TagsDetails
DOI
https://doi.org/10.4271/560052
Pages
7
Citation
Frey, D., "New Alloys for Automotive Turbines," SAE Technical Paper 560052, 1956, https://doi.org/10.4271/560052.
Additional Details
Publisher
Published
Jan 1, 1956
Product Code
560052
Content Type
Technical Paper
Language
English