Turbine rotor

Fluid reaction surfaces (i.e. – impellers) – Support mounting – carrier or fairing structure

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Details

416241A, 416241B, F01D 508

Patent

active

042795753

ABSTRACT:
A machined-to-size superalloy turbine rotor disc for a gas turbine engine has its fatigue life increased by coating its fatigue-prone machined surfaces with an air-impervious protective layer of material which retains its integrity and adherence to the machined surfaces for a large number of mechanical and heat stress cycles.

REFERENCES:
patent: 1504736 (1924-08-01), Brown
patent: 2709569 (1955-05-01), Roush
patent: 3144349 (1964-08-01), Swingler et al.
patent: 3262674 (1966-07-01), Huebner, Jr. et al.
patent: 3373485 (1968-03-01), Nelsen
patent: 3664766 (1972-05-01), Rahnke
patent: 3748110 (1973-07-01), Hodshire et al.
patent: 3973875 (1976-08-01), Bird
patent: 4141127 (1979-02-01), Cretella et al.
Modern Plastics, Jun., 1946, pp. 134-135, "A New Industrial Resin".
Product Engineering, vol. 44, No. 5, May, 1973, pp. 20-23, "Power Spray Coatings".
Steel, Jan. 24, 1949, pp. 59-82, "High-Temperature Ceramic Coatings".
Mechanical Engineering, vol. 87, No. 3, Mar., 1975, pp. 52-57, "Protective Coatings for Turbine Parts".

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