Accession Number : ADD009195

Title :   Hydrogen Cooled Turbine.

Descriptive Note : Patent,

Corporate Author : DEPARTMENT OF THE AIR FORCE WASHINGTON DC

Personal Author(s) : Pinaire,Lonnie W

Report Date : 26 Jan 1982

Pagination or Media Count : 6

Abstract : A bladed rotor for a turbine having a rotor disk and a plurality of blades. The blades contain a plurality of passages therein for circulating a hydrogen coolant in order to cool the blade. In order to prevent leakage of the hydrogen the blade is electron welded onto the rotor disk. (Author)

Descriptors :   *Patents, *Gas turbine rotors, *Gas turbine blades, *Cooling, *Hydrogen, Gas turbines, Coolants, Disks, Electron beam welding, Leakage(Fluid), Inventions

Subject Categories : Air Condition, Heating, Lighting & Ventilating
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE