Turbojet engine rotor

Details Turbojet engine rotor Turbojet engine rotor

1993-10-14

1995-03-07

Look, Edward K.

Fluid reaction surfaces (i.e., impellers)

Specific working member mount

Blade received in well or slot

F01D 502

Patent

active

053952138

ABSTRACT:
A turbojet engine rotor, wherein the circumference of the disk is occupied y teeth and slots in an alternating form. The teeth have a variable rigidity in the axial direction, which leads to different shapes of their cross-section. The teeth have a twisted outer surface and oblique recesses are provided on the circumference of the rotor for receiving vane roots which alternate with the teeth for separating and retaining the vanes.

REFERENCES:
patent: 3661475 (1972-05-01), Anderson et al.
patent: 3891351 (1975-06-01), Norbut
patent: 4135857 (1979-01-01), Pannone et al.
patent: 5067876 (1991-11-01), Moreman

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