Split disk blade support

Fluid reaction surfaces (i.e. – impellers) – Specific working member mount – Blade held between separable surfaces

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Details

416220R, 416219R, F01D 514

Patent

active

054860954

ABSTRACT:
A blade support includes first and second abutting disks, with the first disk having a plurality of axial dovetail slots at one end thereof, and a circumferential dovetail first half-slot at an opposite end thereof, with the second disk having a circumferential dovetail second half-slot therein. A plurality of rotor blades have axial dovetails disposed in respective ones of the axial dovetail slots, and circumferential dovetails disposed in part in each of the first and second half-slots. The first and second disks are retained together so that the first and second half-slots collectively support the circumferential dovetails.

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patent: 5310317 (1994-05-01), Bailey et al.
Garrett Engine Division, "Cast-Hollow Fan Blade Technology," USAF Report WL-TR-91-2006, Dec. 1990, pp.: Cover, Title, iii, V, I, 25, 27, 28, and 29.

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