Multiple rotor disk assembly

Fluid reaction surfaces (i.e. – impellers) – Specific working member mount – Turbo machine

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416210A, 416213R, 416219R, 416220R, B63H 120, B63H 500

Patent

active

051978571

ABSTRACT:
A rotor assembly for supporting rotor blades includes a plurality of axially adjoining discrete disks each having a rim, web, and hub. The rims include axial dovetail grooves for collectively supporting a respective blade dovetail therein. Each of the disks includes at least one axially extending annular arm joined integrally with the disk and fixedly joined to an adjacent one of the arms. The disks are fixedly joined together solely by the blade dovetails in the rim dovetail grooves and by the arms so that upon a crack failure of one of the disks, centrifugal load from the failed disk is transferred to an adjacent disk.

REFERENCES:
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patent: 3356339 (1967-12-01), Thomas et al.
patent: 4062638 (1977-12-01), Hall, Jr.
patent: 4097194 (1978-06-01), Barack et al.
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patent: 4310286 (1982-01-01), Peters et al.
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patent: 4784572 (1988-11-01), Wovotny et al.
patent: 5062769 (1991-11-01), Ortolano
D. J. Nicholas, "The Wide-Chord Fan Blade-A Rolls-Royce First", Paper presented 15-19 Jun. 1987 (NTIS Order No. N88-10789), Title sheet and page containing FIG. 9b.
Intervia Aerospace Review, "Civil Engine Wars," Feb. 1991, pp. 11 & 12.
Flight International, figure on p. 1473, Dec. 3, 1983.

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