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US3689177A Expired / Lapsed US ⏱️ 0.0 years remaining

Blade constraining structure

Assignee: General Electric Co
•
Filing: 1971-04-19
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Granted: 1972-09-05
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Expires: 1991-04-19
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Abstract

Abstract In an axial flow apparatus including stator and rotor elements, means are included for constraining axial movement of individual blade members relative to the rotor axis when the rotor is subjected to high centrifugal loading. The constraining means include a ring which is circumferentially expandable under centrifugal loading. Part of the outward radial force causing the expansion of the ring is directed axially against the blade members to provide an axially constraining force which is proportional to the centrifugal loading on the rotor. The invention herein described was made in the course of or under a contract or subcontract thereunder, (or grant) with the Department of the Army.

Inventors

  • 👤 David Dubble Klassen

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-04 20:39
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/02; F01D5/06; F01D11/00; F01D11/005; F01D11/006; F01D5/12; F01D5/22; F01D5/24; F01D5/30; F01D5/3007

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 260 words
In an axial flow apparatus having stator and rotor elements, a blade constraining structure comprising: a first rotor element having axially opposed faces and a plurality of open-ended generally radial slots extending from one face to the other, with each slot having side walls which are undercut to provide inwardly directed abutment faces; a second rotor member axially spaced from said first member and including an axially extending circumferential flange, the tip of which is in closely spaced opposing relation to said slots and is axially undercut to provide an inwardly directed surface; a wedge ring whose outer radial annular surface is axially overcut to provide an outwardly directed surface abutting said inwardly directed surface of said flange, such that under the influence of centrifugal loading said wedge ring circumferentially expands and said overcut surface slides over said undercut surface in both an outward radial direction and an axial direction, effecting an axial translation of said wedge ring; a plurality of blades having root portions inserted into said slots so that the forward inserted face of each root abuts said wedge ring, wherein each root is thickened to provide outwardly extending shoulders which abut the inwardly extending shoulders of said slots so as to radially retain said blades under centrifugal loading; locking means constraining the other face of each root to inhibit axial movement of said roots such that under centrifugal loading the axial translation of said wedge ring is directed against the abutting root faces and cooperates with said locking means to further restrict axial movement of said blades.
Claim 2
Dependent Claim 260 words
In an axial flow apparatus having stator and rotor elements, a blade constraining structure comprising: a first rotor element having axially opposed faces and a plurality of open-ended generally radial slots extending from one face to the other, with each slot having side walls which are undercut to provide inwardly directed abutment faces; a second rotor member axially spaced from said first member and including an axially extending circumferential flange, the tip of which is in closely spaced opposing relation to said slots and is axially undercut to provide an inwardly directed surface; a wedge ring whose outer radial annular surface is axially overcut to provide an outwardly directed surface abutting said inwardly directed surface of said flange, such that under the influence of centrifugal loading said wedge ring circumferentially expands and said overcut surface slides over said undercut surface in both an outward radial direction and an axial direction, effecting an axial translation of said wedge ring; a plurality of blades having root portions inserted into said slots so that the forward inserted face of each root abuts said wedge ring, wherein each root is thickened to provide outwardly extending shoulders which abut the inwardly extending shoulders of said slots so as to radially retain said blades under centrifugal loading; locking means constraining the other face of each root to inhibit axial movement of said roots such that under centrifugal loading the axial translation of said wedge ring is directed against the abutting root faces and cooperates with said locking means to further restrict axial movement of said blades.
Claim 3
Dependent Claim 45 words
The structure of claim 1 wherein said second rotor member includes a plurality of circumferentially spaced blades disposed about its periphery wherein said blades are radially and axially retained by means of a circumferential dovetail groove around the outer periphery of said second rotor member.
Claim 4
Dependent Claim 17 words
The structure of claim 1 wherein said wedge ring provides an air seal between the rotor elements.
Claim 5
Dependent Claim 40 words
The structure of claim 1 wherein said wedge ring is a plastic-like resilient material which allows the circumference of the ring to be expanded slightly without fracture, yet is of sufficient stiffness to resist axial cross-sectional compression without substantial deformation.
Claim 6
Dependent Claim 11 words
The structure of claim 4 wherein said wedge ring is polyimide.
Claim 7
Dependent Claim 50 words
The structure of claim 4 wherein said locking means includes a locking ring abutting the other faces of said blade roots and maintained in abutting relation by a plurality of projections axially extending from said first rotor with each projection including an inward extending radial lip overlapping said locking ring.
Claim 8
Dependent Claim 35 words
The structure of claim 6 wherein said first and second rotor members are mated by a series of axially extending interlocking male and female splines so as to prevent circumferential slippage between the rotor elements.
Claim 9
Dependent Claim 34 words
The structure of claim 7 including an annular resilient plastic ring, the outside surface of which is in abutting relation with the inside surfaces of the interlocking splines to provide an air seal therebetween.

References Cited (Backward Citations)

US2356605A Cited
US2656147A Cited
CH284188A Cited
FR1145755A Cited
US3356339A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-09-05 1976-03-06 1976-09-05 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-09-05 1980-03-06 1980-09-05 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-09-05 1984-03-06 1984-09-05 $7700.00 Window Closed / Lapsed

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