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US3692429A Expired / Lapsed US ⏱️ 0.0 years remaining

Rotor structure and method of broaching the same

Assignee: Westinghouse Electric Corp
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Filing: 1971-02-01
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Granted: 1972-09-19
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Expires: 1991-02-01
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Abstract

Abstract A method of broaching an axial row of grooves for roots or rotor blades in a multi-stage, frusto-conical rotor structure by inclining the angle of reciprocation of the cutting tool of the broach relative to the periphery of the rotor structure and to the axis of rotation of the rotor. The grooves in the largest diameter land are cut to the full size of the broach, while the succeeding lands are cut with a smaller portion of the cutting tool in a diminishing manner, with the smallest diameter land having blade root grooves of smallest cross-sectional area. The resulting structure is a rotor having a plurality of increasing diameter lands, each land having an annular row of grooves, the grooves in each land axially aligned with the grooves in the adjacent lands to form a plurality of axial rows of grooves. The grooves in the smallest diameter lands have smaller grooves than those in the largest diameter lands.

Inventors

  • 👤 Arnold H Redding

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 07:59
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/30; F01D5/3007; B; B23; B23D; B23D37/00; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49316; Y10T29/4932; Y10T29/49321

Claims Analysis

Total Claims: 11
Claim 1
Independent Claim 105 words
A method of cutting grooves in a multi-stage rotor structure comprising the steps of: a. inclining the angle of attack of the cutting tool relative to the periphery of the rotor structure; b. relatively moving the cutting tool along a line forming an acute angle with respect to the axis of the rotor and into engagement with the rotor structure; and c. cutting the grooves in the rotor structure so that the end adjacent the rotor structure is cut to the full size of the cutting tool, while the succeeding portions of the rotor are cut with a corresponding smaller portion of the cutting tool.
Claim 2
Independent Claim 105 words
A method of cutting grooves in a multi-stage rotor structure comprising the steps of: a. inclining the angle of attack of the cutting tool relative to the periphery of the rotor structure; b. relatively moving the cutting tool along a line forming an acute angle with respect to the axis of the rotor and into engagement with the rotor structure; and c. cutting the grooves in the rotor structure so that the end adjacent the rotor structure is cut to the full size of the cutting tool, while the succeeding portions of the rotor are cut with a corresponding smaller portion of the cutting tool.
Claim 3
Dependent Claim 30 words
The method recited in claim 1 and further including the initial step of machining the rotor structure to form a plurality of annular gaps defined by radially extending annular lands.
Claim 4
Dependent Claim 13 words
The method recited in claim 1, wherein broaching is the method of cutting.
Claim 5
Dependent Claim 59 words
The method recited in claim 1 and further including the steps of: a. machining the rotor structure to form a plurality of annular gaps defined by radially extending lands, and b. broaching the lands so that a portion of the cutting tool cutting the land adjacent the cutting tool does not cut the land furthest from the cutting tool.
Claim 6
Dependent Claim 62 words
The method recited in claim 1 wherein the rotor structure is frusto-conically shaped so that step 1 (c) further comprises cutting the grooves so that the largest diameter end of the rotor structure is cut to the full size of the cutting tool while the diminishing diameter potions of the rotor are cut to a cOrresponding smaller size of the cutting tool.
Claim 7
Dependent Claim 142 words
A multi-stage rotor structure for carrying a plurality of blades in an axial flow multi-fluid utilizing machine said rotor structure comprising: a plurality of radially extending lands; each of said lands defining an annular array of equally spaced and axially disposed grooves for carrying blades having roots of the side entry type; each of said arrays having an equal number of grooves and said array of groves in each land being aligned axially with corresponding arrays of grooves in the other lands to from a plurality of axial rows of grooves, said lands varying in diameter, and the depth of the grooves in each land being a direct function of the outer diameter of the land so that the larger diameter lands have deeper grooves and the grooves in the smallest diameter land is duplicated in a portion of the other lands.
Claim 8
Dependent Claim 142 words
A multi-stage rotor structure for carrying a plurality of blades in an axial flow multi-fluid utilizing machine said rotor structure comprising: a plurality of radially extending lands; each of said lands defining an annular array of equally spaced and axially disposed grooves for carrying blades having roots of the side entry type; each of said arrays having an equal number of grooves and said array of groves in each land being aligned axially with corresponding arrays of grooves in the other lands to from a plurality of axial rows of grooves, said lands varying in diameter, and the depth of the grooves in each land being a direct function of the outer diameter of the land so that the larger diameter lands have deeper grooves and the grooves in the smallest diameter land is duplicated in a portion of the other lands.
Claim 9
Dependent Claim 30 words
The structure recited in claim 6, wherein the grooves in each array are uniform in cross section and are equally spaced from the axis of rotation of the rotor structure.
Claim 10
Dependent Claim 28 words
The structure recited in claim 6, wherein the rotor structure is frusto-conically shaped so that the lands are of diminishing cross section from one end to the other.
Claim 11
Dependent Claim 31 words
The structure recited in claim 6, wherein the rotor structure is frusto-conically shaped and the grooves in the lands are of diminishing cross-section corresponding to the diminishing diameter of the lands.

References Cited (Backward Citations)

US2461402A Cited
GB603578A Cited
US2619318A Cited
GB640969A Cited
US2743080A Cited
DE1140306B Cited
US3255515A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-09-19 1976-03-20 1976-09-19 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-09-19 1980-03-20 1980-09-19 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-09-19 1984-03-20 1984-09-19 $7700.00 Window Closed / Lapsed

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