Turbine coolant supply system
US-9091173-B2 · Jul 28, 2015 · US
US10458243B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10458243-B2 |
| Application number | US-201815954118-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 16, 2018 |
| Priority date | Jan 20, 2015 |
| Publication date | Oct 29, 2019 |
| Grant date | Oct 29, 2019 |
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The present disclosure provides devices and methods related to rotor disk bosses. For example, a rotor disk assembly comprises a first rotor disk, wherein the first rotor disk comprises a web, disposed between a rim and a bore. The rotor disk assembly further comprises a second rotor disk operatively coupled to the first rotor disk, an inter-disk device disposed on the second rotor disk and extending axially toward the first rotor disk, and a boss disposed on the first rotor disk, wherein the boss protrudes axially from the web toward the inter-disk device.
Opening claim text (preview).
What is claimed is: 1. A method for designing a rotor disk assembly, the method comprising: determining a probable point of contact on a first rotor disk in response to an inter-disk device failure, wherein: the first rotor disk comprises a web that is disposed between a rim and a bore; the bore abuts the web at a web foot that is a radially inwardmost portion of the web; the rotor disk assembly further comprises a second rotor disk operatively coupled to the first rotor disk; the inter-disk device is disposed on the second rotor disk and extends axially toward the first rotor disk; and the inter-disk device comprises a spacer arm that is a portion of the inter-disk device that extends farthest axially from the second rotor disk; and redesigning the first rotor disk to include a boss at the probable point of contact. 2. The method of claim 1 , further comprising adding material at the probable point of contact to create the boss such that: the boss protrudes axially from the web toward the spacer arm of the inter-disk device; a distance is defined between the spacer arm and the boss; a radial-direction span of the boss is radially aligned with the spacer arm; the boss is disposed radially outward of, and immediately adjacent to, the web foot; the boss comprises a planar surface extending radially; and the web foot extends axially outward and away, relative to a radius of the first rotor disk, from a radial inner edge of the planar surface. 3. The method of claim 1 , further comprising determining the life cycle of a rotor disk. 4. The method of claim 1 , further comprising improving the manufacturability of the rotor disk.
Blades ({specially adapted for radial flow machines or engines F01D5/04}; blade roots F01D5/30; rotors with blades adjustable in operation F01D7/00; stator blades F01D9/02) · CPC title
Component parts, details, or accessories, not provided for in, or of interest apart from, other groups · CPC title
Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections {(F01D5/022, F01D5/023 take precedence)} · CPC title
for turbines · CPC title
with concentric rows of axial blades · CPC title
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