US2018269748A1PendingUtilityA1
Flywheel Rotor
Est. expiryAug 26, 2034(~8.1 yrs left)· nominal 20-yr term from priority
C21D 8/00Y02E60/16F16C 15/00C21D 8/005H02K 7/025C21D 9/0068F16C 2361/55C21D 2261/00
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Claims
Abstract
A solid steel flywheel rotor having improved material properties offers improved energy storage at reduced cost. A process for manufacturing the rotor is also provided.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . A flywheel rotor comprising a rotationally symmetric mass made of a single piece of steel having:
a yield strength of at least 900 MPa; a fracture toughness of at least 40 MPa·m 0.5 ; and a maximal intrinsic defect size that is 2 mm or smaller, wherein the mass has a diameter that is greater along a first axis than its widest thickness along a second axis, the widest thickness being between 8 inches and 14 inches, the mass configured to rotate about the second axis.
2 . The flywheel rotor of claim 1 , wherein the mass does not include a hole through a center axis of the mass.
3 . The flywheel rotor of claim 1 , further comprising a plurality of journals protruding from the mass, each journal shaped to physically couple to a shaft.
4 . The flywheel rotor of claim 1 , wherein the rotor has a mass in a range from 2 tons to 10 tons.
5 . The flywheel rotor of claim 1 , wherein the mass has an outer diameter in a range from 36 inches to 94 inches.
6 . The flywheel rotor of claim 1 , wherein the mass is formed of through-hardened and tempered 300M steel, formed using at least one of:
a vacuum-arc-remelting (VAR) process, an electro-slag-remelting (ESR) process, or a vacuum induction melting (VIM) process.
7 . The flywheel rotor of claim 1 , wherein the mass has a fishtail shape.
8 . The flywheel rotor of claim 1 wherein the fracture toughness is in a range from 150 MPa·m 0.5 to 300 MPa·m 0.5 .
9 . A flywheel rotor comprising:
a rotationally symmetric body made of a single piece of through-hardened and tempered steel, the mass having a diameter greater along a first axis than its widest thickness along a second axis, wherein the mass is in a range between 2 tons and 5 tons; and a plurality of journals protruding from the body, each journal shaped to physically couple to a shaft, wherein the body is configured to rotate about the second axis.
10 . The flywheel rotor of claim 9 , wherein the body has a yield strength of at least 900 MPa.
11 . The flywheel rotor of claim 9 , wherein the body has a fracture toughness of at least 40 MPa·m 0.5 .
12 . The flywheel rotor of claim 9 , wherein the body has a maximal intrinsic defect size that is equal to or smaller than 2 mm.
13 . The flywheel rotor of claim 9 , wherein the body does not include a hole through a center axis of the body.
14 . The flywheel rotor of claim 9 , wherein at least some portion of the body is greater than 4 inches from an outer surface of the mass.
15 . The flywheel rotor of claim 9 , wherein the widest thickness is in a range between 8 inches and 16 inches.
16 . The flywheel rotor of claim 9 , wherein the diameter is at least 48 inches.
17 . The flywheel rotor of claim 9 , wherein the body has a fishtail shape.
18 . A method for manufacturing a flywheel rotor comprising:
alloying a plurality of elements to form a single mass of steel, the mass having a diameter greater along a first axis than its widest thickness along a second axis, the widest thickness being between 8 inches and 14 inches, the mass configured to rotate about the second axis; refining the mass using one of:
a vacuum-arc-remelting (VAR) process,
an electro-slag-remelting (ESR) process, and
a vacuum induction melting (VIM) process;
performing a multi-step forging process to align grain size and direction within the mass; heating and quenching the mass to through-harden the mass; tempering the mass; and machining the mass.Cited by (0)
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