US2012163997A1PendingUtilityA1
Vane compressor with integrated motor
Est. expiryDec 27, 2030(~4.5 yrs left)· nominal 20-yr term from priority
F04D 25/0606
39
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Claims
Abstract
A rotor disk of a vane compressor includes a multiple of slots along an outer diameter and a multiple of magnets along an inner diameter. Each of the multiple of slots is radially aligned with one of the multiple of magnets.
Claims
exact text as granted — not AI-modified1 . A rotor comprising:
a rotor disk with a multiple of slots along an outer diameter of said rotor disk; and a multiple of magnets located along an inner diameter of said rotor disk, each of said multiple of slots radially aligned with one of said multiple of magnets.
2 . The rotor as recited in claim 1 , further comprising a vane mounted within each of said multiple of slots.
3 . The rotor as recited in claim 1 , wherein said multiple of magnets are located axially within the rotor disk.
4 . The rotor as recited in claim 1 , wherein said multiple of magnets are oriented to avoid need for a back iron.
5 . The rotor as recited in claim 1 , wherein said multiple of magnets are oriented to define a circumferential magnetic field.
6 . A rotary vane compressor comprising:
a non-circular cam; a rotor within said non-circular cam; and a stator within said rotor to form a motor to rotate said rotor within said non-circular cam about said stator.
7 . The vane compressor as recited in claim 6 , wherein said rotor includes a rotor disk with a multiple of slots along an outer diameter and a multiple of magnets along an inner diameter, each of said multiple of slots radially aligned with one of said multiple of magnets.
8 . The vane compressor as recited in claim 6 , further comprising a vane mounted within each of said multiple of slots to form a seal with said non-circular cam.
9 . The vane compressor as recited in claim 6 , wherein said multiple of magnets are oriented to define a circumferential magnetic field.
10 . A method of minimizing a rotor diameter within a rotary vane compressor comprising:
locating each of a multiple of vanes within respect to a magnetic field to minimize disruption to the magnetic field.
11 . The method as recited in claim 10 , further comprising locating each of the multiple of vanes radially outboard of a respective magnet.
12 . The method as recited in claim 10 , further comprising circumferentially orienting the magnetic field.Cited by (0)
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