US5869912A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Direct-cooled dynamoelectric machine stator core with enhanced heat transfer capability
Assignee: General Electric Co
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Filing: 1997-07-25
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Granted: 1999-02-09
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Expires: 2017-07-25
Abstract
Abstract In a dynamoelectric machine stator core assembly wherein adjacent packages of stacked laminations are separated by a plurality of radially extending spacer blocks, and wherein each adjacent pair of spacer blocks define in cooperation with adjacent axially spaced laminations, a cooling duct, the improvement comprising a plurality of turbulator elements in each cooling duct, each turbulator element extending into the duct from one of the adjacent axially spaced laminations.
Inventors
- 👤 Philip Lynn Andrew
- 👤 Frederick John Rink, Jr.
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 08:19
CPC Classifications
H; H02; H02K; H02K1/00; H02K1/06; H02K1/12; H02K1/20
Claims Analysis
Total Claims: 13
Claim 1
Independent Claim
97 words
In a dynamoelectric machine stator core assembly wherein adjacent packages of stacked laminations are separated by a plurality of radially extending spacer blocks, and wherein each adjacent pair of spacer blocks define in cooperation with adjacent axially spaced laminations, a radial cooling duct having a height dimension, the improvement comprising a plurality of turbulator elements in each radial cooling duct, each turbulator element extending into said radial cooling duct from at least one side of said adjacent axially spaced laminations, and wherein each turbulator has a height less than the height dimension of said radial cooling duct.
Claim 2
Dependent Claim
97 words
In a dynamoelectric machine stator core assembly wherein adjacent packages of stacked laminations are separated by a plurality of radially extending spacer blocks, and wherein each adjacent pair of spacer blocks define in cooperation with adjacent axially spaced laminations, a radial cooling duct having a height dimension, the improvement comprising a plurality of turbulator elements in each radial cooling duct, each turbulator element extending into said radial cooling duct from at least one side of said adjacent axially spaced laminations, and wherein each turbulator has a height less than the height dimension of said radial cooling duct.
Claim 3
Dependent Claim
21 words
The improvement of claim 1 wherein each turbulator element is formed integrally with said one of said adjacent axially spaced laminations.
Claim 4
Dependent Claim
48 words
The improvement of claim 2 wherein each turbulator element is partially cut from said one of said adjacent axially spaced laminations, and bent into said duct, said turbulator element extending at an angle of about 30° to about 90° to said one of said adjacent axially spaced laminations.
Claim 5
Dependent Claim
28 words
The improvement of claim 2 wherein each turbulator element extends at an angle of about 30° to about 45° to said one of said adjacent, axially spaced laminations.
Claim 6
Dependent Claim
24 words
The improvement of claim 3 wherein each turbulator element is oriented substantially perpendicular to a flow direction of coolant through said radial cooling duct.
Claim 7
Dependent Claim
20 words
The improvement of claim 3 wherein each turbulator is formed by a pair of ribs arranged in a substantially V-shape.
Claim 8
Dependent Claim
30 words
The improvement of claim 1 wherein each turbulator has a height equal to about 20% of the radial cooling duct height or 10% of the radial cooling duct hydraulic diameter.
Claim 9
Dependent Claim
33 words
The improvement of claim 7 wherein the turbulators are radially spaced along said radial cooling duct such that a ratio between the radial spacing and said height dimension of said radial cooling duct.
Claim 10
Dependent Claim
21 words
The improvement of claim 8 wherein said turbulator elements are spaced radially along said radial cooling duct by about 0.375 inch.
Claim 11
Dependent Claim
34 words
The improvement of claim 1 wherein each turbulator comprises an integral tab partially cut from said one of said adjacent axially spaced laminations, thereby also creating a cavity along the respective radial cooling duct.
Claim 12
Dependent Claim
14 words
The improvement of claim 1 wherein said turbulators extend parallel to a flow direction.
Claim 13
Dependent Claim
24 words
The improvement of claim 1 wherein said radial cooling turbulator elements extend into said duct from both sides of said adjacent axially spaced laminations.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 2002-02-08 | 2002-08-10 | 2003-02-09 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 2006-02-08 | 2006-08-10 | 2007-02-09 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2010-02-08 | 2010-08-10 | 2011-02-09 | $7700.00 | Window Closed / Lapsed |