Patent US2836846A successfully refreshed from Google Patents.
Patent US4303771A successfully refreshed from Google Patents.
Patent US2497059A successfully refreshed from Google Patents.
← Back to Patent Explorer
US4738020A Expired / Lapsed US ⏱️ 0.0 years remaining

Method for manufacture of laminated parts

Assignee: LH Carbide Corp
•
Filing: 1986-04-17
•
Granted: 1988-04-19
•
Expires: 2006-04-17
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract Elongated thin strip stock is blanked to form interlocking laminas for electric motor or generator rotors or stators at successive blanking stations. At a final assembly station the laminas are stacked and pressed into interlocking relationship. In response to an operator input a predetermined number of reversals, or half turns about the stack axis of the previously stacked lamina are provided in order to compensate for nonuniform strip thickness to obtain a rotor or stator of substantially uniform height. Alternatively the thickness of the strip stock is gauged at transversely spaced points on the strip to determine cross feed thickness variation in the strip whereupon the stacked laminas are automatically provided with a number of reversals about the stack axis in response to a thickness differential that would result in a parallelism error in the stack that exceeds a predetermined amount. Rotor conductor slots are formed in the stacked laminas and are skewed to the stack axis by providing arcuate indexing of each lamina relative to the next preceding lamina in the stack by an arcuate increment that is automatically determined in response to operator entered inputs relative to the stack height, the skew angle, nominal lamina thickness and skew direction.

Inventors

  • 👤 Thomas R. Neuenschwander

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 00:14
CPC Classifications
B; B21; B21D; B21D28/00; B21D28/02; B21D28/22; H; H02; H02K; H02K15/00; H02K15/02; H02K15/021; H02K2201/00; H02K2201/09; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49002; Y10T29/49009; Y10T29/49012; Y10T29/53; Y10T29/53039; Y10T29/53061; Y10T29/5313; Y10T29/5317

Claims Analysis

Total Claims: 12
Claim 1
Independent Claim 156 words
A method of manufacturing laminated parts wherein the laminas of the parts are blanked from lamina areas on sheet stock and then stacked to form the part, the laminas having opposite planar surfaces, comprising: a first step of measuring the thickness of first and second spaced points on lamina stock for obtaining first and second thicknesses, respectively, of a lamina; a second step of comparing said first and second thicknesses and determining a thickness variation therebetween; a third step of stacking the laminas; a fourth step of where 112 selecting relative rotations between the lamina stack and a lamina to be stacked about a lamina axis perpendicular to the lamina planar surfaces according to said thickness variation to provide a lamina stack having a desired parallelism; a fifth step of providing said relative rotation of a selected lamina in said fourth step prior to stacking of said selected lamina to thereby compensate for lamina thickness variations.
Claim 2
Independent Claim 156 words
A method of manufacturing laminated parts wherein the laminas of the parts are blanked from lamina areas on sheet stock and then stacked to form the part, the laminas having opposite planar surfaces, comprising: a first step of measuring the thickness of first and second spaced points on lamina stock for obtaining first and second thicknesses, respectively, of a lamina; a second step of comparing said first and second thicknesses and determining a thickness variation therebetween; a third step of stacking the laminas; a fourth step of where 112 selecting relative rotations between the lamina stack and a lamina to be stacked about a lamina axis perpendicular to the lamina planar surfaces according to said thickness variation to provide a lamina stack having a desired parallelism; a fifth step of providing said relative rotation of a selected lamina in said fourth step prior to stacking of said selected lamina to thereby compensate for lamina thickness variations.
Claim 3
Dependent Claim 20 words
The method of claim 1 wherein said fifth step provides said relative rotation within an arcuate range of approximately 90°-270°.
Claim 4
Dependent Claim 16 words
The method of claim 1 wherein said fifth step provides a relative rotation of approximately 180°.
Claim 5
Dependent Claim 54 words
The method of claim 1 wherein said fourth step comprises selecting said relative rotations according to the difference of the sum of the first thicknesses of each lamina in the stack and the sum of the second thicknesses of each lamina in the stack in relation to a factor of the desired stack parallelism.
Claim 6
Dependent Claim 64 words
The method of claim 4 wherein said fourth step selecting is performed in the following manner; ______________________________________ CONDITION relative rotation ______________________________________ ΣT.sub.1 - ΣT.sub.2 > +/- E.sub.P /2 Yes ΣT.sub.1 - ΣT.sub.2 < +/- E.sub.P /2 No ______________________________________ where: T 1 =said first thickness measurement of said sheet stock; T 2 =said second thickness measurement of said sheet stock; E p =Predetermined parallelism error.
Claim 7
Independent Claim 253 words
A method of manufacturing laminated parts wherein the laminas of the parts are blanked from lamina areas on sheet stock and then stacked to form the part, the laminas having opposite planar surfaces, comprising: a first step of stacking the laminas; a second step of selecting relative rotations between the lamina stack and a lamina to be stacked about a lamina axis substantially perpendicular to said lamina planar sufaces to provide a lamina having a desired parallelism; said selecting being performed in the following manner; ______________________________________ CONDITION relative rotation ______________________________________ n < (N/2Q - 1/2) No (N/2Q - 1/2) < n < (N/2Q + 1/2) Yes (N/2Q + 1/2) < n < (1.5N/2Q - 1/2) No (1.5N/2Q - 1/2) < n < (1.5N/2Q + 1/2) Yes (1.5N/2Q + 1/2) < n < (2.5N/2Q - 1/2) No (2.5N/2Q - 1/2) < n < (2.5N/2Q + 1/2) Yes (2.5N/2Q + 1/2) < n < (3.5N/2Q - 1/2) No (3.5N/2Q - 1/2) < n < (3.5N/2Q + 1/2) Yes (3.5N/2Q + 1/2) < n < (4.5N/2Q - 1/2) No (4.5N/2Q - 1/2) < n < (4.5N/2Q + 1/2) Yes (4.5N/2Q + 1/2) < n No ______________________________________ Where: N=nominal total number of laminas in a stack; Q=number of predetermined stack relative rotations; n=the particular lamina number in a stack where n=1 for the first lamina and n=N for the last lamina; a third step of providing said relative rotatio for a selected lamina prior to stacking of said selected lamina to thereby compensate for lamina thickness variations.
Claim 8
Independent Claim 253 words
A method of manufacturing laminated parts wherein the laminas of the parts are blanked from lamina areas on sheet stock and then stacked to form the part, the laminas having opposite planar surfaces, comprising: a first step of stacking the laminas; a second step of selecting relative rotations between the lamina stack and a lamina to be stacked about a lamina axis substantially perpendicular to said lamina planar sufaces to provide a lamina having a desired parallelism; said selecting being performed in the following manner; ______________________________________ CONDITION relative rotation ______________________________________ n < (N/2Q - 1/2) No (N/2Q - 1/2) < n < (N/2Q + 1/2) Yes (N/2Q + 1/2) < n < (1.5N/2Q - 1/2) No (1.5N/2Q - 1/2) < n < (1.5N/2Q + 1/2) Yes (1.5N/2Q + 1/2) < n < (2.5N/2Q - 1/2) No (2.5N/2Q - 1/2) < n < (2.5N/2Q + 1/2) Yes (2.5N/2Q + 1/2) < n < (3.5N/2Q - 1/2) No (3.5N/2Q - 1/2) < n < (3.5N/2Q + 1/2) Yes (3.5N/2Q + 1/2) < n < (4.5N/2Q - 1/2) No (4.5N/2Q - 1/2) < n < (4.5N/2Q + 1/2) Yes (4.5N/2Q + 1/2) < n No ______________________________________ Where: N=nominal total number of laminas in a stack; Q=number of predetermined stack relative rotations; n=the particular lamina number in a stack where n=1 for the first lamina and n=N for the last lamina; a third step of providing said relative rotatio for a selected lamina prior to stacking of said selected lamina to thereby compensate for lamina thickness variations.
Claim 9
Independent Claim 240 words
A method of stamping electric motor stator or rotor laminas from sheet stock material, provided from a supply, to form a stack of laminas each having a planar surface comprising the steps of: a first step of guiding sheet stock material from the supply; a second step of stamping laminas in predetermined planar configurations each having an axis substantially perpendicular to the lamina plane and each having conductor slot openings arcuately spaced about said axis; a third step of coaxially stacking said laminas so that the lamina axes are coaxial to form a stack having a stack axis substantially coaxial with said lamina axes, said stack axis being substantially perpendicular to the plane of each of said laminas; a fourth step of providing incremental indexing of each of said laminas relative said stack rotationally about said stack axis a predetermined degree of rotational arc prior to stacking of said each lamina so that said openings form conductor slots having a slot axis skewed to said stack axis by a skew angle corresponding to said degree of rotational arc; a fifth step of adjustable presetting the degree of said rotational arc to automatically obtain a desired skew angle; a sixth step of utilizing the parameters of relative skew between said slot axes and said stack axis, stack height, and lamina thickness to determine said predetermined degree of rotational arc for automatically arcuately indexing each lamina to obtain said desired skew angle.
Claim 10
Independent Claim 240 words
A method of stamping electric motor stator or rotor laminas from sheet stock material, provided from a supply, to form a stack of laminas each having a planar surface comprising the steps of: a first step of guiding sheet stock material from the supply; a second step of stamping laminas in predetermined planar configurations each having an axis substantially perpendicular to the lamina plane and each having conductor slot openings arcuately spaced about said axis; a third step of coaxially stacking said laminas so that the lamina axes are coaxial to form a stack having a stack axis substantially coaxial with said lamina axes, said stack axis being substantially perpendicular to the plane of each of said laminas; a fourth step of providing incremental indexing of each of said laminas relative said stack rotationally about said stack axis a predetermined degree of rotational arc prior to stacking of said each lamina so that said openings form conductor slots having a slot axis skewed to said stack axis by a skew angle corresponding to said degree of rotational arc; a fifth step of adjustable presetting the degree of said rotational arc to automatically obtain a desired skew angle; a sixth step of utilizing the parameters of relative skew between said slot axes and said stack axis, stack height, and lamina thickness to determine said predetermined degree of rotational arc for automatically arcuately indexing each lamina to obtain said desired skew angle.
Claim 11
Dependent Claim 95 words
The method of claim 7 comprising a seventh step of rotating at least one of said laminas relative to said stack about a stack axis that is substantially perpendicular to the planar surface of said laminas in a rotational arc that is in addition to and substantially greater than said fourth step indexing rotational arc; said fourth and seventh steps in addition to providing incremental indexing of each of said laminas relative to said stack rotationally about said stack axis rotating said at least one lamina relative said stack to compensate for lamina thickness variations.
Claim 12
Dependent Claim 21 words
The method of claim 8 wherein said seventh step rotates said at least one lamina within an arc of approximately 90°-270°.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1991-04-19 1991-10-19 1992-04-19 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1995-04-19 1995-10-19 1996-04-19 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1999-04-19 1999-10-19 2000-04-19 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag