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US3579805A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of forming interference fits by heat treatment

Assignee: General Electric Co
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Filing: 1968-07-05
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Granted: 1971-05-25
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Expires: 1988-07-05
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Abstract

Abstract An interference fit can be provided between metal components where at least one of the components is formed of a precipitation-hardenable metal alloy which undergoes a substantially permanent dimensional change in addition to a reversible dimensional change upon heat treatment at elevated temperatures. The interference fit itself will be irreversible if both components are formed of the preciptitation-hardenable alloy and reversible if only one of the components is formed of the alloy.

Inventors

  • 👤 Howard Berdolt Kast

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-23 14:12
CPC Classifications
C; C21; C21D; C21D6/00; C21D6/02; B; B23; B23P; B23P11/00; B23P11/02; B23P11/025; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49826; Y10T29/49863; Y10T29/49865

Claims Analysis

Total Claims: 11
Claim 1
Independent Claim 98 words
A method for forming an interference fit between inner and outer members adapted to be interfitted, comprising the steps of: a. providing at least one of said members of a precipitationhardenable alloy which undergoes substantially irreversible dimensional change upon heat treatment thereof, b. solution annealing said precipitation-hardenable alloy at a temperature in excess of the solutioning temperature of said alloy, c. interfitting said members to form an assembly with a clearance between said members smaller than the substantially irreversible dimensional change, and d. subjecting said assembly to a precipitation-hardening heat treatment which causes said substantially irreversible dimensional change.
Claim 2
Independent Claim 98 words
A method for forming an interference fit between inner and outer members adapted to be interfitted, comprising the steps of: a. providing at least one of said members of a precipitationhardenable alloy which undergoes substantially irreversible dimensional change upon heat treatment thereof, b. solution annealing said precipitation-hardenable alloy at a temperature in excess of the solutioning temperature of said alloy, c. interfitting said members to form an assembly with a clearance between said members smaller than the substantially irreversible dimensional change, and d. subjecting said assembly to a precipitation-hardening heat treatment which causes said substantially irreversible dimensional change.
Claim 3
Dependent Claim 24 words
A method, as claimed in claim 1, wherein said precipitation-hardening heat treatment is accomplished at a temperature of from about 900* to 1,150* F.
Claim 4
Dependent Claim 23 words
A method, as claimed in claim 1, wherein said members are both formed of said precipitation-hardenable alloy and said interference fit is irreversible.
Claim 5
Dependent Claim 28 words
A method, as claimed in claim 3, including the additional step after solution annealing of said precipitatioN-hardenable alloy of cooling said alloy prior to interfitting of said members.
Claim 6
Dependent Claim 32 words
A method, as claimed in claim 4, wherein said dimensional change is a contraction and including the additional step of subjecting said inner member to a precipitation-hardening heat treatment after solution-annealing thereof.
Claim 7
Dependent Claim 33 words
A method, as claimed in claim 4, wherein said dimensional change is an expansion and including the additional step of subjecting said outer member to a precipitation-hardening heat treatment after solution annealing thereof.
Claim 8
Dependent Claim 36 words
A method, as claimed in claim 1 wherein one of said members is formed of said precipitation-hardenable alloy, the other of said members is formed of a conventional alloy, and said resulting interference fit is reversible.
Claim 9
Dependent Claim 27 words
A method, as claimed in claim 7, including the additional step after solution-annealing of said precipitation-hardenable alloy of cooling said alloy prior to interfitting of said members.
Claim 10
Dependent Claim 23 words
A method, as claimed in claim 8, wherein said dimensional change is a contraction and said outer member is formed of said alloy.
Claim 11
Dependent Claim 23 words
A method, as claimed in claim 8, wherein said dimensional change is an expansion and said inner member is formed of said alloy.

References Cited (Backward Citations)

GB475244A Cited
US2647847A Cited
US3098662A Cited
US3316129A Cited
US3408178A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1974-05-24 1974-11-23 1975-05-25 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1978-05-24 1978-11-23 1979-05-25 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1982-05-24 1982-11-23 1983-05-25 $7700.00 Window Closed / Lapsed

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