US3574924A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Solid state repair method and means
Assignee: Boeing North American Inc
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Filing: 1968-10-28
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Granted: 1971-04-13
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Expires: 1988-10-28
Abstract
Abstract A method of rebuilding a jet engine compressor, fan, or turbine blade containing a worn or damaged area by trimming off the portion of such blade surrounding the area and replacing such portion with another of precisely corresponding size and metallurgical composition. Standardized templates define the size of the trimmed off portion. The replaced portion is integrally joined to the blade by solid state molecular diffusion bonding in a mold exactly duplicating the contour of the original blade when new.
Inventors
- 👤 Gordon L Dibble
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 12:51
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/005; B; B22; B22D; B22D19/00; B22D19/10; Y; Y02; Y02T; Y02T50/00; Y02T50/60; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49718; Y10T29/49732; Y10T29/49734; Y10T29/49737
Claims Analysis
Total Claims: 12
Claim 1
Independent Claim
166 words
A method of repairing a worn or damaged metallic article, comprising the steps of: providing a pair of mating dies, the workfaces of which are adapted to define a cavity having the precise size and shape of said article in the new and undamaged condition when said dies are in mating relationship; removing a portion of said article to create a vacant area thereon, said portion including the worn or damaged area of said article; placing said article in said dies with at least one separate incremental mass positioned in said vacant area, said mass being of the same material as said article, the volumetric content of said mass being at least equal to the volume of the void formed by said vacant area in said cavity when said dies are in mating relationship; and applying sufficient heat and pressure to said dies to cause said mass both to deform into conformity with said void and to join said article by solid-state molecular diffusion bonding therebetween.
Claim 2
Independent Claim
166 words
A method of repairing a worn or damaged metallic article, comprising the steps of: providing a pair of mating dies, the workfaces of which are adapted to define a cavity having the precise size and shape of said article in the new and undamaged condition when said dies are in mating relationship; removing a portion of said article to create a vacant area thereon, said portion including the worn or damaged area of said article; placing said article in said dies with at least one separate incremental mass positioned in said vacant area, said mass being of the same material as said article, the volumetric content of said mass being at least equal to the volume of the void formed by said vacant area in said cavity when said dies are in mating relationship; and applying sufficient heat and pressure to said dies to cause said mass both to deform into conformity with said void and to join said article by solid-state molecular diffusion bonding therebetween.
Claim 3
Dependent Claim
73 words
The method set forth in claim 1 above, further including, prior to said removing step: providing at least one template for mass production use on a plurality of damaged articles corresponding generally with said damaged article; placing said template in close proximity to said damaged article over said damaged area; and tracing said template on said article to define said vacant area whereby said removed portion corresponds in plan view with said template.
Claim 4
Dependent Claim
27 words
The method set forth in claim 1 above wherein: said mass has a volumetric content from 0.01 to 10.0 percent larger than said volume of said void.
Claim 5
Dependent Claim
37 words
The method set forth in claim 1 above wherein: said metallic article is made of Ti-6A1-4V titanium alloy; and said heat and pressure are from about 1600* to 1725* F. and from 2000 to 5000 p.s.i., respectively.
Claim 6
Dependent Claim
39 words
The method set forth in claim 4 above, wherein: said dies containing said article and said mass are positioned within an airtight retort; and a vacuum is maintained in said retort continuously during application of said heat and pressure.
Claim 7
Dependent Claim
107 words
A mass-production method for repairing a multitude of worn or damaged metallic articles having identical design but a variety of different types and locations of wear or damage, comprising the steps of: forming a plurality of standardized templates having predetermined area dimensions; prefabricating a plurality of incremental masses corresponding in area with said area dimensions of said templates; removing portions of said articles, said removed portions containing said worn or damaged areas and corresponding in area with said templates; placing said masses in the voids resulting in said articles from removal of said portions; and joining said masses to said articles by solid-state molecular diffusion bonding therebetween.
Claim 8
Dependent Claim
107 words
A mass-production method for repairing a multitude of worn or damaged metallic articles having identical design but a variety of different types and locations of wear or damage, comprising the steps of: forming a plurality of standardized templates having predetermined area dimensions; prefabricating a plurality of incremental masses corresponding in area with said area dimensions of said templates; removing portions of said articles, said removed portions containing said worn or damaged areas and corresponding in area with said templates; placing said masses in the voids resulting in said articles from removal of said portions; and joining said masses to said articles by solid-state molecular diffusion bonding therebetween.
Claim 9
Dependent Claim
79 words
The method set forth in claim 6 above, wherein: said bonding is accomplished by the steps of placing said individual articles together with said masses between a pair of mating dies defining a cavity having the contour of said articles in the undamaged condition; heating said dies and said articles to a temperature sufficient for said bonding to occur at a coordinated pressure; and applying said pressure to said dies to compress said articles therebetween until said bonding occurs.
Claim 10
Dependent Claim
31 words
The method set forth in claim 6 above, wherein: said masses have a total volumetric content from 0.01 to 10.0 percent larger than the total volumetric content of said removed portions.
Claim 11
Independent Claim
289 words
The method of mass production rebuilding a plurality of worn or damaged metallic articles of identical design, comprising the steps of: forming a plurality of standardized templates having predetermined plan area dimensions; prefabricating a plurality of incremental masses corresponding in plan view with said templates; trimming said articles to remove portions therefrom, said removed portions containing said worn or damaged locations and corresponding in plan area with said templates; providing a pair of mating dies, the workfaces of which are adapted to define a cavity having the precise size and shape of said articles in the new or undamaged condition when said dies are in fully mated relationship; successively placing each of said trimmed articles between said dies with a plurality of said masses positioned in the vacant areas resulting in said articles from removal of said portions therefrom, said masses being of the same material as said articles, the volumetric content of said masses in combination being at least equal to the volume of the voids formed in said cavity due to removal of said portions when said dies contain said trimmed articles and are in fully mated relationship; surrounding said dies with an airtight retort; maintaining a vacuum within said retort; heating said retort and its contents to a temperature sufficient for solid-state molecular diffusion bonding between said incremental masses and said trimmed articles; applying sufficient pressure to said dies to compress said articles and masses therebetween in an amount sufficient to deform said masses into conformity with said cavity and to achieve said diffusion bonding; and said masses having an initial combined volumetric content from 0.01 to 10.0 percent larger than said volume of said voids in said cavity resulting from said removal of said portions.
Claim 12
Independent Claim
289 words
The method of mass production rebuilding a plurality of worn or damaged metallic articles of identical design, comprising the steps of: forming a plurality of standardized templates having predetermined plan area dimensions; prefabricating a plurality of incremental masses corresponding in plan view with said templates; trimming said articles to remove portions therefrom, said removed portions containing said worn or damaged locations and corresponding in plan area with said templates; providing a pair of mating dies, the workfaces of which are adapted to define a cavity having the precise size and shape of said articles in the new or undamaged condition when said dies are in fully mated relationship; successively placing each of said trimmed articles between said dies with a plurality of said masses positioned in the vacant areas resulting in said articles from removal of said portions therefrom, said masses being of the same material as said articles, the volumetric content of said masses in combination being at least equal to the volume of the voids formed in said cavity due to removal of said portions when said dies contain said trimmed articles and are in fully mated relationship; surrounding said dies with an airtight retort; maintaining a vacuum within said retort; heating said retort and its contents to a temperature sufficient for solid-state molecular diffusion bonding between said incremental masses and said trimmed articles; applying sufficient pressure to said dies to compress said articles and masses therebetween in an amount sufficient to deform said masses into conformity with said cavity and to achieve said diffusion bonding; and said masses having an initial combined volumetric content from 0.01 to 10.0 percent larger than said volume of said voids in said cavity resulting from said removal of said portions.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1974-04-12 | 1974-10-12 | 1975-04-13 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1978-04-12 | 1978-10-12 | 1979-04-13 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1982-04-12 | 1982-10-12 | 1983-04-13 | $7700.00 | Window Closed / Lapsed |