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US4023966A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of hot isostatic compaction

Assignee: RTX Corp
•
Filing: 1975-11-06
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Granted: 1977-05-17
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Expires: 1995-11-06
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Abstract

Abstract This invention involves a method for the hot isostatic compaction of particulate material into an article of intricate configuration. It comprises providing a removable pattern in the appropriate precompaction configuration of the article to be produced, coating the pattern with a first layer of conductive material and a second layer of metallic material, the two layers cooperating to provide a self-supporting and gas-impervious shell around the pattern and removing the pattern from the shell to provide a self-supporting and gas-impervious container having an internal configuration corresponding to the precompaction shape of the article to be produced. The container is then filled with particulate material, evacuated and sealed, and isostatically compacted in a pressure vessel at elevated temperature until the particulate material is compacted into a dense article of complex shape. The container is thereafter removed to obtain the compacted article. Dense articles of complex shape, such as gas turbine engine components including blades, discs and the like, are readily produced by the method of the invention.

Inventors

  • 👤 Joseph Frederick Loersch
  • 👤 Peter Alan Hurwitz
  • 👤 Lester Warren Jordan

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 07:57
CPC Classifications
B; B22; B22F; B22F3/00; B22F3/12; B22F3/14; B22F3/15; B22F3/1208; B22F3/1216; B22F3/1258; B22F3/1275

Claims Analysis

Total Claims: 41
Claim 1
Independent Claim 190 words
A method for hot isostatic compaction of particulate material into an article of intricate configuration comprising the steps of: a. providing a removable pattern in the appropriate precompaction configuration of the article to be made; b. coating the pattern with a first layer of conductive material, the thickness of said layer being sufficient to provide a substantially continuous conductive surface; c. electroplating over the first layer with a second layer of metallic material, the thickness of said second layer in combination with the thickness of said first layer being sufficient to provide a self-supporting and gas-impervious shell around the pattern; d. removing the pattern from the shell, thereby providing a self-supporting and gas-impervious container for receiving and confining the particulate material in the appropriate precompaction configuration of the article to be made; e. filling the container with particulate material, including the step of establishing a vacuum therein; f. sealing the container against the atmosphere; g. compacting the container and particulate material at elevated temperature by isostatic pressure so that a dense article of desired configuration is formed from the particulate material; and h. removing the container from the compacted article.
Claim 2
Independent Claim 190 words
A method for hot isostatic compaction of particulate material into an article of intricate configuration comprising the steps of: a. providing a removable pattern in the appropriate precompaction configuration of the article to be made; b. coating the pattern with a first layer of conductive material, the thickness of said layer being sufficient to provide a substantially continuous conductive surface; c. electroplating over the first layer with a second layer of metallic material, the thickness of said second layer in combination with the thickness of said first layer being sufficient to provide a self-supporting and gas-impervious shell around the pattern; d. removing the pattern from the shell, thereby providing a self-supporting and gas-impervious container for receiving and confining the particulate material in the appropriate precompaction configuration of the article to be made; e. filling the container with particulate material, including the step of establishing a vacuum therein; f. sealing the container against the atmosphere; g. compacting the container and particulate material at elevated temperature by isostatic pressure so that a dense article of desired configuration is formed from the particulate material; and h. removing the container from the compacted article.
Claim 3
Dependent Claim 32 words
The method of claim 1 wherein the removable pattern is treated to reduce the surface asperity and provide a clean, continuous surface prior to coating with said first layer of conductive material.
Claim 4
Dependent Claim 12 words
The method of claim 1 wherein the pattern is a nonconductive material.
Claim 5
Dependent Claim 11 words
The method of claim 3 wherein the pattern is casting wax.
Claim 6
Dependent Claim 14 words
The method of claim 1 wherein the pattern is formed in a mold cavity.
Claim 7
Dependent Claim 11 words
The method of claim 5 wherein the pattern is injection molded.
Claim 8
Dependent Claim 16 words
The method of claim 1 wherein the first layer of conductive material is applied by electroless-deposition.
Claim 9
Dependent Claim 16 words
The method of claim 1 wherein the first layer of conductive material is a metallic deposit.
Claim 10
Dependent Claim 20 words
The method of claim 1 wherein the second layer of metallic material is coated with at least one gas-impervious layer.
Claim 11
Dependent Claim 19 words
The method of claim 1 wherein the pattern is provided in the shape of a gas turbine engine component.
Claim 12
Dependent Claim 13 words
The method of claim 1 wherein the particulate material is a superalloy powder.
Claim 13
Independent Claim 203 words
A method for hot isostatic compaction of particulate material into an article of intricate configuration comprising the steps of: a. providing a removable pattern in multiple sections in the appropriate precompaction configuration of the article to be made; b. coating the pattern sections with a first layer of conductive material, the thickness of said layer being sufficient to provide a substantially continuous conductive surface; c. electroplating over the first layer with a second layer of metallic material, the thickness of said second layer in combination with the thickness of said first layer being sufficient to provide self-supporting and gas-impervious shell sections around the pattern sections; d. removing the pattern sections from the shell sections; e. joining the shell sections together, thereby providing a self-supporting and gas-impervious container for receiving and confining the particulate material in the appropriate precompaction configuration of the article to be made; f. filling the container with particulate material, including the step of establishing a vacuum therein; g. sealing the container against the atmosphere; h. compacting the container and particulate material at elevated temperature by isostatic pressure so that a dense article of desired configuration is formed from the particulate material; and i. removing the container from the compacted article.
Claim 14
Independent Claim 203 words
A method for hot isostatic compaction of particulate material into an article of intricate configuration comprising the steps of: a. providing a removable pattern in multiple sections in the appropriate precompaction configuration of the article to be made; b. coating the pattern sections with a first layer of conductive material, the thickness of said layer being sufficient to provide a substantially continuous conductive surface; c. electroplating over the first layer with a second layer of metallic material, the thickness of said second layer in combination with the thickness of said first layer being sufficient to provide self-supporting and gas-impervious shell sections around the pattern sections; d. removing the pattern sections from the shell sections; e. joining the shell sections together, thereby providing a self-supporting and gas-impervious container for receiving and confining the particulate material in the appropriate precompaction configuration of the article to be made; f. filling the container with particulate material, including the step of establishing a vacuum therein; g. sealing the container against the atmosphere; h. compacting the container and particulate material at elevated temperature by isostatic pressure so that a dense article of desired configuration is formed from the particulate material; and i. removing the container from the compacted article.
Claim 15
Dependent Claim 32 words
The method of claim 12 wherein each pattern section is treated to reduce the surface asperity and provide a clean, continuous surface prior to coating with said first layer of conductive material.
Claim 16
Dependent Claim 12 words
The method of claim 12 wherein the pattern is a nonconductive material.
Claim 17
Dependent Claim 11 words
The method of claim 14 wherein the pattern is casting wax.
Claim 18
Dependent Claim 15 words
The method of claim 12 wherein each pattern section is formed in a mold cavity.
Claim 19
Dependent Claim 16 words
The method of claim 12 wherein the first layer of conductive material is applied by electroless-deposition.
Claim 20
Dependent Claim 16 words
The method of claim 12 wherein the first layer of conductive material is a metallic deposit.
Claim 21
Dependent Claim 20 words
The method of claim 12 wherein the second layer of metallic material is coated with at least one gas-impervious layer.
Claim 22
Dependent Claim 14 words
The method of claim 12 wherein the shell sections are joined together by welding.
Claim 23
Dependent Claim 22 words
The method of claim 12 wherein the pattern of multiple sections is provided in the shape of a gas turbine engine component.
Claim 24
Dependent Claim 13 words
The method of claim 12 wherein the particulate material is a superalloy powder.
Claim 25
Independent Claim 191 words
A method for hot isostatic compaction of nickel-base superalloy particulate material into a gas turbine engine component comprising the steps of: a. providing a removable, nonconductive pattern in the appropriate precompaction configuration of the component to be made; b. electroless-depositing on the pattern a first layer of conductive material, the thickness of said layer being sufficient to provide a substantially continuous conductive surface for subsequent coating; c. electroplating the first layer with a second layer of metallic material, the thickness of said second layer in combination with the thickness of said first layer being sufficient to provide a self-supporting and gas-impervious shell around the pattern; d. removing the pattern from the shell, thereby providing a self-supporting and gas-impervious container for receiving and confining the powder in the appropriate precompaction configuration of the component; e. filling the container with particulate material, including the step of establishing a vacuum therein; f. sealing the container against the atmosphere; g. compacting the container and particulate material at elevated temperature by isostatic pressure so that a near 100 percent dense component is formed from the particulate material; and h. removing the container from the compacted component.
Claim 26
Independent Claim 191 words
A method for hot isostatic compaction of nickel-base superalloy particulate material into a gas turbine engine component comprising the steps of: a. providing a removable, nonconductive pattern in the appropriate precompaction configuration of the component to be made; b. electroless-depositing on the pattern a first layer of conductive material, the thickness of said layer being sufficient to provide a substantially continuous conductive surface for subsequent coating; c. electroplating the first layer with a second layer of metallic material, the thickness of said second layer in combination with the thickness of said first layer being sufficient to provide a self-supporting and gas-impervious shell around the pattern; d. removing the pattern from the shell, thereby providing a self-supporting and gas-impervious container for receiving and confining the powder in the appropriate precompaction configuration of the component; e. filling the container with particulate material, including the step of establishing a vacuum therein; f. sealing the container against the atmosphere; g. compacting the container and particulate material at elevated temperature by isostatic pressure so that a near 100 percent dense component is formed from the particulate material; and h. removing the container from the compacted component.
Claim 27
Dependent Claim 11 words
The method of claim 23 wherein the pattern is injection molded.
Claim 28
Dependent Claim 11 words
The method of claim 23 wherein the pattern is casting wax.
Claim 29
Dependent Claim 32 words
The method of claim 23 wherein the pattern is glass peened to reduce the surface asperity and provide a clean, continuous surface prior to coating with the first layer of conductive material.
Claim 30
Dependent Claim 16 words
The method of claim 23 wherein the first layer of conductive material is a metallic deposit.
Claim 31
Dependent Claim 11 words
The method of claim 27 wherein the metallic deposit is nickel.
Claim 32
Dependent Claim 11 words
The method of claim 27 wherein the metallic deposit is iron.
Claim 33
Dependent Claim 14 words
The method of claim 23 wherein the second layer of metallic material is nickel.
Claim 34
Dependent Claim 14 words
The method of claim 23 wherein the second layer of metallic material is iron.
Claim 35
Dependent Claim 11 words
The method of claim 23 wherein the component is a disc.
Claim 36
Dependent Claim 19 words
The method of claim 23 wherein the thickness of the layer of conductive material is at least 0.010 mils.
Claim 37
Dependent Claim 26 words
The method of claim 23 wherein the thickness of the second layer in combination with the thickness of the first layer is at least 40 mils.
Claim 38
Independent Claim 118 words
A method for forming a self-supporting and gas-impervious container for use in the hot isostatic compaction of particulate material into an article of intricate configuration comprising the steps of: a. providing a removable pattern in the appropriate precompaction configuration of the article to be made; b. coating the pattern with a first layer of conductive material, the thickness of said layer being sufficient to provide a substantially continuous conductive surface; c. electroplating over the first layer with a second layer of metallic material, the thickness of said second layer in combination with the thickness of said first layer being sufficient to provide a self-supporting and gas-impervious shell around the pattern; and d. removing the pattern from the shell.
Claim 39
Independent Claim 118 words
A method for forming a self-supporting and gas-impervious container for use in the hot isostatic compaction of particulate material into an article of intricate configuration comprising the steps of: a. providing a removable pattern in the appropriate precompaction configuration of the article to be made; b. coating the pattern with a first layer of conductive material, the thickness of said layer being sufficient to provide a substantially continuous conductive surface; c. electroplating over the first layer with a second layer of metallic material, the thickness of said second layer in combination with the thickness of said first layer being sufficient to provide a self-supporting and gas-impervious shell around the pattern; and d. removing the pattern from the shell.
Claim 40
Independent Claim 131 words
A method for forming a self-supporting and gas-impervious container for use in the hot isostatic compaction of particulate material into an article of intricate configuration comprising the steps of: a. providing a removable pattern in multiple sections in the appropriate precompaction configuration of the article to be made; b. coating the pattern sections with a first layer of conductive material, the thickness of said layer being sufficient to provide a substantially continuous conductive surface; c. electroplating over the first layer with a second layer of metallic material, the thickness of said second layer in combination with the thickness of said first layer being sufficient to provide self-supporting and gas-impervious shell sections around the pattern sections; d. removing the pattern sections from the shell sections; and e. joining the shell sections together.
Claim 41
Independent Claim 131 words
A method for forming a self-supporting and gas-impervious container for use in the hot isostatic compaction of particulate material into an article of intricate configuration comprising the steps of: a. providing a removable pattern in multiple sections in the appropriate precompaction configuration of the article to be made; b. coating the pattern sections with a first layer of conductive material, the thickness of said layer being sufficient to provide a substantially continuous conductive surface; c. electroplating over the first layer with a second layer of metallic material, the thickness of said second layer in combination with the thickness of said first layer being sufficient to provide self-supporting and gas-impervious shell sections around the pattern sections; d. removing the pattern sections from the shell sections; and e. joining the shell sections together.

References Cited (Backward Citations)

US3622313A Cited
US3450528A Cited
US3804575A Cited
US3841870A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-05-16 1980-11-15 1981-05-17 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-05-16 1984-11-15 1985-05-17 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-05-16 1988-11-15 1989-05-17 $7700.00 Window Closed / Lapsed

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