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Patent metadata

Field	Value
Publication number	US-11351606-B2
Application number	US-201816634916-A
Country	US
Kind code	B2
Filing date	Aug 2, 2018
Priority date	Aug 4, 2017
Publication date	Jun 7, 2022
Grant date	Jun 7, 2022

Abstract

A method of manufacturing a part, the method involving providing an apparatus, the apparatus having a metal skin component; a metal HIP can and a hollow space between a portion of the HIP can and a portion of the skin component, the method further involving filling the HIP can with a metal powder; evacuating the HIP can; sealing the evacuated HIP can; and applying a HIP process to the apparatus in a HIP chamber so as to form the part.

First claim

The invention claimed is:

1. A method of manufacturing a part, the method comprising the steps of:
providing an apparatus, the apparatus comprising:
a skin component formed of a metal sheet having a first side and a second side;
a HIP can formed of metal and having a first side and a second side;
wherein the second side of the HIP can is joined to the first side of the skin component, and wherein the HIP can defines a sealed volume and wherein the HIP can comprises a filling means to fill the sealed volume with metal powder;
wherein there is a hollow space between a portion of the second side of the HIP can and a portion of the first side of the skin component, and the apparatus comprises a vent into the hollow space to allow pressure applied during the HIP process to be communicated into the hollow space;
filling the HIP can with a metal powder;
evacuating the HIP can;
sealing the evacuated HIP can; and
applying a HIP process to the apparatus in a HIP chamber so as to form the part,
wherein the part is a hollow part.

2. The method according to claim 1 , wherein the HIP can is electron beam welded to the skin.

3. The method according to claim 1 , wherein the HIP can is not subsequently removed after the HIP process.

4. The method according to claim 1 , wherein the skin component, the HIP can and the metal powder are formed from metals with the same thermal expansion coefficient ±15% differential.

5. The method according to claim 1 , wherein the skin component, the HIP can, and the metal powder are formed from the same metal.

6. The method according to claim 1 , wherein the skin component, the HIP can and the metal powder are formed from the same titanium alloy.

7. The method according to claim 1 , wherein applying the HIP process to the apparatus in a HIP chamber changes the apparatus to the part and wherein the hollow part of the apparatus becomes the hollow part of part.

8. The method according to claim 1 , wherein applying the HIP process to the apparatus in a HIP chamber consolidates the HIP can with the metal powder and consolidates the portion of the second side of the HIP can with the first side of the skin component at the points of contact.

9. The method according to claim 1 , wherein the part is an aircraft part.

10. The method according to claim 9 , wherein the part is an aircraft stringer consolidated with an aircraft skin.

11. The method according to claim 1 , further comprising attaching the apparatus to a base plate using a vacuum prior to applying the HIP process.

12. The method according to claim 1 , wherein providing the apparatus, comprises
forming a skin component from a metal sheet, the metal sheet having a first side, a second side, and a vent component through the first and second sides;
forming a HIP can having a first side, a second side, a sealed volume, and a filling means from metal;
joining the second side of the HIP can to the first side of the skin component so as to align the vent into the hollow space and so as to form a hollow space between a portion of the second side of the HIP can and a portion of the first side of the skin component.

13. An aircraft part produced by the method as defined in claim 1 .

14. A method of manufacturing a part, the method comprising the steps of:
providing an apparatus, the apparatus comprising:
a skin component formed of a metal sheet having a first side and a second side;
a HIP can formed of metal and having a first side and a second side;
wherein the second side of the HIP can is joined to the first side of the skin component, and wherein the HIP can defines a sealed volume and wherein the HIP can comprises a filling means to fill the sealed volume with metal powder;
wherein there is a hollow space between a portion of the second side of the HIP can and a portion of the first side of the skin component, and the apparatus comprises a vent into the hollow space to allow pressure applied during the HIP process to be communicated into the hollow space;
filling the HIP can with a metal powder;
evacuating the HIP can;
sealing the evacuated HIP can; and
applying a HIP process to the apparatus in a HIP chamber so as to form the part,
wherein the part is an aircraft part.

15. A method of manufacturing a part, the method comprising the steps of:
providing an apparatus, the apparatus comprising:
a skin component formed of a metal sheet having a first side and a second side;
a HIP can formed of metal and having a first side and a second side;
wherein the second side of the HIP can is joined to the first side of the skin component, and wherein the HIP can defines a sealed volume and wherein the HIP can comprises a filling means to fill the sealed volume with metal powder;
wherein there is a hollow space between a portion of the second side of the HIP can and a portion of the first side of the skin component, and the apparatus comprises a vent into the hollow space to allow pressure applied during the HIP process to be communicated into the hollow space;
filling the HIP can with a metal powder;
evacuating the HIP can;
sealing the evacuated HIP can;
attaching the apparatus to a base plate using a vacuum; and
applying a HIP process to the apparatus in a HIP chamber so as to form the part.

Assignees

• Bae Systems Plc

Inventors

• Price Howard James
• Chippendale John

Classifications

• B64C1/064

  Stringers; Longerons · CPC title

• B22F2999/00

  Aspects linked to processes or compositions used in powder metallurgy · CPC title

• B64F5/10

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• B22F5/10

  of articles with cavities or holes, not otherwise provided for in the preceding subgroups · CPC title

• B22F2003/153

  apparatus specific to HIP · CPC title