Metal alloy knit fabric for high temperature insulating materials

Patent metadata

Field	Value
Publication number	US-11053615-B2
Application number	US-201916441353-A
Country	US
Kind code	B2
Filing date	Jun 14, 2019
Priority date	Feb 1, 2016
Publication date	Jul 6, 2021
Grant date	Jul 6, 2021

Abstract

Metal alloy knit fabrics, thermal protective members formed therefrom and their methods of construction are disclosed. This unique capability to knit high temperature metal alloy wire that is drapable allows for the creation of near net-shape preforms at production level speed. Additionally, ceramic insulation can also be integrated concurrently to provide increased thermal protection. The metal alloy knit fabrics described herein overcome the limitations of current welded stainless steel mesh seal coverings by providing coverings that withstand higher operational temperatures than stainless steel, are wear and snag resistant, can be a separate seal layer or as a portion of an integrated seal construction, can accommodate tight curvature changes to achieve complex shapes without wrinkling or buckling, and can be joined in the knitting process, sewed or mechanically fastened, without the need for welding.

First claim

What is claimed is:

1. A method of forming a thermal sealing member, comprising:
combining an intermediate wrap member with an outer abrasion resistant wrap member,
wherein the intermediate wrap member comprises one or more layers of a ceramic-based fiber material;
wherein the ceramic-based fiber material is a ceramic-based knit fabric, comprising:
a continuous ceramic strand; and
a continuous load-relieving process aid strand, wherein the continuous ceramic strand is served around the continuous load-relieving process aid strand;

wherein the outer abrasion resistant wrap member comprises one or more layers of a single-layer metal alloy knit fabric formed by knit loops of a first metal alloy wire; and
wherein the single-layer metal alloy knit fabric can withstand temperatures greater than or equal to 1,000 degrees Fahrenheit (538 degrees Celsius).

2. The method of claim 1 , wherein the first metal alloy wire is constructed of a nickel-chromium superalloy.

3. The method of claim 1 , wherein the first metal alloy wire has a diameter from about 0.003 inches (0.0762 millimeters) to about 0.007 inches (0.1778 millimeters).

4. The method of claim 1 , wherein the single-layer metal alloy knit fabric has between 3 and 10 wales per centimeter and between 3 and 10 courses per centimeter.

5. The method of claim 1 , wherein the single-layer metal alloy knit fabric is constructed using a flat knitting technique.

6. The method of claim 1 , wherein the single-layer metal alloy knit fabric is formed into a tubular structure using a tubular knitting technique.

7. The method of claim 1 , wherein the first metal alloy wire is knit in a soft-tempered state.

8. The method of claim 7 , wherein the first metal alloy wire is heat hardened after a final shape of the single-layer metal alloy knit fabric is achieved.

9. The method of claim 1 , wherein the continuous load-relieving process aid strand comprises a second metal alloy wire constructed of a material selected from a nickel-chromium based alloy, a nickel-chromium-molybdenum based alloy, aluminum, and stainless steel.

10. The method of claim 9 , wherein the continuous ceramic strand comprises one or more inorganic fibers selected from thoria-silica metal (III) oxide fibers, zirconia silica fibers, alumina-silica fibers, alumina-chromia-metal, and alumina-boria-silica fibers.

11. The method of claim 1 , further comprising adding an insulation material to the intermediate wrap member.

12. The method of claim 1 , further comprising adding a core member constructed of a resilient material having spring-like properties.

13. The method of claim 1 , wherein the thermal sealing member is selected from an M-shaped double-blade bulb seal, an omega-shaped bulb seal, and a p-shaped bulb seal.

14. The method of claim 1 , further comprising:
feeding the first metal alloy wire through a single material feeder of a knitting machine; and
knitting the first metal alloy wire to form the single-layer metal alloy knit fabric.

15. A method of forming a thermal sealing member, comprising:
forming an intermediate wrap member, comprising:
simultaneously feeding a continuous ceramic strand and a continuous load-relieving process aid strand through a first material feeder and a first metal alloy wire through a second material feeder; and
concurrently knitting the continuous ceramic strand, the continuous load-relieving process aid strand and the first metal alloy wire to form a single-layer ceramic-based knit fabric, wherein the first metal alloy wire is in a soft-tempered state;

forming an outer abrasion resistant wrap member, comprising:
feeding a second metal alloy wire through a single material feeder; and
knitting the second metal alloy wire to form one or more layers of a single-layer metal alloy knit fabric formed by knit loops of the second metal alloy wire, wherein the single-layer metal alloy knit fabric can withstand temperatures greater than or equal to 1,000 degrees Fahrenheit (538 degrees Celsius); and

combining the intermediate wrap member with the outer abrasion resistant wrap member.

16. The method of claim 15 , wherein the second metal alloy wire is constructed of a nickel-chromium superalloy.

17. The method claim 16 , wherein the second metal alloy wire has a diameter from about 0.003 inches (0.0762 millimeters) to about 0.007 inches (0.1778 millimeters).

18. The method of claim 15 , wherein the continuous load-relieving process aid strand comprises a third metal alloy wire constructed of a material selected from a nickel-chromium based alloy, a nickel-chromium-molybdenum based alloy, aluminum, and stainless steel.

19. The method of claim 18 , wherein the continuous ceramic strand comprises one or more inorganic fibers selected from thoria-silica metal (III) oxide fibers, zirconia silica fibers, alumina-silica fibers, alumina-chromia-metal, and alumina-boria-silica fibers.

20. A method of forming a thermal sealing member, comprising:
combining an intermediate wrap member with an outer abrasion resistant wrap member,
wherein the intermediate wrap member comprises one or more layers of a ceramic-based fiber material;
wherein the outer abrasion resistant wrap member comprises one or more layers of a single-layer metal alloy knit fabric formed by knit loops of a first metal alloy wire;
wherein the single-layer metal alloy knit fabric can withstand temperatures greater than or equal to 1,000 degrees Fahrenheit (538 degrees Celsius);
wherein the first metal alloy wire is knit in a soft-tempered state; and
wherein the first metal alloy wire is heat hardened after a final shape of the single-layer metal alloy knit fabric is achieved.

21. A method of forming a thermal sealing member, comprising:
combining an intermediate wrap member with an outer abrasion resistant wrap member,
wherein the intermediate wrap member comprises one or more layers of a ceramic-based fiber material;
wherein the outer abrasion resistant wrap member comprises one or more layers of a single-layer metal alloy knit fabric formed by knit loops of a first metal alloy wire; and
wherein the single-layer metal alloy knit fabric can withstand temperatures greater than or equal to 1,000 degrees Fahrenheit (538 degrees Celsius); and

adding an insulation material to the intermediate wrap member.

Assignees

• Boeing Co

Inventors

• Stewart Tiffany A
• Chappell Amoret M
• Henry Christopher P

Classifications

• D04B1/225

  Elongated tubular articles of small diameter, e.g. coverings or reinforcements for cables or hoses · CPC title

• C22F1/10 Primary

  of nickel or cobalt or alloys based thereon · CPC title

• D04B1/14 Primary

  Other fabrics or articles characterised primarily by the use of particular thread materials · CPC title

• D10B2505/06

  Packings, gaskets, seals · CPC title

• B21F27/12

  Making special types or portions of network by methods or means specially adapted therefor · CPC title