Deicer boots having elastomer fibers with aligned carbon allotrope materials
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B29C-070/14
B64D-015/16
B29C-070/18
B29C-070/42
D01D-005/00
B29K-075/00
B29K-105/08
B29K-105/16
B29K-505/02
B29K-507/04
B29L-031/30
출원번호
US-0140024
(2016-04-27)
등록번호
US-9994326
(2018-06-12)
발명자
/ 주소
Hu, Jin
출원인 / 주소
Goodrich Corporation
대리인 / 주소
Kinney & Lange, P.A.
인용정보
피인용 횟수 :
0인용 특허 :
19
초록▼
A deicer boot includes an aircraft structure and an outer layer. The outer layer includes a plurality of elastomer fibers and a carbon allotrope material. The carbon allotrope material is aligned with at least one elastomer fiber belonging to the plurality of elastomer fibers. A method of forming a
A deicer boot includes an aircraft structure and an outer layer. The outer layer includes a plurality of elastomer fibers and a carbon allotrope material. The carbon allotrope material is aligned with at least one elastomer fiber belonging to the plurality of elastomer fibers. A method of forming a layer of a deicer boot includes aligning a carbon allotrope material with a first elastomer fiber, joining the first elastomer fiber with a plurality of additional elastomer fibers to form a non-woven fiber fabric, and incorporating the non-woven fiber fabric into a sheet.
대표청구항▼
1. A deicer boot comprising: an aircraft structure; andan outer layer comprising: a plurality of elastomer fibers; anda carbon allotrope material within at least one elastomer fiber belonging to the plurality of elastomer fibers, wherein the carbon allotrope material is aligned with the at least one
1. A deicer boot comprising: an aircraft structure; andan outer layer comprising: a plurality of elastomer fibers; anda carbon allotrope material within at least one elastomer fiber belonging to the plurality of elastomer fibers, wherein the carbon allotrope material is aligned with the at least one elastomer fiber. 2. The deicer boot of claim 1, further comprising: an inner elastomer layer located between the outer layer and the aircraft structure;a carcass layer having inflation tubes and located between the aircraft structure and the inner layer; anda bond layer adjacent the carcass layer and configured to attach the carcass layer to the aircraft structure. 3. The deicer boot of claim 1, wherein the carbon allotrope material is selected from the group consisting of carbon nanotubes, graphene, graphite, carbon black and combinations thereof. 4. The deicer boot of claim 1, wherein the elastomer fibers comprise a material selected from the group consisting of neoprene, polyurethane, natural rubbers and combinations thereof. 5. The deicer boot of claim 1, wherein the plurality of elastomer fibers and the carbon allotrope material form a non-woven electrospun fiber fabric sheet. 6. The deicer boot of claim 1, further comprising an icephobic material located on the outer layer. 7. The deicer boot of claim 6, wherein the icephobic material is selected from the group consisting of siloxanes, fluorocarbons, polycarbosiloxanes, polysiloxanes, and combinations thereof. 8. The deicer boot of claim 1, wherein the outer layer further comprises: aluminum flake. 9. The deicer boot of claim 8, wherein the aluminum flake is aligned with at least one elastomer fiber belonging to the plurality of elastomer fibers. 10. The deicer boot of claim 5, wherein the non-woven electrospun fiber fabric sheet further comprises a non-electrospun elastomer. 11. The deicer boot of claim 10, wherein the non-woven electrospun fiber fabric sheet further comprises an additive selected from the group consisting of antioxidants, carbon black and combinations thereof. 12. A method of forming a layer of a deicer boot, the method comprising: aligning a carbon allotrope material within a first elastomer fiber with the first elastomer fiber;joining the first elastomer fiber with a plurality of additional elastomer fibers to form a non-woven fiber fabric; andincorporating the non-woven fiber fabric into a sheet. 13. The method of claim 12, wherein the carbon allotrope material is selected from the group consisting of carbon nanotubes, graphene, graphite, carbon black and combinations thereof. 14. The method of claim 12, wherein aligning the first elastomer fiber with the carbon allotrope material is carried out by electrospinning an elastomer solution containing the first carbon allotrope material. 15. The method of claim 12, wherein incorporating the non-woven fabric into the sheet comprises fusing or melting the non-woven fabric to form the sheet. 16. The method of claim 12, further comprising: applying an icephobic material to the sheet, wherein the icephobic material is selected from the group consisting of siloxanes, fluorocarbons, polycarbosiloxanes, polysiloxanes, and combinations thereof. 17. The method of claim 12, further comprising: aligning a first elastomer fiber with aluminum flake material by electro spinning an elastomer solution containing the aluminum flake material. 18. The method of claim 12, wherein the sheet is a neoprene or polyurethane sheet, and wherein incorporating the non-woven fabric into the sheet comprises embedding the non-woven fabric into the sheet. 19. The method of claim 12, wherein the sheet is a polyurethane elastomer sheet having aluminum flake, and wherein incorporating the non-woven fabric into the sheet comprises embedding the non-woven fabric into the sheet. 20. A deicer boot comprising: an aircraft structure; andan outer layer comprising: a plurality of elastomer fibers; andaluminum flake material within at least one elastomer fiber belonging to the plurality of elastomer fibers, wherein the aluminum flake is aligned with the at least one elastomer fiber.
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이 특허에 인용된 특허 (19)
Shah, Tushar K.; Malecki, Harry C.; Adcock, Daniel Jacob, CNT-based resistive heating for deicing composite structures.
Webster Steven D. (2092 Wimpole Ct. Roanoke TX 76262) Williams Randy B. (2711 Edinboro Dr. Arlington TX 76012), Electromagnetic wave attenuating and deicing structure.
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