Title:
一体型の加熱要素を備えた複合航空機構造
Document Type and Number:
Japanese Patent JP7234293
Kind Code:
B2
Abstract:
A heated composite structure and a method for forming a heated composite structure. The structure includes carbon fibers embedded within a thermoplastic matrix. The carbon fibers are connected with first and second electrodes that are configured to be connected with an electric source such that applying current to the electrodes causes current to flow through the embedded carbon fibers to provide resistive heating sufficient to heat the composite structure to impede formation of ice on the composite structure.
Inventors:
Hardman, Kyle, Bee.
Calder, Mark, A.
Delx, Ian, Sea.
Calder, Mark, A.
Delx, Ian, Sea.
Application Number:
JP2021083532A
Publication Date:
March 07, 2023
Filing Date:
May 18, 2021
Export Citation:
Assignee:
Carvone Aerospace (Foundation), LLC
International Classes:
B64D15/12; H05B3/03; H05B3/14
Domestic Patent References:
| JP2020516534A | ||||
| JP2015143101A | ||||
| JP2014531361A | ||||
| JP2014020371A | ||||
| JP2012525476A | ||||
| JP2001517583A |
Foreign References:
| US20180084613 | ||||
| US20140151353 |
Attorney, Agent or Firm:
Taro Yaguchi