Title:
局所化されたプライ絶縁を伴う熱可塑性航空機構造および航空機構造を形成する方法
Document Type and Number:
Japanese Patent JP7268112
Kind Code:
B2
Abstract:
A composite wingbox structure formed of reinforced thermoplastic. The composite includes carbon fiber reinforcement and a plurality of insulation elements to localize the heat formed during the process of manufacturing the structure. The process of manufacturing the wingbox includes the steps of interleaving a series of insulations elements within a plurality of laminae and consolidating the insulation elements and laminae to form a laminate. The laminate is then aligned with a support structure such that the insulation elements overlie the supports structure. The laminate is then fused to the support structure using a non-contact heating process, such as inductive welding.
Inventors:
Calder, Mark, A.
Ellis, John, F.
Denison, William, David
Wimmer, Martin, A.
Stone, Earl, El., The Third
Ellis, John, F.
Denison, William, David
Wimmer, Martin, A.
Stone, Earl, El., The Third
Application Number:
JP2021173927A
Publication Date:
May 02, 2023
Filing Date:
October 25, 2021
Export Citation:
Assignee:
Carvone Aerospace (Foundation), LLC
International Classes:
B64C3/22; B29C65/46; B64C1/00; B64C3/18
Domestic Patent References:
| JP2000356358A | ||||
| JP2011517635A | ||||
| JP3065317A |
Foreign References:
| US3768760 |
Attorney, Agent or Firm:
Taro Yaguchi
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