Title:
Integrated surface thermal management system
Document Type and Number:
Japanese Patent JP6352187
Kind Code:
B2
Abstract:
Systems to apply heat to an aircraft surface are disclosed. In some embodiments, heaters are embedded in a composite structure of an aircraft. In one embodiment, a composite aircraft structure comprises a base comprising a plurality of resin impregnated plies, a heating layer adjacent the base, wherein the heating layer comprises at least one heater, an adhesive layer adjacent the heating layer, a lightning protection layer adjacent the heating layer, and an exterior surface layer adjacent the lightning protection layer. Other embodiments may be described.
Inventors:
Almatrio, andrew
Birch, Daniel A.
Justin Nida
Olivier, Roland J.
Schencol, Jared
Loftis, Richard J.
Birch, Daniel A.
Justin Nida
Olivier, Roland J.
Schencol, Jared
Loftis, Richard J.
Application Number:
JP2014530665A
Publication Date:
July 04, 2018
Filing Date:
July 10, 2012
Export Citation:
Assignee:
The Boeing Company
International Classes:
B64D15/14; B32B5/28; B32B7/02; B64D45/02
Foreign References:
| CA2740524A1 | ||||
| CN102007038A | ||||
| EP1845018A2 | ||||
| WO2007107732A1 | ||||
| US20110006049 |
Attorney, Agent or Firm:
Sonoda Yoshitaka
Kobayashi Yoshinori
Kobayashi Yoshinori