发明申请
- 专利标题: AIRCRAFT ICE PROTECTION SYSTEM AND METHOD
- 专利标题(中): 飞机冰保护系统和方法
-
申请号: US14812610申请日: 2015-07-29
-
公开(公告)号: US20150329211A1公开(公告)日: 2015-11-19
- 发明人: David Patrick Calder , Julian Alexander Opificius , Erik Thomas Pederson , David Cenit Flosdorf
- 申请人: MRA Systems Inc. , Kelly Aerospace Thermal Systems, LLC
- 主分类号: B64D15/14
- IPC分类号: B64D15/14
摘要:
A system and method for ice protection of a component, wherein the system is adapted to be adhesively bonded to a surface of the component. The system includes a heating element layer, at least one thermally conductive adhesive layer that adhesively bonds a first side of the heating element layer to the component, an insulation layer, at least one thermally insulating adhesive layer that adhesively bonds a second side of the heating element to the insulation layer, an electrical bus bar adapted to provide a connection between a power supply and the heating element layer, and at least one temperature sensor.
公开/授权文献
- US09309001B2 Aircraft ice protection system and method 公开/授权日:2016-04-12
信息查询