Abstract: 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.
Type:
Grant
Filed:
July 29, 2015
Date of Patent:
April 12, 2016
Assignees:
MRA SYSTEMS INC., KELLY AEROSPACE THERMAL SYSTEMS, LLC
Inventors:
David Patrick Calder, Julian Alexander Opificius, Erik Thomas Pederson, David Cenit Flosdorf
Abstract: 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.
Type:
Grant
Filed:
November 19, 2012
Date of Patent:
November 24, 2015
Assignees:
MRA Systems, Inc., Kelly Aerospace Thermal Systems, LLC
Inventors:
David Patrick Calder, Julian Alexander Opificius, Erik Thomas Pederson, David Cenit Flosdorf
Abstract: A system and method thereof is provided for electrically heating a component. The system includes at least one heating element adapted to be adhesively bonded to a surface on the component and means for controlling flow and duration of an electrical current to the heating element from a power supply. The controlling means comprises a first heating cycle for curing an adhesive to bond the heating element to the surface and has a second heating cycle for providing ice protection to the surface.
Type:
Application
Filed:
November 27, 2012
Publication date:
January 16, 2014
Applicants:
KELLY AEROSPACE THERMAL SYSTEMS LLC, MRA SYSTEMS INC.
Inventors:
David Patrick Calder, Julian Alexander Opificius, Mark Fairbert, Erik Thomas Pederson, David Cenit Flosdorf
Abstract: 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.
Type:
Application
Filed:
November 19, 2012
Publication date:
January 16, 2014
Applicants:
Kelly Aerospace Thermal Systems, LLC, MRA SYSTEMS INC.
Inventors:
MRA Systems Inc., Kelly Aerospace Thermal Systems, LLC