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1. WO2010074942 - ANTI-ICING SYSTEM AND METHOD FOR PREVENTING ICE ACCUMULATION

Publication Number WO/2010/074942
Publication Date 01.07.2010
International Application No. PCT/US2009/066997
International Filing Date 07.12.2009
IPC
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
15
De-icing or preventing icing on exterior surfaces of aircraft
12
by electric heating
H ELECTRICITY
05
ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
B
ELECTRIC HEATING; ELECTRIC LIGHTING NOT OTHERWISE PROVIDED FOR
3
Ohmic-resistance heating
B64D 15/12 (2006.01)
H05B 3/00 (2006.01)
CPC
B64D 15/12
B64D 2033/0233
H05B 2203/005
H05B 2203/013
H05B 2203/014
H05B 2203/017
Applicants
  • MRA SYSTEMS, INC. [US/US]; 103 Chesapeake Park Plaza Baltimore, MD 21220, US (AllExceptUS)
  • CALDER, David, P. [US/US]; US (UsOnly)
  • HOWARTH, Graham [US/US]; US (UsOnly)
Inventors
  • CALDER, David, P.; US
  • HOWARTH, Graham; US
Agents
  • GNIBUS, Michael, M.; General Electric Company Global Patent Operation PO Box 861, 2 Corporate Drive, Suite 648 Shelton, CT 06484, US
Priority Data
12/343,82024.12.2008US
Publication Language English (EN)
Filing Language English (EN)
Designated States
Title
(EN) ANTI-ICING SYSTEM AND METHOD FOR PREVENTING ICE ACCUMULATION
(FR) SYSTÈME ANTIGIVRAGE ET PROCÉDÉ PERMETTANT DE PRÉVENIR L'ACCUMULATION DE GLACE
Abstract
(EN)
An anti-icing system (200) includes a component surface (202) having a composite structure including a composite layer (214), aid at least one heating element (220) formed within the composite layer (214), wherein the heating element (220) is configured to provide a transfer of heat to the component surface (202).
(FR)
La présente invention concerne un système antigivrage (200) qui comprend une surface de composant (202) pourvue d'une structure composite renfermant une couche composite (214), et au moins un élément chauffant (220) formé dans la couche composite (214). L'élément chauffant (220) est conçu pour transférer de la chaleur à la surface de composant (202).
Latest bibliographic data on file with the International Bureau