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A region of an airfoil to be protected from accreted ice is heated to reduce the strength of the bond between the ice and the airfoil, and is mechanically deformed to shed the accreted ice after the bond has been sufficiently weakened. Heating ceases before substantial water runback is generated. Th

A region of an airfoil to be protected from accreted ice is heated to reduce the strength of the bond between the ice and the airfoil, and is mechanically deformed to shed the accreted ice after the bond has been sufficiently weakened. Heating ceases before substantial water runback is generated. The mechanical deformation and the cessation of heating occur approximately simultaneously.

대표청구항 ▼

1. A method of deicing a protected region of an airfoil surface, comprising the following steps: using a heater to heat the protected region of the surface to a temperature that will melt ice at its interface with the protected region;ceasing to heat the protected region of the surface once said tem

1. A method of deicing a protected region of an airfoil surface, comprising the following steps: using a heater to heat the protected region of the surface to a temperature that will melt ice at its interface with the protected region;ceasing to heat the protected region of the surface once said temperature has been reached; andapproximately simultaneously with said ceasing step, mechanically deforming the heater and the protected region of the surface to shed ice accreted thereon. 2. A method of deicing a protected region of an airfoil surface, comprising the following steps: using a heater to heat the protected region of the surface to a temperature that will acceptably reduce the force of adhesion of ice to the protected region of the surface;ceasing to heat the protected region of the surface once said temperature has been reached; andapproximately simultaneously with said ceasing step, mechanically deforming the heater and the protected region of the surface to shed ice accreted thereon. 3. A method of deicing a protected region of an airfoil surface, comprising the following steps: using a heater to electro-thermally heat the protected region of the surface to a temperature that will acceptably reduce the force of adhesion of ice to the protected region of the surface;ceasing to heat the protected region of the surface once said temperature has been reached; andapproximately simultaneously with said ceasing step, mechanically deforming the heater and the protected region of the surface to shed ice accreted thereon. 4. A method of deicing a protected region of an airfoil surface, comprising the following steps: using a heater to electro-thermally heat the protected region of the surface to a temperature that will melt ice at its interface with the airfoil;ceasing to heat the protected region of the surface once said temperature has been reached; andapproximately simultaneously with said ceasing step, mechanically deforming the heater and the protected region of the surface to shed ice accreted thereon. 5. The method of claim 4, wherein said heating step is initiated by a crew member. 6. The method of claim 4, wherein said heating step is initiated automatically. 7. The method of claim 4, wherein said ceasing step is carried out automatically at the end of a period of time that is determined based upon true airspeed and outside air temperature. 8. The method of claim 4, wherein said ceasing step is carried out automatically based upon actual temperature of the protected region. 9. A method of deicing a protected region of the aerodynamic surface of an airfoil in flight when the airfoil is moving at a known true airspeed (TAS) through air at a known outside air temperature (OAT), comprising the following steps: obtaining the TAS of the airfoil;obtaining the OAT of the air;using the obtained TAS and OAT to determine a period of time during which the protected region of the aerodynamic surface is to be heated;heating the protected region of the aerodynamic surface for said determined period of time;momentarily flexing the protected region of the aerodynamic surface at approximately the end of said determined period of time; andrepeating said heating and flexing steps. 10. The method of claim 9, wherein said heating step is carried out using electro-thermal heating. 11. A method of deicing a protected region of an airfoil surface, comprising the following steps: delivering heat to the protected region of the surface in such a quantity as will under worst-case conditions melt ice at its interface with the protected region;ceasing to heat the protected region of the surface once such quantity of heat has been delivered; andapproximately simultaneously with said ceasing step, mechanically deforming the protected region of the surface to shed ice accreted thereon. 12. A method of deicing a protected region of an airfoil surface, comprising the following steps: delivering heat to the protected region of the surface in such a quantity as will under worst-case conditions acceptably reduce the force of adhesion of ice to the protected region of the surface;ceasing to heat the protected region of the surface once such quantity of heat has been delivered; andapproximately simultaneously with said ceasing step, mechanically deforming the protected region of the surface to shed ice accreted thereon. 13. A method of deicing a protected region of an airfoil surface, comprising the following steps: using an electro-thermal heater to deliver heat to the protected region of the surface in such a quantity as will under worst-case conditions acceptably reduce the force of adhesion of ice to the protected region of the surface;ceasing to heat the protected region of the surface once said quantity of heat has been delivered; andapproximately simultaneously with said ceasing step, mechanically deforming the heater and the protected region of the surface to shed ice accreted thereon. 14. A method of deicing a protected region of an airfoil surface, comprising the following steps: using an electro-thermal heater to deliver heat to the protected region of the surface in such a quantity as will under worst-case conditions melt ice at its interface with the airfoil;ceasing to heat the protected region of the surface once said quantity of heat has been delivered; andapproximately simultaneously with said ceasing step, mechanically deforming the heater and the protected region of the surface to shed ice accreted thereon. 15. A method of deicing a protected region of the aerodynamic surface of an airfoil in flight when the airfoil is moving at a known true airspeed (TAS) through air at a known outside air temperature (OAT), comprising the following steps: obtaining the TAS of the airfoil;obtaining the OAT of the air;using the obtained TAS and OAT to determine a quantity of heat to be delivered to the protected region of the aerodynamic surface under worst-case conditions;heating the protected region of the aerodynamic surface for period of time required to deliver such quantity of heat thereto;momentarily flexing the protected region of the aerodynamic surface at approximately the end of said determined period of time; andrepeating said heating and flexing steps. 16. A method of protecting a protected region of an airfoil surface from excessive ice accumulation, comprising the following steps: allowing an acceptable thickness of ice to accrete on the protected region of the surface;delivering heat to the protected region of the surface in such a quantity as will under worst-case conditions melt ice accreted thereon;ceasing the delivery of heat to the protected region of the surface once such quantity of heat has been delivered; andapproximately simultaneously with said ceasing step, mechanically deforming the protected region of the surface to shed ice accreted thereon. 17. A method of protecting a protected region of an airfoil surface from excessive ice accumulation, comprising the following steps: allowing an acceptable thickness of ice to accrete on the protected region of the surface;delivering heat to the protected region of the surface in such a quantity as will under worst-case conditions acceptably reduce the force of adhesion of ice accreted thereon;ceasing the delivery of heat to the protected region of the surface once such quantity of heat has been delivered; andapproximately simultaneously with said ceasing step, mechanically deforming the protected region of the surface to shed ice accreted thereon.