Aircraft de-icing

• US 4,036,457 A
• Filed: 09/08/1975
• Issued: 07/19/1977
• Est. Priority Date: 09/10/1974
• Status: Expired due to Term

• Current Assignee: Licentia Patent-Verwaltungs-GmbH
• Original Assignee: Licentia Patent-Verwaltungs-GmbH
• Inventors: Schmedemann, Hellmuth, Volkner, Wolfgang
• Primary Examiner(s): Blix, Trygve M.
• Assistant Examiner(s): Kelmachter, Barry L.
• Application Number:
  US05/611,270
• Time in Patent Office: 680 Days
• Field of Search: 244/134 D, 244/134 R, 244/134 F, 73/336.5, 219/201, 219/209, 219/486, 340/234, 200/61.06
• US Class Current: 244/134.00D
• CPC Class Codes: B64D 15/14 controlled cyclically along length of surface
• CPC Class Codes: G05D 23/1905 associated with tele control

Abstract

In a method for de-icing aircraft surfaces by means of a plurality of electrical resistance heaters which are sequentially supplied with heating current, the delivery of current to each heater being effectuated during a succession of cycles each constituted by a heating period during which heating current is supplied to the heater and a nonheating period during which no current is supplied to the heater, thereby controlling the average current supplied to the heater, the range of ice accumulation rates to which the de-icing process can adjust is enlarged by controlling the duration of the heating periods in dependence on the temperature at the resistance heaters and by controlling the duration of the nonheating periods in dependence on the water content of the atmosphere surrounding the aircraft.

Claims

1. In a method for de-icing aircraft surfaces by means of a plurality of electrical resistance heaters which are sequentially supplied with heating current, the delivery of current to each heater being effectuated during a succession of cycles each constituted by a heating period during which heating current is supplied to the heater and a nonheating period during which no current is supplied to the heater, thereby controlling the average current supplied to the heater, the improvement comprising controlling the duration of each period of a cycle by the steps of:

measuring the temperature at the resistance heaters;

measuring the water vapor content of the atmosphere surrounding the aircraft;

adjusting the length of the heating period of each heater during each cycle as a function of the measured temperature at the resistance heaters; and

adjusting the length of the nonheating period for each heater during each cycle as a function of the measured water vapor content.

2. A method as defined in claim 1 wherein said step of measuring the water vapor content is effectuated by an ice warning system.

3. A method as defined in claim 1 wherein:

said step of measuring the temperature comprises producing an electrical signal representative of the temperature at the resistance heaters;

said step of measuring the water vapor content comprises producing an electrical signal representative of the water vapor content of the atmopshere surrounding the aircraft;

said step of adjusting the length of the heating period is carried out automatically in response to the value of the signal representative of the temperature; and

said step of adjusting the length of the nonheating period is carried out automatically in response to the value of the signal representative of the water vapor content.

4. A method as defined in claim 3 wherein said step of adjusting the length of the nonheating period comprises varying the length of the nonheating period in response to changes in the value of the electrical signal representative of water vapor content in a direction to reduce the length of the nonheating period upon the occurrence of a signal value change representing an increase in the atmospheric water vapor content.