|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/134D; 244/134A; 244/134B|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 25|
A structure for use with an electrothermal heating element is disclosed comprising a heating element contained in a mat and heater supports attached to one surface of the mat. The heating element is disposed between the skin and internal structure of an aircraft with the heater supports disposed toward the internal structure thereof. The heater supports maintain an insulating layer of air between the mat and the internal structure of the aircraft.
1. An electrothermal heater for a skin of an aircraft, the electrothermal heater comprising: an electrothermal heating element;a mat encasing the electrothermal heating element, the mat comprising a first and a second sheet; anda thermal barrier attached to the second sheet of the mat;wherein the thermal barrier comprises a plurality of rigid support members for maintaining a layer of air between the second sheet and the aircraft. 2. The electrothermal heater of claim 1 wherein the thermal barrier is disposed adjacent to an internal structure of the airc...