|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||73/86168 ; 73/182 ; 165/10426 ; 219/201|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 28 인용 특허 : 0|
Aircraft probe or mast including heat pipe for indirectly heating the probe or mast thereby providing deicing. Heat for the heat pipe configured probe or mast is supplied by remote location of a heat source. The heat source may include a replacement plug in electric heater or a remote heat source such as an engine airbleed duct.
In a probe structure havng a pitot or combined pitot-static pressure tube and including an inner pressure chamber disposed within an outer shell for providing a heating chamber, means for providing indirect heating of said heating chamber comprising heating means outside said heating chamber and further including heat pipe means coupled between said heating chamber and said heating means.