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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0725964 (1985-04-22) |
발명자 / 주소 |
|
출원인 / 주소 |
|
인용정보 | 피인용 횟수 : 4 인용 특허 : 4 |
In one form of the invention, different airflows across a temperature sensor in an aircraft are maintained during different flight conditions. A first airflow is generated during takeoff by a pressure differential existing between two surfaces of the aircraft. A second airflow is maintained during c
In an aircraft engine nacelle, the improvement comprising: (a) a temperature sensor; (b) means for maintaining a first airlow across the temperature sensor during takeoff; and (c) means for maintaining a second airflow across the temperature sensor during cruise which is less than the first airflow.
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