|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||G01P-013/00 B64D-043/02 G05D-001/10 G01C-021/20 G01P-005/10|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 9|
Embodiments of air flow sensing systems are provided herein. In some embodiments, one or more sensors are positionable on an aircraft and dimensioned and arranged to measure vector components of airflow velocity having at least one of a transverse or streamwise direction relative to a flight direction of the aircraft. In some embodiments, the one or more sensors are positioned in front of an aircraft wing and distributed as an array of sensors along the span of the aircraft wing.
1. An air flow sensing system, comprising: a differential airflow probe positionable on an aircraft, the differential airflow probe having a streamwise direction and being dimensioned and arranged to measure airflow velocity vector components at least one of orthogonal or transverse to a flight direction of the aircraft and defining a first airflow channel and a second airflow channel symmetrically oriented relative to the streamwise direction, wherein each airflow channel includes a respective input port defining an airflow path through an opening and e...