|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||G01K-013/02 G01K-001/14 G01C-021/00 G01P-005/165|
|미국특허분류(USC)||374/143 ; 374/148 ; 374/138 ; ; 73/182|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 45 인용 특허 : 22|
An aerodynamic air data sensing probe adapted for mounting to an air vehicle and capable of generating signals related to a fluid flowing relative to the air vehicle. A fluid inlet positioned on a first end of the strut faces generally transverse to the fluid flow selectively admits fluid to an internal strut cavity due to a pressure differential thereacross. In operation, the pressure differential forms between the first end surface of the aerodynamically-shaped, forward-inclined strut and probe exhaust ports. A temperature sensing element disposed in t...
An air data probe for sensing a parameter of a fluid flow moving relative to the probe, wherein the probe has an inlet aperture open to the atmosphere comprising: a strut having a leading edge, a distal portion and a base portion adapted for mounting to an air vehicle, and having the inlet aperture formed through the distal portion and facing generally transverse to the fluid flow, away from the base portion, the strut having an internal cavity fluidly coupled to the inlet aperture and an exhaust port fluidly coupled to the internal cavity; temperature s...