|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||701/04 ; 701/03 ; 701/07 ; 701/014 ; 244/012.1 ; 244/201 ; 244/219 ; 244/203 ; 73/178R ; 73/178T ; 180/116 ; 180/117|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 20 인용 특허 : 37|
A method and apparatus for measuring the lift generated by airfoils of an aircraft. This real-time analysis is accomplished by measuring a differential pressure between the upper and lower lift surfaces of the airfoils. The system comprises the steps of: a) measuring an actual differential pressure between the upper and lower lift surfaces for a given aircraft speed, b) transmitting this actual differential pressure measurement to a computer, c) comparing the actual differential pressure measurement with an optimal pressure differential for the same airc...
[ I claim:] [1.] Apparatus for monitoring and controlling flight of an aircraft comprising:an upper port in an upper surface of a wing portion;a lower port in a lower surface of a wing portion;an upper tube having a first end and a second end, the first end located at the upper port;a lower tube having a first end and a second end, the first end located at the lower port; anda differential pressure sensor having a first side and a second side, the first side connected to the second end of the upper tube and the second side connected to the second end of ...