|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 31|
A parasitic drag induced boundary layer reduction system and methods for reducing the boundary layer on aircraft, vehicles, and structure. The system may include a suction generator configured to utilize parasitic drag in reducing boundary layer effect and enhancing laminate flow. The suction generator may include at least one of a suction port on a rearward facing surface of an aircraft, a suction vane on each wing of the aircraft, a wingtip vane on each wing of the aircraft, and a slotted tail section on a tail of the aircraft. The system may also incl...
1. A parasitic drag induced boundary layer reduction system for an aircraft comprising at least two wings, comprising: a suction generator configured to induce parasitic drag so as to produce suction used to lessen boundary layer effect and improve laminar airflow about the aircraft, the suction generator comprising at least one suction port on a rearward facing surface of a fuselage of the aircraft behind the at least two wings on a surface of the fuselage that also delimits a bottom surface of the aircraft, or on a tail section of the aircraft behind t...