|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|인용정보||피인용 횟수 : 9 인용 특허 : 1|
A porous aircraft skin for wetted areas of an aircraft employed in conjunction with a suction system of the aircraft to draw air inwardly through pores of said skin for laminar flow control. The porous skin is compliant and includes a thin outer skin with fine pores bonded to a lower substantially thicker coarser pore compliant skin with the thicker skin in turn bonded to the structural skin of the aircraft. Vacuum chambers beneath the aircraft structural skin receive air sucked through the porous compliant skin and through communicating holes of the str...
A suction surface laminar flow aircraft capable of fixed-wing flight constructed so that the interior wing root of the aircraft acts as a suction chamber for the suction porous skin wing, and whereby a low by-pass ratio engine is immersed in the wing root suction chamber and the by-pass portion of the jet engine becomes the suction pump for the suction laminar flow control system by separating the intake air for the by-pass portion of the jet engine from the jet engine intake air by use of appropriate separate intake ducts with ram air from the leading e...