|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/207 ; 244/198 ; 416/20R ; 416/90A|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 6 인용 특허 : 5|
A non-moving fluid thrust deflector and force augmentor is disclosed for aerodynamic and hydrodynamic vehicles and devices. When the deflector is utilized in an aerodynamic application and in conjunction with a thrust producer and a plenum, upon pressure initiation within the plenum, a jet sheet issues and remains attached to a specially designed wing having a rounded trailing edge by balancing reduced static pressure with centrifugal force, and thus provides a controlled resultant force or thrust in some direction other than that corresponding to the or...
A thrust deflection, thrust reversal and force augmentation device for an aircraft capable of short takeoff and landing, and vertical takeoff and landing, comprising; an aircraft wing; a thrust engine mounted on said wing with the exhaust from said engine traveling over the upper surface of said wing; a plenum inside said wing having an inlet connected to a source of gas pressure and an outlet in the trailing edge of said wing; said outlet being formed as a slot means between an upper portion and a lower portion; said upper portion being a part of the up...