|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 5 인용 특허 : 9|
A balanced thrust vectoring system for an aircraft designed to provide even weight distribution, simple thrust vectoring, and hover stability. The system includes a main diverter that connects to a jet output port. Located inside the diverter is a 4 way splitter that divides the diverter into four equal volumes. Attached to the diverter and adjacent to the two upper volumes are two front upward extending ducts. Attached to the diverter and adjacent to the two lower volumes are two rear upward extending ducts. Each duct includes an upper bend that and dia...
I claim: 1. A lift vehicle with a thrust vectoring system to generate even weight distribution, simple thrust vectoring, and hover stability, said lift vehicle, comprising:a. a lift vehicle with an air flow thrust generator mounted therein, said lift vehicle having a vertical and horizontal center gravity axis, said air flow thrust generator has an output exhaust port;b. a hollow, thrust diverter having a longitudinal axis that is longitudinally aligned with said output exhaust port on said air flow thrust generator;c. a stationary four way splitter loca...