|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/0122; 244/0230C; 244/052|
|발명자 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 24 인용 특허 : 15|
The present embodiments and associated methods provide for a progressive 3-axis multi-variable propulsion vectoring aerial and spaceborne vehicle. One embodiment of the vehicle is comprised of top and side air intakes, a curved sphenoid air accumulator, a compressor section, a diffuser, a plurality of fuel burner cans, a turbine section, a gas plenum, top, side, and bottom exhaust ports, propellant burner cans, gas plenum iris, an onboard flight control computer, and top, side, and bottom exhaust port doors. Combustion gasses are produced which are direc...
1. A vehicle adapted for flight, comprising:an airframe comprising a top, side, and bottom; at least one top exhaust port on the airframe top; at least one side exhaust port on the airframe side; at least one bottom exhaust port on the airframe bottom, the top, side and bottom exhaust ports each comprising a door; a gas plenum in fluid communication with the exhaust ports; a gas plenum door; at least one air intake located on the airframe, the at least one air intake comprising a door; a fuel-burning gas-generating means adapted to produce gas, the fuel-...