|국가/구분||United States(US) Patent 등록|
|§371/§102 date||20120822 (20120822)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 8|
This invention is a packaged propellant air-induced variable thrust rocket engine that has a vast number of uses and applications for this invention. The primary purpose of the device described here is to provide a light weight, torque and vibration free thrust generator for the propulsion of aircraft. This device will facilitate the fabrication of very light weight aircraft because of the lack these forces. This device can also be used anywhere high velocity air flow and or the resulting thrust is needed. The invention uses aerodynamic principles to com...
1. A rocket motor comprising: a main airflow housing having an internal airflow space defined by internal walls of the main airflow housing, said main airflow housing having a front airflow inlet, said internal airflow space, and a rear airflow exhaust,a plurality of combustion chambers located adjacent and contiguous to the internal airflow space and releasing combustion exhaust into the internal airflow space, each one of said plurality of combustion chambers having a combustion chamber axis that has one or more oblique angles relative to a longitudina...