|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/039.38 ; 60/039.39 ; 60/039.78 ; 60/039.81 ; 431/01|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 45 인용 특허 : 9|
A pulse detonation engine has a pulse ignition system, a plurality of detonation chambers (15), an oxygen source (33), and a fuel source (35). The oxygen source and the fuel source supply oxygen and fuel, respectively, to both the pulse ignition system and to the detonation chambers. The pulse ignition system creates detonation waves by igniting a first series of fuel mixtures inside a plurality of igniter tubes (39) equal to the number of detonation chambers (15). One detonation wave is delivered by each igniter tube into each detonation chamber for ign...
[ We claim:] [1.] A pulse detonation engine, comprising in combination:an oxygen source;a fuel source;a detonation chamber having an upstream end, an open downstream end, an oxygen port and a fuel port which are supplied with oxygen and fuel from the oxygen source and the fuel source, respectively, and a detonation wave port adjacent to the upstream end;a pulse detonation igniter tube having a downstream end communicating with the detonation wave port of the detonation chamber;an oxygen valve means for admitting oxygen from the oxygen source into the ign...