|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/204 ; 60/247 ; 60/3978 ; 431/1|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 62 인용 특허 : 0|
A pulse detonation engine has a detonation chamber with a sidewall. At least two fuel ports are located in the sidewall, spaced longitudinally apart from each other. An oxygen fuel mixture is introduced into the forward port and detonated. This creates a detonation wave which propagates with an air fuel mixture introduced into the rearward fuel port. After the detonation, purge air passes through the chamber before the next detonation. A rotating sleeve valve mounted around the detonation opens and closes the fuel ports as well the purge ports.
A pulse detonation apparatus, comprising in combination: a detonation chamber having a sidewall, a longitudinal axis, a forward end and a rearward end which is open; first and second detonation chamber ports located in the sidewall, spaced apart from each other in a longitudinal direction, with the first detonation chamber port being located closer to the forward end than the second detonation chamber port; oxygen fuel valve means for introducing into the first detonation chamber port a discrete oxygen fuel mixture containing a fuel and a substantially h...