|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/207 ; 60/211 ; 60/225 ; 60/247 ; 60/245 ; 60/039.76|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 44 인용 특허 : 11|
A pulse detonation rocket engine, having at least two detonation chambers. The rocket propelled vehicle includes at least one fuel delivery system in fluid communication with each of the at least two detonation chambers, and at least one oxidant delivery system in fluid communication with the detonation chambers, along with fast-acting valves to inject fuel and oxidant controlledly into the chambers. An ignitor in each of the detonation chambers intermittently initiates detonation of a fuel and oxidant mixture in the chamber, in a controlled cycle, to pr...
[ The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:] [1.] A method of sequentially detonating a fuel and oxidant mixture in a rocket engine, the method comprising:(a) commencing a pulse detonation cycle by creating a detonable fuel and oxidant mixture in a first of a plurality of detonation chambers of a rocket engine, by controlling the amount of fuel supplied by a fuel injector, and supplying an amount of oxidant sufficient to produce a detonable fuel-oxidant mixture to the chamber;(b) ignit...