|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/55 ; 244/53B ; 244/73R ; 60/225|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 25 인용 특허 : 2|
A propulsion system for an aircraft capable of hypersonic flight combines a turbo-jet with a ramjet which are so arranged that the ramjet or jets are located directly adjacent to the aircraft body while the turbo-jet or jets are located away from the aircraft body so that the ramjet or jets is placed between the turbo-jets and the body. This arrangement makes the turbo-jets much more accessible for maintenance and exchange work. Both types of engines have a common air intake which is provided with flaps capable of guiding the body boundary layer through ...
An air breathing propulsion system for hypersonic flight of an aircraft having a body, comprising ramjet means mounted in a location directly next to said body, turbo-jet means mounted away from said body next to said ramjet means, so that said ramjet means are located between said body and said turbo-jet means, said ramjet means and said turbo-jet means having separate thrust nozzles, common air intake means arranged for supplying air to said ramjet means and to said turbo-jet means, first flap means for controlling an air intake of said common air inta...