|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||60/39464 ; 60/253|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 5 인용 특허 : 3|
A solid fuel turbine engine comprises a centrally disposed axially extending shaft having an annular combustion chamber disposed thereabout intermediate the ends thereof. A compressor is mounted at one end of the shaft for delivering air to the combustion chamber to provide the principal source of oxygen for combustion and a turbine is mounted at the other end of the shaft. The turbine is driven by combustion gases and drives the compressor. An annular solid fuel charge is disposed in the combustion chamber for producing combustion gases.
A solid fuel turbine engine comprising a centrally disposed axially extending rotatable compressor drive shaft, an annular combustion chamber having an inlet end and an outlet end and disposed about said compressor drive shaft intermediate the ends thereof, the annular configuration of said combustion chamber being defined by a pair of radially spaced, cylindrical walls which are concentric with one another and with said shaft, an annular solid fuel charge in said combustion chamber for producing combustion gases, an expansion chamber at the outlet end o...