|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 1 인용 특허 : 23|
A curved diffuser (210) in a gas turbine engine (201) directs a primary portion of air flow from a compressor (202) through a curved discharge opening (213) into a plenum (220). The curved diffuser (210) also comprises ports (217) through which a secondary portion of air passes into confined space (225) that is defined in part by a pressure boundary element that may be comprised of at least one plate (222) or at least one conduit (306). The at least one plate (222) and the at least one conduit (306) respectively comprise apertures (246, 312) through whic...
I claim as my invention: 1. A gas turbine engine comprising:a. an air compressor;b. a plurality of combustion chambers, each comprising an intake end and an outlet end, and connected in parallel with respect to airflow;c. a plurality of transitions, each comprising an inboard side, two lateral sides, and an outboard side, and each associated with a respective combustion chamber, providing fluid communication between the respective outlet end and an entrance port of a turbine;d. a curved diffuser in fluid communication between the compressor and a plenum ...