|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02C-003/04 F23R-003/42 F23R-003/54|
|미국특허분류(USC)||060/751; 060/752; 060/039.37; 060/760|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 0 인용 특허 : 12|
A turbine engine having a plenum for passing fluids from an outlet of a compressor to an inlet of a combustor that may increase the efficiency of the turbine engine. The turbine engine may include a combustor, a compressor positioned upstream of the combustor, a transition channel extending from the compressor to the combustor, and a shell extending between the compressor and a combustor portal and positioned around the at least one transition channel. The turbine engine may also include an axial diffusor in the shell near the at least one transition cha...
1. A turbine engine, comprising: a combustor;a compressor positioned upstream of the combustor;at least one transition channel forming at least a portion of a plenum between the compressor and the combustor;a shell forming at least a portion of the plenum between the compressor and a combustor portal of the combustor and positioned around the at least one transition channel;an axial diffusor protruding from a downstream wall of the shell toward the at least one transition channel; andwherein the axial diffusor includes a fluid flow recess in a trailing e...