|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/747; 060/740; 431/278|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 30 인용 특허 : 17|
An axially staged combustion system is provided for a gas turbine engine comprising a main body structure having a plurality of first and second injectors. First structure provides fuel to at least one of the first injectors. The fuel provided to the one first injector is adapted to mix with air and ignite to produce a flame such that the flame associated with the one first injector defines a flame front having an average length when measured from a reference surface of the main body structure. Each of the second injectors comprising a section extending ...
What is claimed is: 1. An axially staged combustion system for a gas turbine engine comprising: a main body structure having a plurality of first injectors and a plurality of second injectors, compressed air being provided to said first injectors; first structure to provide fuel to each of said first injectors, said fuel provided to said first injectors being adapted to mix with the compressed air provided to said first injectors and ignite to produce a flame such that the flame associated with said first injectors defines a flame front that is axially ...