|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 7 인용 특허 : 17|
A gas turbine diffuser assembly and a method for assembling same, includes providing a loose fit between the diffuser body and the diffuser pipes. Damper members provide a snug attachment.
We claim: 1. A diffuser assembly for a gas turbine engine, the diffuser comprising: an annular diffuser body having a plurality of orifices disposed circumferentially around an outer periphery thereof, the orifices having an inner wall; a plurality of diffuser pipes each having a first end thereof received in one of the orifices adjacent the inner wall thereof; and a flexible damper member disposed between the first end and the inner wall of at least one of the orifices. 2. The diffuser assembly as claimed in claim 1 wherein the at least one orifice ...