|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/752; 431/114; 060/748; 060/725; 060/798; 060/799|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 20 인용 특허 : 30|
A multi-axial pivoting liner within the combustion system of a turbine engine allows the system to work with minimum thermal interference, especially during system operation at transient conditions, by allowing the liner to pivot and slide about its centerline and relative to the turbine scroll. The pivoting liner has the ability to control and minimize air leakage from part to part, for example, from the liner to the turbine scroll and liner to the surrounding structures, during various operating conditions. Additionally, the liner provides for easy as...
We claim: 1. A liner for a turbine engine, comprising: a lower joint that movably connects said liner with a combustion gas output receiving device; an upper joint that movably attaches a housing to said liner, said upper joint formed by contacting two substantially spherical surfaces; and said lower joint providing angular and axial axes of movement for said liner with respect to said combustion gas output receiving device, and said upper joint providing angular axes of movement for said liner with respect to said housing. 2. The liner according...