|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/796; 060/797; 060/798; 060/799; 403/144|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 4 인용 특허 : 17|
An exemplary turbine engine link assembly includes a link extending longitudinally from a rod end and terminating at a hemispherical end. The rod end is secured to an engine liner or an engine casing. The hemispherical end is biased toward a corresponding hemispherical recess in the engine liner or in the other of the engine liner or the engine casing.
1. A turbine engine assembly comprising: a first attachment structure secured directly to an engine liner;a second attachment structure secured directly to an engine casing, wherein the engine liner and the engine casing together establish a bypass flowpath of a turbine engine;a link having a rod portion extending longitudinally from a hemispherical end portion and terminating at a rod end portion, the hemispherical end portion received within a recess defined by the first attachment structure, the rod end portion secured relative to the second attachmen...