|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||060/226.1; 415/208.4; 415/209.4|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 34 인용 특허 : 49|
A casing for an aircraft turbine bypass engine comprises a splitter having slots to receive and be welded to a plurality of struts extending between an outer ring and an inner hub of the casing.
The invention claimed is: 1. A casing for an aircraft turbofan bypass engine, comprising: an outer ring portion and an inner hub portion defining an airflow passage therebetween; a plurality of load-bearing hollow struts arranged in a circumferential array and extending from at least the inner hub portion to the outer ring portion, thereby mounting the inner hub portion to the outer ring portion, the struts configured to provide a primary load path between the inner hub and outer ring portion; a splitter disposed intermediate the inner hub and outer rin...