|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 20|
A gas turbine engine includes a nosecone assembly attached to a gas turbine engine. The nosecone assembly includes a support structure and a nosecone attached to the support structure. The nosecone includes at least a first tool hole extending through the nosecone. The first tool hole is structurally reinforced.
1. A gas turbine engine comprising: a nosecone assembly attached to the gas turbine engine, the nosecone assembly comprising: a support structure;a nosecone attached to the support structure, the nosecone comprising: a tip end;an aft end opposite the tip end; andat least a first tool hole extending through the nosecone, wherein the first tool hole is positioned on or nearer the tip end than the aft end; anda first reinforcing structure joined to the nosecone at the first tool hole. 2. The gas turbine engine of claim 1, wherein the first reinforcing struc...