|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/053R; 060/226.3; 060/039.163|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 43|
A gas turbine engine includes a spool along an engine centerline axis which drives a gear train, said spool includes a low stage count low pressure turbine.
1. A gas turbine engine comprising: a gear train defined along an engine centerline axis;a spool along said engine centerline axis which drives said gear train, said spool includes a low stage count low pressure turbinea fan rotatable at a fan speed about the centerline axis and driven by the low pressure turbine through the gear train, wherein the fan speed is less than a speed of the low pressure turbine;a core surrounded by a core nacelle defined about the engine centerline axis;a fan nacelle mounted at least partially around said core nacelle to defi...