|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02K-001/72 F02K-001/70 F02K-001/12|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 1 인용 특허 : 39|
A fan case of a gas turbine engine includes a fan blade containment section defined about an engine axis, a thrust reverser cascade section downstream of the blade containment section and a Fan Exit Guide Vane section downstream of the thrust reverser cascade section.
1. A fan case of a gas turbine engine comprising: a fan blade containment section defined about anengine axis;a thrust reverser cascade section downstream of said blade containment section, said thrust reverser cascade section including an array of cascade airfoils and a plurality of inner thrust reverser doors radially inwards of said array of cascade airfoils, said inner thrust reverser doors opening inwards toward said engine axis and being arranged in a helix; anda Fan Exit Guide Vane section downstream of said thrust reverser cascade section. 2. The...