公开(公告)号：EP2915742B1

公开(公告)日：2016-11-09

申请号：EP15157399.5

申请日：2015-03-03

Applicant: United Technologies Corporation

Inventor： ROACH, James T. ,  COOK, III, Grant O. ,  KLING, Colin J. ,  O'BRIEN, James F. ,  BUGAJ, Shari L.

IPC: B64C11/14 ,  F02C7/04 ,  F01D5/02

CPC classification number: F01D9/02 ,  B64C11/14 ,  F01D5/02 ,  F01D5/12 ,  F02C7/04 ,  F05D2220/32 ,  F05D2300/10 ,  F05D2300/603 ,  F05D2300/6034 ,  Y02T50/672

Abstract: A spinner (80) for a gas turbine engine (20) comprises an outer shell (82) for defining an airflow path when mounted in a gas turbine engine (20). An inner surface (84) is provided with a plurality of webs (86). A gas turbine engine (20) and a fan section (22) for a gas turbine engine (20) are also disclosed.

公开(公告)号：EP2915742B2

公开(公告)日：2019-08-28

申请号：EP15157399.5

申请日：2015-03-03

Applicant: United Technologies Corporation

Inventor： ROACH, James T. ,  COOK, III, Grant O. ,  KLING, Colin J. ,  O'BRIEN, James F. ,  BUGAJ, Shari L.

IPC: B64C11/14 ,  F02C7/04 ,  F01D5/02

公开(公告)号：EP2915742A1

公开(公告)日：2015-09-09

申请号：EP15157399.5

申请日：2015-03-03

Applicant: UNITED TECHNOLOGIES CORPORATION

Inventor： ROACH, James T. ,  COOK, III, Grant O. ,  KLING, Colin J. ,  O'BRIEN, James F. ,  BUGAJ, Shari L.

IPC: B64C11/14 ,  F02C7/04

CPC classification number: F01D9/02 ,  B64C11/14 ,  F01D5/02 ,  F01D5/12 ,  F02C7/04 ,  F05D2220/32 ,  F05D2300/10 ,  F05D2300/603 ,  F05D2300/6034 ,  Y02T50/672

Abstract: A spinner (80) for a gas turbine engine (20) comprises an outer shell (82) for defining an airflow path when mounted in a gas turbine engine (20). An inner surface (84) is provided with a plurality of webs (86). A gas turbine engine (20) and a fan section (22) for a gas turbine engine (20) are also disclosed.

Abstract translation: 用于燃气涡轮发动机（20）的旋转器（80）包括用于在安装在燃气涡轮发动机（20）中时限定气流路径的外壳（82）。 内表面（84）设置有多个腹板（86）。 还公开了一种燃气涡轮发动机（20）和用于燃气涡轮发动机（20）的风扇部分（22）。