-
公开(公告)号:US10018050B2
公开(公告)日:2018-07-10
申请号:US14390566
申请日:2013-04-03
Applicant: SNECMA
Inventor: Vincent Paul Gabriel Perrot , Julien Cointe , Jean-Francois Rios
CPC classification number: F01D5/141 , F01D5/14 , F04D19/002 , F04D29/324 , F04D29/384 , F05D2220/36 , F05D2250/38 , Y02T50/673
Abstract: A turbomachine rotor blade including a blade root and a blade tip spaced apart by a blade height, including at least one intermediate segment between the blade root and the blade tip that presents forward sweep over at least 50% of the blade height, and a distal segment with backward sweep between the intermediate segment and the blade tip, the distal segment also presenting a positive tangential angle of inclination.
-
公开(公告)号:US20150118059A1
公开(公告)日:2015-04-30
申请号:US14390566
申请日:2013-04-03
Applicant: SNECMA
Inventor: Vincent Perrot , Julien Cointe , Jean-Francois Rios
CPC classification number: F01D5/141 , F01D5/14 , F04D19/002 , F04D29/324 , F04D29/384 , F05D2220/36 , F05D2250/38 , Y02T50/673
Abstract: A turbomachine rotor blade including a blade root and a blade tip spaced apart by a blade height, including at least one intermediate segment between the blade root and the blade tip that presents forward sweep over at least 50% of the blade height, and a distal segment with backward sweep between the intermediate segment and the blade tip, the distal segment also presenting a positive tangential angle of inclination.
Abstract translation: 一种涡轮机转子叶片,包括叶片根部和叶片顶端,叶片顶端间隔开叶片高度,包括在叶片根部和叶片尖端之间的至少一个中间部分,其向前扫掠至少50%的叶片高度,以及远端 在中间段和叶片尖端之间具有向后扫掠的段,远端段也呈现正切向倾角。
-