| 摘要 |
The invention relates to the field of turbomachine rotor blades and notably to a turbomachine rotor blade comprising a blade root and a blade tip which are separated by a blade height (h), and at least one intermediate portion (112a), having a negative tangential inclination, and a distal portion (112b), situated between the intermediate segment (112a) and the blade tip, having a positive tangential inclination, in which the distal portion (112b) extends over at most 30% of the said blade height (h). |
