Turbomachine blade rotor

The invention relates to the field of turbine engine rotor blades, including a blade (112) of a turbomachine rotor comprising a blade root (113) and a blade head (114) separated by a blade height ( h) and at least one intermediate segment (112a) between the blade root (113) and the blade head (114) having an arrow before at least 50% of said blade height ( h) and a distal segment (112b) back arrow between the intermediate segment (112a) and the blade head (114).