发明名称 Rotor of a turbomachine compressor, with an optimised inner end wall
摘要 A rotor of a turbomachine compressor, including a bladed rotor disk fitted at its radially external end with a wall forming the inner end of an annual flow channel of a primary gas flow, and formed from multiple angular sectors, each of which is delimited between two blades of the disk which are consecutive in a circumferential direction and includes a bulging portion which is convex in the axial direction and in the circumferential direction, together with, upstream from the bulging portion, a troughed portion which is concave in the axial direction and in the circumferential direction and which has a base which is roughly punctiform.
申请公布号 US9200638(B2) 申请公布日期 2015.12.01
申请号 US201013498696 申请日期 2010.10.01
申请人 SNECMA;CENAERO 发明人 Boston Eric Jacques;Chartoire Alexandre Franck Arnaud;Iliopoulou Vasiliki;Lepot Ingrid;Obrecht Thierry Jean-Jacques
分类号 F04D29/32;F01D5/14 主分类号 F04D29/32
代理机构 Oblon, McClelland, Maier & Neustadt, L.L.P. 代理人 Oblon, McClelland, Maier & Neustadt, L.L.P.
主权项 1. A rotor of a turbomachine compressor, comprising: a rotor disk which holds blades each of which has an extrados surface and an intrados surface, wherein the disk is fitted, at its radially outer end, with a wall forming an inner end of an annular flow channel of a primary gas flow in the turbomachine, wherein this wall is formed from multiple angular sectors, each of which is delimited between the extrados surface of a first blade and the intrados surface of a second blade which follows the first blade directly in a circumferential direction, wherein each of the sectors include a bulging portion which is convex in the axial direction and in the circumferential direction and has an apex located radially outside relative to an imaginary surface of revolution around the axis of the rotor disk and passing through four points defined by the intersection of the wall with, respectively, a leading edge of each of the first and second blades, and a trailing edge of each of the blades, wherein the apex of the bulging portion is roughly punctiform and is separated circumferentially from the extrados surface of the first blade by a distance of between 30% and 70% of the circumferential distance between the extrados and intrados surfaces of the blades measured at the apex, and wherein the wall also includes, upstream from the bulging portion, a troughed portion which is concave in the axial direction and concave in the circumferential direction, and has a base which is roughly punctiform and is located upstream from the apex of the bulging portion.
地址 Paris FR