发明名称 Wheel for e.g. turbojet of aircraft, has disk with circumferential groove, and internal part, where rotation of part leads to elastic strain so as to generate spring force such that part is moved towards its deployed configuration
摘要 The wheel has a disk with a circumferential groove, a radial external part (32) for blocking of a blade, and a radial internal part (34). The internal part is ready to present itself in a radially deployed configuration and in a retracted configuration. The internal part causes rotation of a bolt (46) like rotation of a set of telegraphic portions (45) between feet of the blade and a tread groove. The rotation of the internal part leads to elastic strain so as to generate a spring force such that the internal part is moved towards its deployed configuration. An independent claim is also included for a method for assembly of a wheel.
申请公布号 FR2997722(A1) 申请公布日期 2014.05.09
申请号 FR20120060530 申请日期 2012.11.06
申请人 SNECMA 发明人 CLOAREC YVON
分类号 F01D5/02;F01D5/32 主分类号 F01D5/02
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