发明名称 PROCEDE ET SYSTEME DE DEGIVRAGE D'UNE ENTREE D'AIR DE TURBOMACHINE
摘要 <p>The system (17) has pneumatic expansion units i.e. inflatable bands (18, 19), placed against parts of an air inlet casing so as to eliminate white frosts (15, 16) on an air inlet (3) by mechanical shock. The air inlet comprises a front cone (12) and a direct inlet wheel provided with radial arms (13) that are fixed between an annular external structure (11) and the front cone. Parts of the pneumatic expansion units are arranged against the front cone. Holes are connected with cavities. An independent claim is also included for a method for de-icing an air inlet of a turboshaft engine.</p>
申请公布号 FR2962489(B1) 申请公布日期 2014.06.13
申请号 FR20100055619 申请日期 2010.07.09
申请人 SNECMA 发明人 DOS SANTOS NELSON;IGEL DOMINIK;PICART JEAN YVES
分类号 F02C7/04 主分类号 F02C7/04
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