| 发明名称 | Gas flow separator with a thermal bridge de-icer | ||
| 摘要 | The invention relates to a gas flow separator dividing the flow into a primary and a secondary stream, especially for a dual rotor axial turbomachine. The separator comprises a splitter nose of the turbomachine and includes a generally wedge-shaped leading edge in the gas flow to be split. The flow separator also comprises a metal blade having a longitudinal section in the form of an “S” and located in the nose in contact with the back of the leading edge and extending from the leading edge to a rear end of the separator at some distance from the leading edge, so as to be in contact with a heat source, such as a heat exchanger, located at some distance from the leading edge. | ||
| 申请公布号 | US8899917(B2) | 申请公布日期 | 2014.12.02 |
| 申请号 | US201213429627 | 申请日期 | 2012.03.26 |
| 申请人 | Techspace Aero S.A. | 发明人 | Bajusz Denis;Raimarckers Nicholas;Stephany Antoine;Broers Georges;Culot Yves;Strengnart Marc;Cornet Albert;Depaepe David |
| 分类号 | F01D25/02;F02C7/047 | 主分类号 | F01D25/02 |
| 代理机构 | Polster Lieder | 代理人 | Polster Lieder |
| 主权项 | 1. A gas flow separator for splitting a gas flow into a first flow and a second flow, said separator comprising: a separator leading edge; and a leading edge de-icing device comprising at least a metal blade in thermal contact with the leading edge and extending from the leading edge to a rear end of the separator at some distance from leading edge where the metal blade is in thermal contact with a heat source located at some distance from the leading edge. | ||
| 地址 | BE | ||