公开(公告)号：US20160023771A1

公开(公告)日：2016-01-28

申请号：US14877098

申请日：2015-10-07

Applicant: AIRCELLE

Inventor： Audrey RIQUET ,  Caroline COAT-LENZOTTI

IPC: B64D15/00 ,  B64D33/02

CPC classification number: B64D15/00 ,  B64D33/02 ,  B64D2033/0233 ,  B64D2033/0286 ,  F02C7/04 ,  F05D2300/512

Abstract: The present disclosure provides an aircraft element including a leading edge section and a trailing edge section, and the leading edge section includes an anti-frost treatment device. This aircraft element is remarkable in that the trailing edge section includes a superhydrophobic surface.

Abstract translation: 本公开内容提供了一种包括前缘部分和后缘部分的飞行器元件，并且前缘部分包括防霜处理装置。 该飞机元件是显着的，因为后缘部分包括超疏水表面。

公开(公告)号：US20150292351A1

公开(公告)日：2015-10-15

申请号：US14749808

申请日：2015-06-25

Applicant: AIRCELLE

Inventor： David PEREIRA ,  Hakim MAALIOUNE ,  Caroline COAT-LENZOTTI

IPC: F01D25/02

CPC classification number: F01D25/02 ,  B64D15/12 ,  B64D2033/0233

Abstract: The present disclosure provides an electric de-icing/anti-icing device for a turbojet engine or turbo-prop nacelle element to be protected from icing. The device includes: a heating assembly including first and second heating stages positioned in the nacelle element; an electricity supply circuit delivering a primary voltage to the first heating stage of the heating assembly. In particular, the electricity supply circuit includes an electricity source, and a de-icing/anti-icing circuit which is connected to the heating assembly and supplied voltage by the electricity source. Furthermore, the de-icing/anti-icing device includes components to supply a complementary voltage to the second heating stage of the heating assembly.

Abstract translation: 本公开提供了一种用于涡轮喷气发动机或涡轮支架机构元件的电除冰/防冰装置，以防止结冰。 该装置包括：加热组件，其包括定位在机舱元件中的第一和第二加热台; 向该加热组件的第一加热阶段提供初级电压的电力供应电路。 特别地，电力供给电路包括电源和除冰/除冰电路，其连接到加热组件并由电源供电。 此外，除冰/防冰装置包括向加热组件的第二加热台提供互补电压的部件。