公开(公告)号：US08444093B1

公开(公告)日：2013-05-21

申请号：US13088630

申请日：2011-04-18

Applicant: Eran Epstein

Inventor： Eran Epstein

IPC: B64D15/02 ,  B64D15/04 ,  B64D15/06

CPC classification number: B64D15/02

Abstract: An airplane leading edge de-icing apparatus having a heat diffuser for heating the leading edges of an airplane is provided. The heat diffuser has a first heat diffuser side having a concave shape and a second heat diffuser side having a convex shape. The heat diffuser is joined to the leading edge of an airplane. A counter current heat exchanger is provided and heats a heat transfer fluid with heat energy absorbed from hot gases. The heat transfer fluid is pumped in and out of a reservoir tank with a first pump. A second pump pumps the heat transfer fluid in and out of the heat diffuser. The heat energy in the heat transfer fluid housed in the heat diffuser is transferred to the convex surface of the second heat diffuser side and prevents and/or melts ice build-up.

Abstract translation: 提供一种具有用于加热飞机前缘的散热器的飞机前缘除冰装置。 散热器具有第一散热器侧，其具有凹形，第二热扩散器侧具有凸形。 散热器连接到飞机的前缘。 提供了逆流热交换器，并且利用从热气体吸收的热能来加热传热流体。 传热流体用第一泵泵入和流出贮槽。 第二泵将传热流体泵入和散出热量扩散器。 容纳在散热器中的传热流体中的热能被传递到第二散热器侧的凸面，并且防止和/或熔化积冰。

公开(公告)号：US08702039B1

公开(公告)日：2014-04-22

申请号：US13868410

申请日：2013-04-23

Applicant: Eran Epstein

Inventor： Eran Epstein

IPC: B64D15/02

CPC classification number: B64D15/02

Abstract: An airplane leading edge de-icing apparatus having a heat diffuser for heating the leading edges of an airplane is provided. The heat diffuser has a first heat diffuser side having a concave shape and a second heat diffuser side having a convex shape. The heat diffuser is joined to the leading edge of an airplane. A counter current heat exchanger is provided and heats a heat transfer fluid with heat energy absorbed from hot gases. The heat transfer fluid is pumped in and out of a reservoir tank with a first pump. A second pump pumps the heat transfer fluid in and out of the heat diffuser. The heat energy in the heat transfer fluid housed in the heat diffuser is transferred to the convex surface of the second heat diffuser side and prevents and/or melts ice build-up.

Abstract translation: 提供一种具有用于加热飞机前缘的散热器的飞机前缘除冰装置。 散热器具有第一散热器侧，其具有凹形，第二热扩散器侧具有凸形。 散热器连接到飞机的前缘。 提供了逆流热交换器，并且利用从热气体吸收的热能来加热传热流体。 传热流体用第一泵泵入和流出贮槽。 第二泵将传热流体泵入和散出热量扩散器。 容纳在散热器中的传热流体中的热能被传递到第二散热器侧的凸面，并且防止和/或熔化积冰。