公开(公告)号：US20160362184A1

公开(公告)日：2016-12-15

申请号：US15172014

申请日：2016-06-02

Applicant: Fuji Jukogyo Kabushiki Kaisha

Inventor： Taro TANAKA ,  Takeshi YOSHIDA

IPC: B64D15/00 ,  B64D15/12 ,  C09K3/18

CPC classification number: B64D15/00 ,  B64D15/12 ,  C08L2205/02 ,  C08L2666/04 ,  C09D127/12 ,  C09D127/18 ,  C09D133/00 ,  C09K3/18 ,  C09K3/185 ,  F03D80/40 ,  C09D175/04 ,  C08L27/18 ,  C08L75/04 ,  C08L27/12

Abstract: A mixed coating material includes: a cold curing resin that undergoes reaction curing at normal room temperature; and a particulate fluororesin. The constituent ratio of the particulate fluororesin in a coating film that is a cured state of the mixed coating material is 43 wt % or more and 82 wt % or less. A wing includes a non-water-repellent coating film that forms an outermost layer in a water droplet impact region in a leading edge portion of the wing; and a water-repellent coating film that is formed of the mixed coating material and that forms an outermost layer in a water-repellent region adjacent to the water droplet impact region P. An anti-icing system includes the wing and a heating unit that heats the water droplet impact region.

Abstract translation: 混合涂料包括：在一般室温下进行反应固化的冷固化树脂; 和颗粒状氟树脂。 作为混合涂料的固化状态的涂膜中的颗粒状氟树脂的组成比为43重量％以上且82重量％以下。 翼包括在翼的前缘部分中的水滴冲击区域中形成最外层的非防水涂膜; 以及由混合涂料形成的防水涂膜，并且在与水滴冲击区域P相邻的防水区域中形成最外层。防冰系统包括机翼和加热单元 水滴冲击区域。

公开(公告)号：US20230357590A1

公开(公告)日：2023-11-09

申请号：US14662120

申请日：2015-03-18

Applicant: Fuji Jukogyo Kabushiki Kaisha

Inventor： Taro TANAKA ,  Takeshi YOSHIDA

IPC: C09D127/18 ,  C09D175/04

CPC classification number: C09D127/18 ,  C09D175/04

Abstract: A mixed coating material is obtained by mixing a cold curing resin that undergoes reaction curing at normal room temperature, and a fluororesin. The constituent ratio of the fluororesin in a coating film ranges from 43 wt % to 68 wt %.