公开(公告)号：EP2644511A3

公开(公告)日：2017-02-22

申请号：EP13154308.4

申请日：2013-02-07

申请人： Keystone Engineering Company

发明人： Tuttle, Wayne H. ,  Adams, David ,  Anaya, Marcial Alexander ,  Pearson, Jeffry K.

IPC分类号： B64G1/40 ,  F02K9/60 ,  F17C13/00

CPC分类号： B64G1/402 ,  F02K9/605 ,  F05D2300/611 ,  F17C2201/0128 ,  F17C2201/056 ,  F17C2203/0607 ,  F17C2203/0617 ,  F17C2203/0619 ,  F17C2203/0646 ,  F17C2203/0648 ,  F17C2209/225 ,  F17C2221/08 ,  F17C2260/053 ,  F17C2270/0194

摘要： A demisable fuel supply system for a satellite includes a pressurized aluminum alloy tank (12) with an aluminum alloy propellant management device therein. The propellant management device (PMD) can have any capillary action surface tension fluid transport features known in the art. Selected inner surfaces of the tank (12) and the PMD are covered with a plasma powder sprayed titanium based coating to guarantee propellant wettability and corrosion resistance of the fuel supply system.

公开(公告)号：EP2644511B1

公开(公告)日：2018-09-19

申请号：EP13154308.4

申请日：2013-02-07

申请人： Keystone Engineering Company

发明人： Tuttle, Wayne H. ,  Adams, David ,  Anaya, Marcial Alexander ,  Pearson, Jeffry K.

IPC分类号： B64G1/40 ,  F02K9/60 ,  F17C13/00

CPC分类号： B64G1/402 ,  F02K9/605 ,  F05D2300/611 ,  F17C2201/0128 ,  F17C2201/056 ,  F17C2203/0607 ,  F17C2203/0617 ,  F17C2203/0619 ,  F17C2203/0646 ,  F17C2203/0648 ,  F17C2209/225 ,  F17C2221/08 ,  F17C2260/053 ,  F17C2270/0194

摘要： A demisable fuel supply system for a satellite includes a pressurized aluminum alloy tank (12) with an aluminum alloy propellant management device therein. The propellant management device (PMD) can have any capillary action surface tension fluid transport features known in the art. Selected inner surfaces of the tank (12) and the PMD are covered with a plasma powder sprayed titanium based coating to guarantee propellant wettability and corrosion resistance of the fuel supply system.

公开(公告)号：EP2644511A2

公开(公告)日：2013-10-02

申请号：EP13154308.4

申请日：2013-02-07

申请人： Keystone Engineering Company

发明人： Tuttle, Wayne H. ,  Adams, David ,  Anaya, Marcial Alexander ,  Pearson, Jeffry K.

IPC分类号： B64G1/40

CPC分类号： B64G1/402 ,  F02K9/605 ,  F05D2300/611 ,  F17C2201/0128 ,  F17C2201/056 ,  F17C2203/0607 ,  F17C2203/0617 ,  F17C2203/0619 ,  F17C2203/0646 ,  F17C2203/0648 ,  F17C2209/225 ,  F17C2221/08 ,  F17C2260/053 ,  F17C2270/0194

摘要： A demisable fuel supply system for a satellite includes a pressurized aluminum alloy tank (12) with an aluminum alloy propellant management device therein. The propellant management device (PMD) can have any capillary action surface tension fluid transport features known in the art. Selected inner surfaces of the tank (12) and the PMD are covered with a plasma powder sprayed titanium based coating to guarantee propellant wettability and corrosion resistance of the fuel supply system.

摘要翻译： 用于卫星的可燃燃料供应系统包括其中具有铝合金推进剂管理装置的加压铝合金罐（12）。 推进剂管理装置（PMD）可以具有本领域已知的任何毛细作用表面张力流体输送特征。 储罐（12）和PMD的选定内表面被等离子体粉末喷涂的钛基涂层覆盖，以保证燃料供应系统的推进剂润湿性和耐腐蚀性。

公开(公告)号：EP2502829B1

公开(公告)日：2020-10-21

申请号：EP12160308.8

申请日：2012-03-20

申请人： Keystone Engineering Company

发明人： Tuttle, Wayne H.

IPC分类号： B64G1/40 ,  F02K9/60 ,  F17C13/00