公开(公告)号：US20170015054A1

公开(公告)日：2017-01-19

申请号：US15209929

申请日：2016-07-14

Applicant: Airbus Operations GmbH

Inventor： Johannes Born ,  Alexander Fabritz ,  Carsten Rowedder

IPC: B29C65/64 ,  B29C65/00 ,  F16L47/02

CPC classification number: B29C65/645 ,  B23K20/002 ,  B23K20/10 ,  B23K20/233 ,  B23K33/006 ,  B23K2101/06 ,  B23K2103/14 ,  B23K2103/172 ,  B23K2103/18 ,  B29C66/1122 ,  B29C66/1142 ,  B29C66/1222 ,  B29C66/1224 ,  B29C66/1226 ,  B29C66/12441 ,  B29C66/5229 ,  B29C66/5344 ,  B29C66/63 ,  B29C66/652 ,  B29C66/71 ,  B29C66/7212 ,  B29C66/7392 ,  B29C66/742 ,  B29C66/7428 ,  B29C66/836 ,  F16L47/02 ,  F16L47/24 ,  B29K2307/04 ,  B29K2309/08 ,  B29K2071/00

Abstract: A system comprising a pipe and at least one fitting, wherein the pipe is made essentially of a thermoplastic, fiber-reinforced composite material, and the fitting is made essentially of titanium or a titanium alloy, and the pipe and the fitting are connected in a fluid-tight manner

Abstract translation: 一种包括管和至少一个配件的系统，其中所述管基本上由热塑性纤维增强复合材料制成，并且所述配件基本上由钛或钛合金制成，并且所述管和所述配件连接在 流畅的方式

公开(公告)号：US20160200447A1

公开(公告)日：2016-07-14

申请号：US14984723

申请日：2015-12-30

Applicant: Airbus Operations GmbH

Inventor： Hauke-Peer Luedders ,  Sijmen Zandstra ,  Alexander Fabritz

IPC: B64D37/32 ,  B64D41/00 ,  H01M8/04082

CPC classification number: B64D37/32 ,  B64D41/007 ,  H01M8/04201 ,  H01M8/04761 ,  H01M2250/20 ,  Y02T90/32

Abstract: A fuel cell system for an aircraft includes at least one fuel cell having a first inlet for providing a fuel, a second inlet for providing an oxidant, an outlet for removing exhaust air and a voltage outlet, an electrically operable hydraulic pump, which is integratable into a hydraulics network of the aircraft and connectable to the voltage outlet of the at least one fuel cell and a controllable hydraulic energy converter with changeable operating behaviour. The hydraulic energy converter is adapted for generating such a power demand in the hydraulics network, that the at least one fuel cell provides a predetermined volume flow of oxygen depleted air at the outlet through delivering electrical power to the hydraulic pump.

Abstract translation: 一种用于飞行器的燃料电池系统包括至少一个燃料电池，其具有用于提供燃料的第一入口，用于提供氧化剂的第二入口，用于除去排气的出口和电压出口，电可操作的液压泵，其是可积分的 进入飞行器的液压网络并且可连接到至少一个燃料电池的电压出口和具有可变操作特性的可控制的液压能量转换器。 液压能量转换器适于在液压网络中产生这样的功率需求，使得至少一个燃料电池通过向液压泵输送电力而在出口处提供预定体积的氧耗尽空气。