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Energy supply system for supplying energy to aircraft systems

A technology of energy supply system and aircraft, which is applied in the direction of power system fuel cell, aircraft parts, energy-saving board measures, etc., to achieve the effect of simplifying the system

Inactive Publication Date: 2008-09-24
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

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  • Energy supply system for supplying energy to aircraft systems

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Embodiment Construction

[0036] Fig. 1 shows a simplified diagram of an energy supply system according to an exemplary embodiment of the present invention, which is used to supply electrical energy to an electrical load of an aircraft. As shown in FIG. 1, the energy supply system 100 includes a fuel cell 101, which is coupled to a capacitor 103 through a first conductive connection device or line 102. In addition, the fuel cell 101 and the capacitor 103 are coupled through a second conductive connection device 104 in which a diode 105 is interconnected. In addition, the energy supply system 100 includes a reverse rectifier 106 that is coupled to the capacitor 103 through a third conductive line 107 and a fourth conductive line 108. The voltmeter 109 is coupled between the third conductive line 107 and the fourth conductive line 108, and the voltmeter 109 is used to determine the voltage provided by the capacitor 103.

[0037] In addition, the energy supply system 100 includes a rectifier 110 that is also ...

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Abstract

An energy supply system 100 for an aircraft comprises at least one fuel cell 101 and at least one energy storage device 103, wherein the fuel cell 101, of which there is at least one, is coupled to the energy storage device 103, of which there is at least one, such that the energy storage device 103 can be charged by means of the fuel cell 101.

Description

[0001] This application claims the priority of German Patent Application No. 10 2005 046729.6 filed on September 29, 2005, and U.S. Provisional Patent Application No. 60 / 721,638 filed on September 26, 2005, and is hereby incorporated by reference The disclosure of this is incorporated herein. Technical field [0002] The present invention relates to an energy supply system for supplying energy to an aircraft system, and a method for supplying energy to an aircraft system, in particular to an energy supply system including a fuel cell and an energy storage device. Background technique [0003] In the current aircraft technology, there are different bus systems for aircraft electronic equipment, namely power line systems, which supply the aircraft with, for example, 28V direct current or 115V, 400 Hz alternating current. Energy is supplied to multiple electrical loads through these bus systems. For example, the opening of the cargo compartment door of an aircraft is realized by a de...

Claims

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Application Information

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IPC IPC(8): B64D41/00H01M8/00
CPCH02J4/00H02J2001/004H01M16/003B64D41/00Y02T90/36Y02T50/53H02J7/345Y02T90/32H02J7/34H01M2250/20B64D2041/005H02J2300/30H02J2310/44Y02T50/50Y02T90/40Y02E60/50
Inventor 拉尔夫-亨宁·施托尔特哈拉尔德·格林德尔
Owner AIRBUS OPERATIONS GMBH
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