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Craft outer skin heat exchanger and method for manufacturing a craft outer skin heat exchanger

a heat exchanger and outer skin technology, applied in the field of craft outer skin heat exchangers, can solve the problems of large amount of thermal energy and high cooling requirements, and achieve the effects of enhancing the cooling capacity of the heat exchanger, and reducing the loss of air

Inactive Publication Date: 2015-01-29
AIRBUS OPERATIONS GMBH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The patent describes a heat exchanger for use in crafts, such as aircraft, that helps to cool the craft's power-generating devices. The heat exchanger is made up of heat transfer modules that are designed to be efficient in transferring heat. These modules can be manufactured in a flat, thin way and can have a relatively large length compared to their thickness. The modules can also have more than one heat transfer channel, which can be arranged in a way that allows the heat to flow from high-power devices to low-power devices. The heat exchanger can also have a separating element, which helps to prevent the entry of ambient air and create a smooth outer surface for the heat exchanger. This design reduces the aerodynamic drag caused by the heat exchanger when in use. Overall, the heat exchanger helps to cool the craft efficiently while minimizing the impact on its aerodynamic performance.

Problems solved by technology

A fuel cell that has a high capacity for generating electrical energy, however, also generates a large amount of thermal energy and therefore has a high cooling requirement.

Method used

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  • Craft outer skin heat exchanger and method for manufacturing a craft outer skin heat exchanger
  • Craft outer skin heat exchanger and method for manufacturing a craft outer skin heat exchanger
  • Craft outer skin heat exchanger and method for manufacturing a craft outer skin heat exchanger

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Embodiment Construction

[0037]FIGS. 1A to 1D show four different embodiments of heat transfer modules 10, 20, 30, 40, each of which may form a layer of a multilayer body 102, 202, 302 of a heat exchanger 100, 200, 300 as, for example, shown in one of FIGS. 2 to 5. Each heat exchanger multilayer body 102, 202, 302 comprises a plurality of heat transfer modules 10, 20, 30, 40 as shown in FIGS. 1A to 1D. If desired, only one type of heat transfer modules 10, 20, 30, 40 might be employed in the heat exchanger multilayer body 102, 202, 302. Alternatively, it is, however, also conceivable to equip the heat exchanger multilayer body 102, 202, 302 with at least two different types of heat transfer modules 10, 20, 30, 40 as shown in FIG. 1A, 1B, 1C or 1D.

[0038]The heat transfer module 10 shown in FIG. 1A comprises a heat transfer module body 10a and a rib or fin 12 which is formed integrally with the heat transfer module body 10a. The rib or fin 12 and the heat transfer module body 10a, however, also may be formed ...

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Abstract

A heat exchanger comprising a plurality of heat transfer modules disposed side by side so as to define a multilayer body of the heat exchanger. Each heat transfer module has at least one heat transfer medium channel configured to allow a flow of a heat-carrying medium therethrough. At least one portion of the multilayer body of the heat exchanger has a curvature configured to allow the heat exchanger to be used as a curved outer skin section of a craft. Adjacent heat transfer modules of the at least one portion of the multilayer body are arranged with a tilt angle of their central axes towards each other such that each heat transfer module is aligned towards the center of a local osculating circle defined by an outer surface of the heat exchanger.

Description

CROSS-REFERENCES TO RELATED APPLICATIONS[0001]This application is a continuation of International Application PCT / EP2013 / 056702 filed Mar. 28, 2013, designating the United States and published on Oct. 10, 2013 as WO 2013 / 149936. This application also claims the benefit of the U.S. Provisional Application No. 61 / 620,474, filed on Apr. 5, 2012, and of the European patent application No. 12002472.4, filed on Apr. 5, 2012, the entire disclosures of which are incorporated herein by way of reference.BACKGROUND OF THE INVENTION[0002]The invention relates to a craft outer skin heat exchanger, to the use of such an outer skin heat exchanger in an aircraft, and to a method for manufacturing such a craft outer skin heat exchanger.[0003]Fuel cell systems enable low-emission, highly efficient generation of electric current. For this reason, efforts are currently made to use fuel cell systems to generate electrical energy in various mobile applications, such as for example in automotive engineeri...

Claims

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Application Information

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IPC IPC(8): F28F21/00
CPCF28F2280/00F28F21/00B64C1/12B64D13/00B64D33/10Y10T29/4935F28F7/02
Inventor EILKEN, FLORIANAUER, UWEMOEGEL, MARTIN
Owner AIRBUS OPERATIONS GMBH
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