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Heat exchange device, aircraft hanger and aircraft

A technology of heat exchange device and heat exchanger, which is applied in the direction of deicing device, gas turbine device, jet propulsion device, etc., can solve the problems of complex integration of heat exchange device and so on.

Active Publication Date: 2022-04-05
AIRBUS OPERATIONS (SAS)
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Thus, the area above the primary structure 22 of the pylon and below the secondary structure 24 of the pylon is increasingly restricted, which tends to complicate the integration of the heat exchange means

Method used

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  • Heat exchange device, aircraft hanger and aircraft
  • Heat exchange device, aircraft hanger and aircraft
  • Heat exchange device, aircraft hanger and aircraft

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0046] Figure 4 An engine assembly 52 is shown comprising:

[0047] - engine 54 in which the core air flow flows,

[0048] - an engine nacelle 56 positioned around the engine 54 so as to define with it an annular duct in which a bypass flow of cold air flows, and

[0049] - A pylon 58 providing the connection between the engine 56 and the wing 60 of the aircraft.

[0050] The pylon 58 includes a rigid primary structure 62, which serves, among other things, to transmit forces between the engine 54 and the rest of the aircraft, and a secondary structure 64 which encloses the primary structure 62, And reduce the resistance of hanger 58.

[0051] A more detailed description of these elements of the engine assembly is not given, since they may be identical to those of the prior art.

[0052] For the remainder of the description, the longitudinal direction is a direction parallel to the engine axis A54. A transverse plane is a plane perpendicular to the longitudinal direction....

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PUM

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Abstract

The present invention relates to a heat exchange device configured to be positioned in an aircraft pylon and to an aircraft, the heat exchange device comprising a heat exchanger and an enclosure configured for use with a closed state and a more or less permissive state in which the closure prevents air flow through the heat exchanger and a more or less permissive state in which the closure allows air flow at a higher or lower For low-velocity flow, the closure includes a plurality of slats, each of which includes a pivot axis, the pivot axes of these different slats being parallel to each other and intersecting the direction of the air flow, the slats can simultaneously surround Their pivot axes move rotationally between a closed position, in which the slats are adjacent, corresponding to the closed position of the closure, and an open position, in which the slats are spread apart, which Corresponds to the permission state of the closure.

Description

technical field [0001] The present application relates to a compact heat exchange device incorporated into an aircraft pylon. Background technique [0002] according to figure 1 and figure 2 In the configuration shown in FIG. 1 , aircraft 10 includes a plurality of engine assemblies 12 positioned under wings 14 . [0003] Such as figure 2 As shown, engine assembly 12 includes: [0004] - engine 16, in which the core air flow flows, [0005] - an engine nacelle 18 positioned around the engine 16 so as to define with it an annular duct in which a bypass flow of cold air flows, and [0006] - A pylon 20 providing the connection between the engine 16 and the wing 14 . [0007] The pylon 20 includes a rigid primary structure 22 for, among other things, transmitting forces between the engine 16 and the rest of the aircraft 10 , and a secondary structure 24 that encloses the primary structure 22 , and reduce the resistance of the hanger 20. [0008] Such as figure 2 and...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D33/08B64D13/08B64D15/04
CPCB64D13/08B64D15/04B64D33/08B64D27/12F02C7/18F02C7/20F05D2220/323F05D2260/213F05D2260/232
Inventor 斯特凡·孔贝斯让·热利奥托马斯·德福雷阿德利纳·苏利耶伯努瓦·奥特乌
Owner AIRBUS OPERATIONS (SAS)