Bidirectional rotational flow mixing device for heat exchanger of air source system

A technology of swirl mixing and heat exchanger, which is applied in the field of aircraft environmental control system, can solve the problems of short distance from the outlet of the precooler to the branch of the downstream pipeline, the uncertainty of the temperature of the air conditioner and anti-icing, and solve the problem of temperature control , to achieve the effect of homogenization

Pending Publication Date: 2022-03-15
COMAC +1
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, it is actually found that the airflow rotates in a single direction, which will lead to greater uncertainty in the temperature on both sides of the air conditioner and anti-icing
And the distance from the outlet of the precooler to the branch of the downstream pipeline is short, so the air mixing device must have higher heat exchange efficiency to ensure the same temperature on both sides of the air conditioner and anti-icing

Method used

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  • Bidirectional rotational flow mixing device for heat exchanger of air source system
  • Bidirectional rotational flow mixing device for heat exchanger of air source system
  • Bidirectional rotational flow mixing device for heat exchanger of air source system

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Embodiment Construction

[0038] The present invention will be further described below in conjunction with specific embodiment and accompanying drawing, set forth more details in the following description so as to fully understand the present invention, but the present invention can obviously be implemented in many other ways different from this description, Those skilled in the art can make similar promotions and deductions based on actual application situations without violating the connotation of the present invention, so the content of this specific embodiment should not limit the protection scope of the present invention.

[0039] In the following description, upstream and downstream refer to the flow direction of the airflow from the precooler to the downstream pipeline, the front side / front end refers to the side or end near the precooler, and the rear side / rear end refers to the side near the downstream The side or end of a pipe, unless otherwise characterized.

[0040] figure 1 , figure 2 ...

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Abstract

The invention discloses a bidirectional rotational flow mixing device for a heat exchanger of an aircraft air source system, the mixing device comprises an outer sleeve and an inner sleeve, the inner sleeve is located in the outer sleeve, and the two sleeves are spaced from each other; the mixing device further comprises a plurality of outer ring stator blades, and the outer ring stator blades are fixedly connected with the inner wall face of the outer sleeve and the outer wall face of the inner sleeve at intervals. The plurality of inner ring stator blades are fixedly connected with the inner wall surface of the inner sleeve in a mutually separated manner; the outer ring stator blades and the inner ring stator blades are arranged at different angles relative to the longitudinal axis of the inner sleeve. When the outer-ring blades and the inner-ring blades incline in opposite directions relative to the longitudinal direction, the two-way rotational flow mixing device can enable air flows passing through the inner-ring blades and the outer-ring blades to rotate in opposite directions, so that the two air flows are wound and mixed with each other, and the purpose of quickly and efficiently realizing temperature field homogenization is achieved.

Description

technical field [0001] The invention relates to an aircraft environment control system, in particular to a two-way swirling flow mixing device used for a precooler of an air source system in the environment control system. Background technique [0002] The environmental control system of modern aircraft is mainly used to control the internal environment of the aircraft. It can provide ventilation for systems such as avionics, fuel and hydraulic systems, and also provide anti-icing and anti-fog functions for the aircraft. [0003] The civil aircraft environmental control system has a pre-cooling heat exchanger, which is used to cool the high-temperature bleed air of the engine, so as to meet the requirements of the downstream air conditioning, anti-icing, fuel tank inerting and other systems for the bleed air temperature. Usually, a temperature sensor is arranged downstream of the outlet of the hot side of the precooler for closed-loop control of the cold side flow of the pre...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D13/06
CPCB64D13/06B64D2013/0603
Inventor 刘嘉诚蒋亮亮潘舜智刘华源王磊南国鹏
Owner COMAC
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