A self-pressurized liquid storage tank for an electronic pod environment control system

A self-pressurized liquid storage tank and environmental control system technology, applied in the field of electronic pod environmental control system or aircraft liquid cooling system, can solve the problems of pump inlet pressure fluctuation, pump impeller cavitation damage, pump inlet negative pressure, etc. , to achieve the effects of stable boost pressure, stable pressure and improved system reliability

Active Publication Date: 2021-10-22
XINXIANG AVIATION IND GROUP +1
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  • Claims
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AI Technical Summary

Problems solved by technology

[0002] In the electronic pod environmental control system or aircraft liquid cooling system, when the flight altitude changes, the atmospheric pressure changes accordingly, and the elastic element of the self-pressurized liquid storage tank of the system will experience displacement when the atmospheric pressure changes, and the self-pressurized liquid storage tank The boost pressure of the tank will also change, which will cause the pump inlet pressure to fluctuate. When the pressure is less than a certain value, the pump inlet will generate negative pressure, which will cause cavitation damage to the pump impeller.

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  • A self-pressurized liquid storage tank for an electronic pod environment control system
  • A self-pressurized liquid storage tank for an electronic pod environment control system

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Embodiment Construction

[0019] Referring to the accompanying drawings, through the description of the embodiments, the specific implementation of the present invention, such as the shape, structure, mutual position and connection relationship between the various parts, the function and working principle of each part, and the manufacturing process And operation and use methods, etc., for further detailed description, to help those skilled in the art have a more complete, accurate and in-depth understanding of the concept and technical solutions of the present invention:

[0020] The present invention will be described in further detail below. see figure 1 , a self-pressurized liquid storage tank for an electronic pod environmental control system, the structure includes a housing 1, an elastic element assembly 2, and a pump 3; wherein the elastic element assembly 2 is placed in the housing 1, and one end is connected to the The housing 1 is fixed and sealed by a sealing ring, and the other end is susp...

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Abstract

The invention belongs to the field of electronic pod environmental control system or aircraft liquid cooling system, and in particular relates to a self-pressurized liquid storage tank of the electronic pod environmental control system, which includes a shell, an elastic element assembly, and a pump. One side of the shell is provided with a The system liquid return port and the pump connection port, the elastic element assembly is arranged in the housing, one end of the elastic element assembly is fixedly connected to the side wall inside the housing away from the system liquid return port and the pump connection port, and the other end is suspended in the housing. And it is close to the liquid return port of the system and the pump connection port. The pump is connected to the pump connection port of the casing. The invention can make the elastic element not be affected by the flight height and stabilize the boost pressure, so as to ensure the stability of the pump inlet pressure and prevent the pump The impeller produces cavitation, improving system reliability.

Description

technical field [0001] The invention belongs to the field of an electronic pod environmental control system or an aircraft liquid cooling system, and in particular relates to a self-pressurized liquid storage tank of an electronic pod environmental control system. Background technique [0002] In the electronic pod environmental control system or aircraft liquid cooling system, when the flight altitude changes, the atmospheric pressure changes accordingly, and the elastic element of the self-pressurized liquid storage tank of the system will experience displacement when the atmospheric pressure changes, and the self-pressurized liquid storage tank The boost pressure of the tank will also change, which will cause the pump inlet pressure to fluctuate. When the pressure is less than a certain value, the pump inlet will generate negative pressure, which will cause cavitation damage to the pump impeller. [0003] There is a need for a self-pressurized liquid storage tank for the ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): F04D29/66
CPCF04D29/669
Inventor 付旭东王超冯有军包胜刘俊峰陈冰
Owner XINXIANG AVIATION IND GROUP
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