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Special-shaped storage tank outflow device

A storage tank and special-shaped technology, which is applied in the field of liquid rocket pressurized delivery system, can solve the problems affecting the normal operation of the engine, propellant air entrainment, engine pump cavitation, etc., and achieve the benefits of carrying capacity, improving carrying capacity and strengthening the structure The effect of stiffness

Active Publication Date: 2021-03-19
BEIJING INST OF ASTRONAUTICAL SYST ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The generation of vortex or liquid surface collapse will lead to gas entrainment of propellant, which may cause cavitation of engine pump, and then affect the normal operation of the engine, causing a major danger of flight failure

Method used

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  • Special-shaped storage tank outflow device
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  • Special-shaped storage tank outflow device

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Embodiment Construction

[0027] In order to better understand the above technical solutions, the technical solutions of the present application will be described in detail below through the accompanying drawings and specific examples. It should be understood that the embodiments of the present application and the specific features in the examples are detailed descriptions of the technical solutions of the present application, and It is not a limitation to the technical solutions of the present application, and the embodiments of the present application and the technical features in the embodiments can be combined without conflict.

[0028] A further detailed description will be given below of a special-shaped storage tank outflow device provided by the embodiment of the present application in conjunction with the accompanying drawings. The specific implementation methods may include (such as figure 1 shown):

[0029] In the scheme provided by the embodiment of this application,

[0030] figure 1 It ...

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Abstract

The invention discloses a special-shaped storage tank outflow device, and belongs to the technical field of liquid rocket pressurization conveying systems. A vortex eliminating plate and a partition plate are installed on a flow outlet of a common-bottom storage tank, holes are formed in the vortex eliminating plate, the structural load of the vortex eliminating plate is reduced, meanwhile, the structural weight of the vortex eliminating plate is reduced, meanwhile, the bearing capacity of the vortex eliminating plate is improved through reasonable layout of the holes, and the vortex eliminating plate is of a 120-degree V-shaped structure, so that fluid transition is smooth as much as possible; and meanwhile, liquid tends to be filled to the center, a cover plate is installed on the upperportion of the flow outlet (the axial direction of the storage tank) of the common-bottom storage tank, the liquid tends to flow downwards (accelerate), tangential force for forming vortexes is destroyed, the vortexes and collapse are restrained through the arrangement, and therefore the unusable amount of the liquid in the storage tank is reduced.

Description

technical field [0001] The invention relates to an outflow device of a special-shaped storage tank, which belongs to the technical field of liquid rocket booster conveying systems. Background technique [0002] The common-bottom storage tank has the advantages of shortening the height of the rocket body structure, reducing the length-to-diameter ratio of the launch vehicle, effectively reducing the weight of the rocket itself, and improving structural efficiency. For tanks with a common bottom structure, the propellant outlet of the upper tank is generally set at the lower end of the tank barrel, and the outflow form is side outflow. At the end of the side outflow, due to the influence of the outlet profile, the geometric parameters of the tank, the flow velocity, and the overload and sloshing in flight on the local flow characteristics, the phenomenon of liquid surface collapse and vortex will appear above the outlet. The generation of vortex or liquid surface collapse wil...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02K9/60F15D1/00
CPCF02K9/605F15D1/0025F15D1/0005
Inventor 吴姮孙善秀吴俊峰贺启林丁蕾刘文川赵涛曹荣石朝锋吕宝西
Owner BEIJING INST OF ASTRONAUTICAL SYST ENG
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