Dynamic modeling method for suspended liquid filling tank

A dynamic modeling and suspension technology, applied in the field of spacecraft dynamic modeling and analysis, can solve the problems of high generalized mass calculation value, dangerous flight status, large difference between normalized mode shape value and test value, etc. , to achieve good consistency

Active Publication Date: 2017-02-08
BEIJING INST OF ASTRONAUTICAL SYST ENG +1
View PDF3 Cites 4 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0009] The second method uses shell element modeling, which is more accurate in simulating the stiffness of the tank connection. However, due to the influence of the breathing mode of the tank shell model, the normalized vibration mode values ​​of the front and rear bottom of the ta

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Dynamic modeling method for suspended liquid filling tank
  • Dynamic modeling method for suspended liquid filling tank
  • Dynamic modeling method for suspended liquid filling tank

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0034] In order to obtain better modal and dynamic response prediction values, the present invention proposes a "shell + beam + concentrated mass point unit" suspension type liquid-filled tank modeling method, such as figure 1 As shown, including the following steps:

[0035] S01: Establish the point, line and surface geometric model of the tank structure according to the inner profile size of the tank, where the point is located on the central axis of the tank and the line is located on the central axis of the tank.

[0036] S02: Apply the Saint-Venant principle to divide the shell elements of the tank section and the tank lugs in the upper and lower H ranges of the circumference of the tank lug to eliminate the influence of boundary effects and ensure a more reasonable connection stiffness simulation. H is not less than the radial length of the lugs of the tank, generally 100mm. The shell elements are divided into the support connecting the lugs of the storage tank and the spacec...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The present invention discloses a dynamic modeling method for a suspended liquid filling tank, and belongs to the field of spacecraft dynamics modeling and analysis. The ''shell + beam + concentrated mass point elements'' dynamic modeling method for the suspended liquid filling tank is adopted, a tank section connected with the support boundary is simulated by using the shell element, and other tank section is simulated by using the beam element; and in addition, in order to ensure a relatively large stiffness after pressurization of the actual tank, the multi-point constraint RBE2 is established on the upper and lower end surfaces of the shell element, and according to the method of consistency of the center of mass, the liquid is attached to the beam element in a corresponding position by using the discrete concentrated mass element. Compared with the traditional ''beam element'' and ''shell element'', the method disclosed by the present invention combines the advantages of different elements, so that on one hand, the connection stiffness between the tank and the main structure is not changed, both local modalities and feature point peak response are taken into account at the same time, and the consistency of the obtained modal and dynamic response predictive value and experimental value is better.

Description

[0001] Technical field: [0002] The invention relates to a dynamic modeling method of a suspended liquid-filled storage tank, which belongs to the field of spacecraft dynamics modeling analysis. [0003] Background technique: [0004] For spacecraft large-size / non-supported liquid-filled tanks, the liquid-filled tanks are generally connected to the main structure support through their own lugs or end frames, and the mass of propellant often accounts for 40% or more of the take-off mass, so , The liquid-filled storage tank has a greater impact on the overall and local modalities of the spacecraft assembly, sometimes up to 50% to 60%; at the same time, due to the limitation of the installation method, there may be a possibility between the branch of the liquid-filled tank and the main structure There is a certain offset or cantilever, which makes the vibration environment of the liquid-filled storage tank and the connected liquid pipes relatively harsh. In engineering, the finite ele...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
IPC IPC(8): G06F17/50
CPCG06F30/23
Inventor 林宏张新宇彭慧莲王国辉陈益安雪岩王明哲王雪梅陆浩然崔照云叶成敏刘志伟张群唐颀杨自鹏杨勇于秀丽杨炜平刘欣刘建忠肖泽宁张巍曹梦磊琚春光
Owner BEIJING INST OF ASTRONAUTICAL SYST ENG
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products