Looking for breakthrough ideas for innovation challenges? Try Patsnap Eureka!

Supporting component used for similar simulation test of high-speed rotor and testing method

A technology similar to simulation, high-speed rotor, used in engine testing, machine/structural component testing, measuring devices, etc., can solve the problems of limited control accuracy of hydraulic devices, low stiffness adjustment accuracy, easy to float up and down, etc., to achieve stiffness Stabilize, weaken adjustment error, increase the effect of strength

Active Publication Date: 2018-10-16
BEIJING AEROSPACE PROPULSION INST
View PDF11 Cites 4 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, although the similarity theory of high-speed flexible rotors has been relatively perfect, many theoretical conditions cannot be satisfied in actual experiments. It is not difficult to scale up or down, but the rotor system usually includes a high-speed rotor, bearings and a test bench support for supporting the bearing. The bearing is used to support the rotation of the high-speed rotor. The test bench support includes the support body and the The inner cavity of the seat body is equipped with a hydraulic device. At present, the support stiffness of the test bench support can only be changed through the hydraulic device. Since the adjustment amount of the hydraulic device to the stiffness is only about 30-50% of the rigidity of the support body, it cannot meet the larger requirements. Stiffness is proportionally transformed, and due to the limited control precision of the hydraulic device, the adjustment precision of the stiffness is low, and it is easy to fluctuate up and down

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
  • Supporting component used for similar simulation test of high-speed rotor and testing method
  • Supporting component used for similar simulation test of high-speed rotor and testing method
  • Supporting component used for similar simulation test of high-speed rotor and testing method

Examples

Experimental program
Comparison scheme
Effect test

specific Embodiment

[0056] A liquid rocket engine high-speed turbo pump rotor with a journal size of 40mm and a length of 300mm, a working speed of 80,000rpm, and a combined support stiffness of the support components of 3x10 7 N / m.

[0057] Since the existing rotor test capability cannot reach the speed of 80000rpm, it is impossible to test and verify the dynamic characteristics of the rotor structure in real operation. Therefore, the similar design method is adopted, and the rotor working rotor is reduced by establishing a similar model.

[0058] If it is necessary to reduce the test speed to 40000rpm, according to the similar proportional relationship, both the journal and the length of the rotor need to be doubled, and the support stiffness should also be doubled, that is, to reach 6x10 7 N / m. Since the overall series stiffness of the combined support is less than the stiffness of each single piece, the squirrel cage and support with higher stiffness are selected for combination, and two pa...

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 invention provides a supporting component used for a similar simulation test of a high-speed rotor and a testing method, and belongs to the field of similar design of the high-speed rotor. The supporting component comprises a bearing, multiple rotor cages and a testing platform support. The bearing is used for supporting the simulation rotor to rotate, inner diameters of the rotor cages are identical and are matched with the outer diameter of the bearing, the rigidities of the rotor cages are different, in the test, different rotor cages are selected to sleeve the exterior of the bearing respectively, and the selected rotor cages and bearing are fixed through the testing platform support to simulate different supporting rigidities. The supporting rigidity of the provided supporting component can be two times or above that of a rotor original part, and the supporting component has high adjustment capacity for the supporting rigidity of a rotor system.

Description

technical field [0001] The invention belongs to the field of similar design of high-speed rotors, and relates to a support assembly for similar simulation tests of high-speed rotors and a similar simulation test method. Background technique [0002] The turbopump rotor system is the main component of the liquid rocket engine turbopump. With the continuous exploration of space and the rapid development of the aerospace industry, the working speed of the engine continues to increase, usually exceeding the first-order, second-order or even super-third-order critical speed. flexible rotor. However, the test capability of the corresponding high-speed flexible rotor does not fully meet the existing design requirements, mainly due to the instability of the existing high-speed test system, immature test methods, uncontrollable test safety, and insufficient high-speed test capability. This restricts the research and development of high-speed flexible rotors. [0003] Through the si...

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
Patent Type & Authority Applications(China)
IPC IPC(8): G01M15/02
CPCG01M15/02
Inventor 闫宇龙冯楚翔黄萍汪士清黄文莉杨永久刘学强
Owner BEIJING AEROSPACE PROPULSION INST
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Patsnap Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Patsnap Eureka Blog
Learn More
PatSnap group products