[PDF][PDF] 航空发动机整机振动耦合动力学模型及其验证

陈果 - 航空动力学报, 2012 - ides.nuaa.edu.cn
针对航空发动机整机振动, 建立了一种通用的复杂转子-支承-机匣耦合动力学模型. 在模型中,
利用有限元方法对转子和机匣系统进行建模. 支承系统采用集总参数模型 …

Vibration modelling and verifications for whole aero-engine

G Chen - Journal of Sound and Vibration, 2015 - Elsevier
In this study, a new rotor–ball-bearing–casing coupling dynamic model for a practical aero-
engine is established. In the coupling system, the rotor and casing systems are modelled …

[PDF][PDF] 双转子航空发动机整机振动建模与分析

陈果 - 振动工程学报, 2011 - ides.nuaa.edu.cn
针对实际的双转子航空发动机, 建立了航空发动机双转子-支承-机匣耦合动力学模型.
在耦合模型中, 利用有限元方法对转子和机匣系统进行建模; 支承系统采用了集总参数模型 …

A parametric study of an unbalanced Jeffcott rotor supported by a rolling-element bearing

AH Haslam, CW Schwingshackl, AIJ Rix - Nonlinear Dynamics, 2020 - Springer
Rolling-element bearings are widely used in industrial rotating machines, and hence there is
a strong need to accurately predict their influence on the response of such systems …

Long duration blade loss simulations including thermal growths for dual-rotor gas turbine engine

G Sun, A Palazzolo, A Provenza, C Lawrence… - Journal of Sound and …, 2008 - Elsevier
This paper presents an approach for blade loss simulation including thermal growth effects
for a dual-rotor gas turbine engine supported on bearing and squeeze film damper. A …

Vibration control of high-speed rotor supported by hybrid foil-magnetic bearing with sudden imbalance

S Jeong, YB Lee - Journal of Vibration and Control, 2017 - journals.sagepub.com
A hybrid foil-magnetic bearing (HFMB) was successfully studied as a vibration isolator by
introducing a sudden imbalance or an unexpected disturbance during turbine/rotor …

The dynamic characteristics of a rotor supported on ball bearings with different floating ring squeeze film dampers

H Zhou, G Feng, G Luo, Y Ai, D Sun - Mechanism and Machine Theory, 2014 - Elsevier
Two different floating ring squeeze film dampers (FSFD) were studied, one has a single oil
film, which is referred as FSFDS, and the other has a double layer oil film, which is referred …

航空发动机整机耦合动力学模型及振动分析

陈果 - 力学学报, 2010 - lxxb.cstam.org.cn
面向航空发动机整机振动, 建立了航空发动机转子-滚动轴承-机匣耦合动力学模型.
该模型具有如下特点:(1) 考虑转子, 滚动轴承及机匣之间的耦合作用;(2) 考虑了实际航空发动机 …

Fault-tolerant homopolar magnetic bearings

MH Li, AB Palazzolo, A Kenny… - IEEE Transactions …, 2004 - ieeexplore.ieee.org
This paper summarizes the development of a novel magnetic suspension that improves
reliability via fault-tolerant operation. The suspension is suitable for flywheels used in …

Application of improved hybrid interface substructural component modal synthesis method in vibration characteristics of mistuned blisk

B Bai, G Bai, C Li - Chinese Journal of Mechanical Engineering, 2014 - Springer
The large and complex structures are divided into hundreds of thousands or millions
degrees of freedom (DOF) when they are calculated which will spend a lot of time and the …