| Citation: | Influences of small mistuning on dynamic characteristicsof bladed disks[J]. Journal of Aerospace Power, 2018, 33(7): 1566-1574. doi: 10.13224/j.cnki.jasp.2018.07.004
|
| [1] |
李其汉,王延荣,王建军.航空发动机叶片高循环疲劳失效研究［J］.航空发动机,2003,29(4):16-18.LI Qihan,WANG Yanrong,WANG Jianjun.Investigation of high cycle fatigue failures for the aero engine blades［J］.Aeroengine,2003,29(4):16-18.(in Chinese)
|
| [2] |
李其汉,王延荣.航空发动机结构强度设计问题［M］.上海：上海交通大学出版社,2014.
|
| [3] |
王建军,李其汉,朱梓根.失谐叶片一轮盘结构系统振动局部化问题的研究进展［J］.力学进展,2000,30(4):517-528.WANG Jianjun,LI Qihan,ZHU Zigen.Vibratory localization of mistuned bladed disk assemblies：a review［J］.Advances in Mechanics,2000,30(4):517-528.(in Chinese)
|
| [4] |
王建军,李其汉.航空发动机失谐叶盘振动减缩模型与应用［M］.北京：国防工业出版社,2009.
|
| [5] |
CASTANIER M P,PIERRE C.Modeling and analysis of mistuned bladed disk vibration:status and emerging directions［J］.Journal of Propulsion and Power,2006,22(2):384-396.
|
| [6] |
臧朝平,兰海强.失谐叶盘结构振动问题研究新进展［J］.航空工程进展,2011(2):133-142.ZANG Chaoping,LAN Haiqiang.Advances in research vibration problem of mistuned blisk assemblies［J］.Advances in Aeronautical Science and Engineering,2011,(2):133-142.(in Chinese)
］白斌,白广忱,童晓晨,等.整体叶盘结构失谐振动的国内外研究状况［J］.航空动力学报,2014,29(1):91-103.BAI Bin,BAI Guangchen,TONG Xiaochen,et al.Research on vibration problem of integral mistuned bladed disk assemblies at home and abroad［J］.Journal of Aerospace Power,2014,29(1):91-103.(in Chinese) |
| [7] |
姚建尧,高阳,王建军.航空发动机失谐叶盘动态特性研究进展［J］.航空制造技术,2016,516(21):76-85.YAO Jianyao,GAO Yang,WANG Jianjun.A review of dynamic characteristics of mistuned bladed disks［J］.Aeronautical Manufacturing Technology,2016,516(21):76-85.(in Chinese)
|
| [8] |
CASTANIER M P,PIERRE C.Using intentional mistuning in the design of turbomachinery rotors［J］.AIAA Journal,2002,40(10):2077-2086.
|
| [9] |
王建军,姚建尧,李其汉.刚度随机失谐叶盘结构概率模态特性分析［J］.航空动力学报,2008,23(2):256-262.WANG Jianjun,YAO Jianyao,LI Qihan.Probability characteristics of vibratory mode of bladed disk assemblies with random stiffness mistuning［J］.Journal of Aerospace Power,2008,23(2):256-262.(in Chinese)
|
| [10] |
BLADH R,PIERRE C,CASTANIER M P.Dynamic response predictions for a mistuned industrial turbomachinery rotor using reduced-order modeling［J］.Journal of Engineering for Gas Turbines and Power,2002,124(4):311-324.
|
| [11] |
王建军,于长波,姚建尧,等.失谐叶盘振动模态局部化定量描述方法［J］.推进技术,2009,30(4):457-461.WANG Jianjun,YU Changbo,YAO Jianyao,et al.Vibratory mode localization factors of mistuned bladed disk assemblies［J］.Journal of Propulsion Technology,2009,30(4):457-461.(in Chinese)
|
| [12] |
于长波,王建军,李其汉.失谐叶盘结构的概率响应局部化特性［J］.航空动力学报,2010(9):2006-2012.YU Changbo,WANG Jianjun,LI Qihan.Probability characteristics for response localization of mistuned bladed disk assemblies［J］.Journal of Aerospace Power,2010(9):2006-2012.(in Chinese)
|
| [13] |
CAPIEZ-LERNOUT E,SOIZE C.Nonparametric modeling of random uncertainties for dynamic response of mistuned balded disks［J］.Journal of Engineering for Gas Turbines and Power,2004,126(7):610-618.
|
| [14] |
CAPIEZ-LERNOUT E,SOIZE C,LOMBARD J P,et al.Blade manufacturing tolerances definition for a mistuned industrial bladed disk［J］.Journal of Engineering for Gas Turbines and Power,2005,127(3):621-628.
|
| [15] |
LIM S H,BLADH R,CASTANIER M P,et al.Compact,generalized component mode mistuning representation for modeling bladed disk vibration［J］.AIAA Journal,2007,45(9):2285-2298.
|
| [16] |
CHOI B K,LENTZ J,RIVAS-GUERRA A J,et al.Optimization of intentional mistuning patterns for the reduction of the forced response effects of unintentional mistuning:formulation and assessment［J］.Journal of Engineering for Gas Turbines and Power,2003,125(1):131-140.
|
| [17] |
YAO Jianyao,WANG Jianjun,LI Qihan.Robustness analysis of mistuned bladed disk using the upper bound of structured singular value［J］.Journal of Engineering for Gas Turbines and Power,2009,131(3):32501.1-32501.7.
|
| [18] |
YAO Jianyao,WANG Jianjun,LI Qihan.Improved modal localization and excitation factors for understanding mistuned bladed disk response［J］.Journal of Propulsion and Power,2011,27(1):50-60.
|
| [19] |
KASZYNSKI A A,BECK J A,BROWN J M.Uncertainties of an automated optical 3D geometry measurement,modeling,and analysis process for mistuned integrally bladed rotor reverse engineering［J］.Journal of Engineering for Gas Turbines and Power,2013,135(10):102504.1-102504.8.
|
| [20] |
VISHWAKARMA V,SINHA A,BHARTIYA Y,et al.Modified modal domain analysis of a bladed rotor using coordinate measurement machine data on geometric mistuning［J］.Journal of Engineering for Gas Turbines and Power,2015,137(4):42502.1-42502.8.
|
| [21] |
BHARTIYA Y,SINHA A.Geometric mistuning identification of integrally bladed rotors using modified modal domain analysis［J］.Journal of Engineering for Gas Turbines and Power,2014,136(12):122504.1-122504.8.
|
| [22] |
VISHWAKARMA V,SINHA A.Forced response statistics of a bladed rotor with geometric mistuning［J］.AIAA Journal,2015,53(9):2776-2781.
|
| [23] |
BECK J A,BROWN J M,KASZYNSKI A A,et al.Geometric mistuning reduced-order models for integrally bladed rotors with mistuned disk--blade boundaries［J］.Journal of Turbomachinery,2015,137(7):71001.1-71001.11.
|
| [24] |
BECK J A,BROWN J M,KASZYNSKI A A,et al.Mistuned response prediction of dual flow-path integrally bladed rotors with geometric mistuning［J］.Journal of Engineering for Gas Turbines and Power,2015,137(6):62501.1-62501.9.
|
| [25] |
王增强.航空发动机整体叶盘加工技术［J］.航空制造技术,2013,42(9):40-43.WANG Zengqiang.Machining technology of aeroengine blisk［J］.Aeronautical Manufacturing Technology,2013,42(9):40-43.(in Chinese)
|
| [26] |
徐家文,赵建社.航空发动机整体构件特种加工新技术［M］.北京:国防工业出版社,2011.
|
| [27] |
陈光.航空发动机结构设计分析［M］.北京：北京航空航天大学出版社,2014.
|
| [28] |
BEIROW B,GIERSCH T,KüHHORN A,et al.Forced response analysis of a mistuned compressor blisk［J］.Journal of Engineering for Gas Turbines and Power,2014,136(6):62507.1-62507.13.
|
| [29] |
KENYON J A,GRIFFIN J H.Experimental demonstration of maximum mistuned bladed disk forced response［J］.Journal of Turbomachinery,2003,125(4):673-682.
|
| [30] |
BATAILLY A,AGRAPART Q,MILLECAMPS A,et al.Experimental and numerical simulation of a rotor/stator interaction event localized on a single blade within an industrial high-pressure compressor［J］.Journal of Sound and Vibration,2016,375:308-331.
|
| [31] |
CHOI Y S,FLEETER S.Aerodynamic damping effects on the resonant response of mistuned IBRs［R］.:AIAA Aerospace Sciences Meeting and Exhibit,2013.
|
DownLoad: